CN105314099A - Single-man manual-control rotorcraft - Google Patents

Abstract

The invention provides a single-man manual-control rotorcraft which is composed of a rotorcraft body, a rotor shaft cantilever tilt structure, a full-manual-control mechanism and a rotor head mechanism having an internal variable distance function. The rotorcraft body has a high-gravity center normal-three-point undercarriage structure, wherein the main rotorcraft body consists of a vertical column, a front beam, a back beam, an engine bracket and a front support beam. A steering wheel is arranged right ahead and empennages are arranged at the back. A driver seat and an engine are respectively at the front and the back of the vertical column. In the rotorcraft, a push-type propeller provides power and a three-point frame-type individual damping support mechanism having a rotor reactive force balancing device is used for balancing the reactive force generated to the rotorcraft body by air during operation of the rotor, so that the rotorcraft is improved in takeoff and landing stability. By means of the full-manual-control mechanism having a steering linking function, a driver can complete the operations comprising distance change of the rotor, rotor shaft tilt, flying direction turning and braking just like driving a motorbike.

Description

Single manual cyclogyro

Technical field

The present invention relates to a kind of aircraft in a kind of aviation aircraft, particularly relate to a kind of single manual cyclogyro of full manual mode operation.

Background technology

Day by day crowded along with ground communications, aircraft can become and realizes the inevitable development direction of multilevel traffic in the near future, and cyclogyro is owing to rising and falling apart from very short, not high to site requirements, and fault is when occurring, its spin forced landing function ratio helicopter is safer, and some has possessed the same function that takes off vertically of similar helicopter especially with function cyclogyro of prewhirling, due to structure, more than pure helicopter, even fixed wing aircraft is simpler, so fault rate is also very low, so such aircraft will more and more welcomed by the people.

The success from Xi Erwa 1923 invention cyclogyro to nineteen twenty-five, so far more than 90 year, cyclogyro brings the revolution of an aircraft, it much designs to be used in by reference on the rotor class aircraft such as helicopter always and continues into the present, initial cyclogyro has made innovation on the basis of fixed wing aircraft, install a pair additional can spin and produce auxiliary lifting and can the rotor of unpowered safe falling, develop into and mainly only rely on rotor lift to maintain flight afterwards, fully phase out fixed-wing mechanism, define a kind of aircraft family of taking the course of its own.

But at the beginning of cyclogyro invention, its control mechanism is according to its driving characteristics, in conjunction with the basis of having continued to use fixed wing aircraft control structure, major control mode uses not too large change till today always, namely the right hand holds a control stalk and controls lifting, left hand controls throttle, both feet by scrunch controlling party to, the helicopter pilot that this drive manner makes most of fixed-wing pilot and continued to use similar this operating mode equally can almost clog-freely accept very soon, but be a process being difficult to adaptation concerning ordinary people, the control of driver right-hand man and both feet is independently in addition, in each control mechanism that right-hand man and both feet control, trick has with a certain distance from the position of working control, all need relatively independent and complicated a set of function unit to realize between this distance, such control mechanism and for the driver of cyclogyro, maintaining maintenance is all one and comparatively bothers, and larger cost of manufacture can be increased for relatively independent and complicated a few cover function uniies wright.

Advance or tractor airscrew because cyclogyro power comes from driving engine, its diameter of propeller goes out greatly a lot than the fixed wing aircraft of same weight classes usually, when its screw propeller enters mode of operation, its oar face is while acting on air generation power, air also gives screw propeller and creates antagonistic force equally, after this antagonistic force is delivered to fuselage by propelling or tractor airscrew axle, can make fuselage centered by propelling or tractor airscrew axle, the generation transverse direction contrary with screw propeller hand of rotation is verted and is rolled, when starting heats state, although the support wheel of both sides and column are all subject to the impact of this power, but this antagonistic force is concentrated and is applied to on the support wheel of screw propeller hand of rotation opposite side during takeoff condition, and overcome by ground supports, once after fuselage side support wheel leaves ground, fuselage is in non-matted state, at this moment propeller reaction power will make fuselage, after support wheel leaves ground, slight inclination occur at once, experienced driver can grasp the rotor head of appropriateness adjustment in advance tilt angle and be balanced in repeatedly practising, but beginner is often therefore in a rush, when causing taking off, rotor destroys rotor because rolling excessive contacting to earth, even make fuselage and driver injured, such inclination has become the difficulty that a lot of beginner inspires awe even from distance, such inclination has also become grasp cyclogyro to drive and problem demanding prompt solution.

Comparing that fixed wing aircraft cyclogyro can propagate its belief on a large scale is because it is not high to site requirements, the coasting distance that rises and falls is shorter, but in order to reduce the dependence to place, the propeller hub that a lot of modern cyclogyro all have employed variable-distance and the rotor Mechanical Driven possessing power extractor structure are prewhirled mechanism, but the requirement of such cyclogyro to power is higher than conventional common cyclogyro, need larger driving engine, but possessing this Liang Zhong mechanism makes rotor can with the form of displacement under low resistance 0 degree of state of angle of attack simultaneously, enter in spinning speed scope very soon by Mechanical Driven, and after entering desired speed, by recover flying angle be that cyclogyro obtains comparatively high lift instantaneously, do like this and not only can substantially reduce rotor and enter the required time of prewhirling, also ground run distance is substantially reduced, the sufficient cyclogyro of some power even can rely on the pre-cyclone of machinery to realize original place richochet completely, the just pre-cyclone of machinery and traditional variable-distance rotor hub complex structure, except because part is too much except the increase of causing trouble rate, these parts are arranged on cyclogyro, a lot of additional weight can be added to complete machine.

Exactly because above reason, the rotor of the single or double cyclogyro of major part is all adopt the angle of attack to fix unadjustable, and the structure be directly fastened on the propeller hub of seesaw type, like this simple and practical, but because rotor angle-of-attack is fixed, enter in spin states process and have certain resistance, this resistance make rotor cyclogyro move ahead sliding run the double action of brushing with propeller race under enter proper spin rotating speed and need enough coasting distances, take-off venue be there are certain requirements, what usually a lot of cyclogyro adopted is strains brake and makes the main support wheel of fuselage keep quiescence and the rotor using propeller race to brush hypsokinesis enters suitable flight rotating speed, then releasing of brake enters sliding race flight, do although it is so and can reduce directly with the requirement of rolling start to place length, but need to provide enough wake flows to brush the time by screw propeller.

Summary of the invention

Single manual cyclogyro of the present invention, not enough for prior art, while reservation traditional rotor machine advantage, propose that a kind of structure is simple, cost and maintenance cost cheap, the single manual cyclogyro that drive manner is more terse.

The technical solution adopted in the present invention: a kind of single manual cyclogyro, by fuselage sections, rotor head mechanism, rotor shaft cantilever inclining rotary mechanism, full manual mechanism composition.

Described fuselage sections has used for reference traditional positive bikini alighting gear fuselage, adopt and settle a steering front wheel in dead ahead, both sides are main is supported for two side support wheels, pusher propeller is power, the common form that empennage is rearmounted, left and right support wheel adopts 3 framework type independence shock-absorbing supports, and entirety is high center of gravity topological design, and fuselage sections is primarily of fuselage main support and 3 framework type independence shock-absorbing support mechanism two parts compositions with propeller reaction thrust balancing device.

Described fuselage main support is by column, front-axle beam, pedal, gauge panel column, gauge panel, the back rest, engine bed beam, front support beam, driving engine, pusher propeller, motor support column, Deng brachium dual control wisp, turn to connector loop, turn to commutation shift fork, can constant speed throttle, left and right support wheel, steering front wheel, front steering wheel shaft, empennage, caudal wing shaft, tail wheel, rotor, vert pull bar, radiator-water box, operator's saddle, column lower end connecting strap, balance wing axle bed, balance wing axle, front support beam lower end connecting cleat, engine beam lower end connecting cleat, double-threaded screw bar, the spherical plain bearing rod end nut composition of horizontal support bar.

Column occupies fuselage central authorities and erects and omit hypsokinesis, its upper end is used for rotor head mechanism, the both hands control stalk mechanism of rotor shaft cantilever inclining rotary mechanism and full manual mechanism, column lower end head turns to the column lower end connecting strap of the connecting bore being connected foundation bolt to be connected on back rest front end position more rearward with clamping plate form under being had by two pieces of front ends, column stage casing upper position, be connected and fixed forward the front-axle beam of a test forward, be fixedly connected with the engine bed beam of a level backward, connected by a motor support column erect between the fuselage back rest stage casing of engine bed beam rear end and below thereof and support, termination, back rest front end connects the front support beam that stretches out of oblique upper forward, front support beam upper end by clamping plate connecting strap with to be fixedly connected with in the middle part of front-axle beam and supplemental support front-axle beam, be connected to front support beam lower end and the front support beam lower end connecting cleat lower end between back rest front end and motor support column lower end connecting cleat lower end be connected with back rest two side backward under stretch out back rest lower surface, form two for installing the clamping plate shape space of balance wing axle bed, the square bulk of balance wing axle bed outside support, balance wing axle bed left and right width is identical with rear beam width and front/rear end is processed with a balance wing axle installs through hole, two balance wing axle beds are close to bottom the back rest with the square upper end face of outside, between the clamping plate space that two sides embedding front support beam lower end connecting cleats of balance wing axle bed and motor support column lower end connecting cleat lower end are formed, the circular mounting through hole run through between two balance wing axle bed front/rear ends is the arrangement of front and back concentric below the back rest, balance wing axle two terminations of a tubulose penetrate the mounting hole at two balance axle bed centers respectively, be arranged on after between two balance wing axle beds below the back rest, the balance wing axle bed both sides of installing below front support beam lower end connecting cleat and motor support column lower end connecting cleat are run through respectively from the side by two double-threaded screw bars, balance wing axle and balance wing axle bed are fastened on below the back rest, after the threaded portion of two double-threaded screw rod end heads is protruding through the both sides of two balance wing axle beds, two threaded ends are respectively stretched out to both sides, two threaded end parts that every side is stretched out are connected with the spherical plain bearing rod end nut of two horizontal support bars of the same side is respectively fixed, nut top, the rod end joint ball-and-socket joint centre hole of two horizontal support bars becomes two horizontal connecting hole of 3 framework type independence shock-absorbing support mechanism bottoms of every side.

Operator's saddle and be placed in column front and back respectively using major diameter pusher propeller backward as the driving engine of power, operator's saddle and engine bottom are in equal height, wherein operator's saddle is a backrest is the seat of fuel tank, operator's saddle bottom be arranged on adopt clamping plate connecting strap to be connected with column front-axle beam rear end on, the top of the fuel tank backrest of operator's saddle be bolted be fixed on before column above stage casing on turn to and be connected on pedestal front end face, radiator-water box is fastened on column rear and is positioned at the position turning to and be connected above pedestal rear end, a gauge panel column is upwards installed by clamping plate connecting strap in the stage casing, front-axle beam front end of front end test, flight gauge panel is installed in gauge panel column upper end, gauge panel column bottom front is horizontally installed with a pedal, because the design's body nodal point is higher, it is upper and lower that the front-axle beam front end pedal of test is convenient to driver, front-axle beam front end installs the front steering wheel shaft that a bottom adopts trailing arm type shock-absorbing support downwards, steering front wheel is arranged on the towing arm lower end of front steering wheel shaft bottom, in the middle part of steering front wheel wheel shaft, side is provided with the spindle arm of the cantilevered steering front wheel that is stretched out on the left of fuselage, driving engine is placed on the engine bed beam that stretches out at column rear, a small-sized support tail wheel is installed with by connecting strap below back rest follower head, and upwards install one by clamping plate connecting strap and have and stretch out cantilevered spindle arm and self vertically rotating caudal wing shaft to the left, the full dynamic formula empennage of connection one above caudal wing shaft, the tailplane on empennage top and the center of thrust line of pusher propeller contour.

Described 3 framework type independence shock-absorbing support mechanism section with propeller reaction thrust balancing device be with the addition of the propeller reaction thrust balancing device be made up of a leg-of-mutton balance wing by tradition 3 framework type independence shock-absorbing support mechanisms and form with designing on this basis.

The presylvian fissure strut that 3 described every sides of framework type independence shock-absorbing support mechanism's fuselage all have, rear horizontal support bar, lateral support bar, left and right supports wheel shaft, water brake clamps, left and right support wheel captive nut and left and right support wheel composition, wherein left and right supports the wheel shaft that wheel shaft is the left and right support wheel that a transverse direction is installed and used, it is presylvian fissure strut that left and right supports wheel shaft, rear horizontal support bar, the common connection strong point of lateral support bar termination toward the outer side, left and right pivot shaft respectively has one section of main body to be the spindle nose of polished rod axial plane towards two terminations of fuselage inner side and outer side, spindle nose end is toward the outer side processed with outside thread, left and right supports two U-shaped engaging lugs that wheel shaft stage casing possesses presylvian fissure strut forward and lateral support bar upward, and a brake callipers towards the rear connects pawl, left and right supports wheel shaft and is connected by penetrating in rear horizontal support bar tubulose termination outwardly towards fuselage inner opposite end polished rod spindle nose, left and right supports the spindle nose of wheel shaft one end toward the outer side through after the left and right support wheel possessing brake disc wheel hub, fixed by left and right support wheel captive nut, left and right supports the middle-end of wheel shaft to be possessed and is respectively used to be connected presylvian fissure strut and lateral support bar engaging lug toward the outer side with the U-shaped engaging lug of two upward forward, left and right supports the water brake pincers that wheel shaft connection pawl is towards the rear used for fixing left and right support wheel.

The main body of presylvian fissure strut and rear horizontal support bar is all tubulose, presylvian fissure strut and rear horizontal support bar are all equipped with U-shaped towards the connection end in fuselage direction, inner side and are connected pawl, presylvian fissure strut toward the outer side termination is equipped with engaging lug, and rear horizontal support bar toward the outer side termination is tubulose termination.

The main body of lateral support bar is tubulose, and lateral support bar is a decoupling rod towards the upper end in fuselage direction, lateral support bar lower end bottom toward the outer side and towards the decoupling rod top of fuselage all with engaging lug.

The presylvian fissure strut of fuselage column both sides and rear horizontal support bar are connected pawl towards the U-shaped of inner side and are connected as bikini framework lower horizontal connecting bore with nut top, two the rod end joints ball-and-socket joint centre hole below fuselage back rest both sides front end and stage casing respectively by bolt, lateral support bar grows many than conventional lateral support bar, lateral support point position is higher, lateral support bar towards the upper end decoupling rod top of inner side engaging lug connect be supported on fuselage column is connected with operator's saddle fuel tank backrest upper end on turn to the U-shaped being connected pedestal both sides to connect on pawl, presylvian fissure strut, rear horizontal support bar and lateral support bar termination toward the outer side are all fastened on left and right and support on wheel shaft.

The connection end toward the outer side of presylvian fissure strut, rear horizontal support bar, lateral support bar is connected to be fastened on and installs after on left and right support wheel shaft, forms 3 framework type independence shock-absorbing support mechanisms with independent shock-absorbing function.

Described propeller reaction thrust balancing device is made up of a balance wing, balance wing is one piece of triangular fibre aerofoil, its principal plane and balance wing axle, presylvian fissure strut, the level triangle frame area that rear horizontal support bar is formed is identical, three limits of triangle aerofoil are processed to hollow sleeve tubular, can as required corresponding be enclosed within any side of fuselage by balance wing axle, presylvian fissure strut, on the triangle horizontal frame that rear horizontal support bar is formed, balance wing principal plane covers balance wing axle, presylvian fissure strut, on the triangle horizontal frame that rear horizontal support bar is formed, form a leg-of-mutton horizontal aerofoil.

According to the difference of pusher propeller hand of rotation, balance wing is arranged on and pusher propeller hand of rotation opposite side

Described rotor head mechanism by possessing the clamping plate type propeller hub mechanism of inner variable-distance and rotor shaft agent structure, rotor connection part three part forms.

The clamping plate type propeller hub mechanism section of described variable-distance is waved buffer shaft, up and down propeller hub face tie bolt by upper propeller hub face, lower propeller hub face, double-range ball bearing, displacement oscillating bearing, displacement oscillating bearing inner covering, rotor pitch change axes, rotary wing changing form apart from spindle nut, displacement buffering gum cover, displacement cushion compound sleeve, rotor.

Upper propeller hub face and lower propeller hub face are the identical and strip shape clamping plate of symmetry of two outward appearances, upper propeller hub face is provided with bolt connecting hole corresponding to each other with lower propeller hub face periphery, upper propeller hub face and center, lower propeller hub face are processed with a vertical double-range ball bearing mounting hole run through, the double-range ball bearing mounting hole of the center in upper propeller hub face and lower propeller hub face is processed with the limited step of double-range ball bearing overcoat upper and lower end face towards the faying face end face outside direction in upper propeller hub face and lower propeller hub face, upper propeller hub face and lower propeller hub face can be combined in the face of detaining by inner side binding end, propeller hub face and lower propeller hub face end face outside are distinguished upward and below, from upper propeller hub face and center, lower propeller hub face double-range ball bearing mounting hole on the end face of two ends, centered by double-range ball bearing mounting hole, along upper propeller hub face and lower propeller hub facing on the line of centers of each termination each corresponding be processed with one vertical run through end face outside in upper propeller hub face and lower propeller hub face displacement oscillating bearing mounting hole and one near external end head, the rectangle elongated hole that displacement cushions gum cover is installed, each displacement oscillating bearing mounting hole is processed with the limited step of displacement oscillating bearing overcoat towards upper propeller hub face and end face outside direction, lower propeller hub face, each displacement oscillating bearing mounting hole is used for installing an oscillating bearing with spherical joint inner sleeve as displacement oscillating bearing using radial direction as Impact direction, the part outer face upper propeller hub face and lower propeller hub face being cushioned the rectangle elongated hole of gum cover for installing displacement is processed to inclined-plane to end portion, the rectangle elongated hole of each correspondence in inner side in conjunction with end face being respectively processed with in two rectangular edges in double-row bearing mounting hole and external end head direction two recessed mounting grooves, when the inner side binding end of upper propeller hub face and lower propeller hub is connected to become a complete propeller hub shell in the face of detaining installation, the groove of these correspondences just defines one by one independently axle head location and installation hole, this rectangle elongated hole is used for being installed into two displacement cushion compound sleeves having penetrated polished rod shape towards the form level arranged side by side in upper propeller hub face and lower propeller hub two ends direction and the displacement retaining certain interval to each other cushions gum cover, and one is erect the displacement that vertical folder is contained between two displacement cushion compounds cover gaps of installing side by side and waves buffer shaft.

The two-port up and down of trepanning each opposed installation displacement oscillating bearing inner covering in each displacement oscillating bearing spherical joint, displacement oscillating bearing inner covering is the round sleeve that lining between trepanning and rotor pitch change axes and outside in displacement oscillating bearing spherical joint is provided with protruding annular stop step, the limited step of axle sleeve outer face is divided into the thin two parts of one section of thick one section of summary, slightly thin one end external diameter but length identical with displacement oscillating bearing internal diameter is the half of the spherical joint inner sleeve axial width of displacement oscillating bearing, two displacement oscillating bearing inner coverings are respectively from the two ends opposed insertion displacement oscillating bearing spherical joint inner sleeve of displacement oscillating bearing spherical inner sleeve endoporus, the limited step of displacement oscillating bearing inner covering outer face is stuck on two ports of displacement oscillating bearing spherical joint inner sleeve endoporus, displacement oscillating bearing inner covering endoporus is used for penetrating rotor pitch change axes, the thicker external end head end face of displacement oscillating bearing inner covering two is for supporting rotor clamping plate.

Rotor pitch change axes and rotary wing changing are a nut through the bolt shank the two linked together while the displacement oscillating bearing inner covering in rotor clamping plate and displacement oscillating bearing endoporus and coupling thereof apart from spindle nut.

Displacement buffering gum cover is limited and makes and cushion the circular tube shaped rubber coating that rotor waves shimmy amplitude, displacement buffering gum cover diameter be greater than propeller hub face be combined with lower propeller hub face external end head after thickness, but displacement buffering gum cover diameter is slightly less than spacing between the thicker external end head end face of displacement oscillating bearing inner covering two in the spherical joint inner sleeve of two opposed insertion displacement oscillating bearings, the displacement cushion compound sleeve being slightly longer than the polished rod shape axial plane of displacement buffering gum cover by one in two end face center holes of its tubular penetrates and outside two ends, stretches out two spindle noses

The displacement that after upper propeller hub face is combined with lower propeller hub face, two penetrate displacement cushion compound sleeve on each side head cushion gum cover and is arranged in the rectangle elongated hole that upper propeller hub face is combined with lower propeller hub face on each side head afterwards side by side, two spindle noses of the displacement cushion compound sleeve stretched out outside each displacement buffering gum cover two ends, upper propeller hub face and lower propeller hub face in conjunction with time embed recessed mounting groove corresponding to two ends rectangle elongated hole two rectangular edges in conjunction with time the axle head location and installation hole that formed in

The round sleeve of to be thick and face, termination, curved recessed two ends, a stage casing be plane that rotor waves buffer shaft and one penetrate the double-threaded screw bar composition of axle sleeve, and rotor is waved between the Flat-end of axle sleeve two ends, buffer shaft stage casing and is arranged between displacement oscillating bearing inner covering two the external end head end faces in displacement oscillating bearing contour.

Rotor is waved in the gap that the curved recessed part in buffer shaft round sleeve stage casing is installed between two displacement buffering gum covers arranged side by side, rotor waves double-threaded screw bar two ends that buffer shaft center the penetrates axle sleeve end face outside towards upper propeller hub face and lower propeller hub face, the upper and lower end face that rotor waves round sleeve two terminations in buffer shaft stage casing is plane, use for supporting rotor clamping plate, the double-threaded screw bar that the round sleeve center that rotor waves buffer shaft stage casing penetrates is supported and fixed between rotor clamping plate for the round sleeve connection of rotor being waved buffer shaft.

Upper propeller hub face and lower propeller hub face are installed in the face of detaining by the inner side binding end in upper propeller hub face and lower propeller hub face, and installed by the face of the propeller hub up and down tie bolt bolt hole that upper propeller hub face is corresponding with lower propeller hub face periphery and penetrate upper and lower propeller hub face tie bolt and fixed, double-range ball bearing, displacement oscillating bearing, displacement buffering gum cover, displacement cushion compound sleeve, rotor are waved buffer shaft and be arranged on wherein, forms the clamping plate type propeller hub that can connect two panels rotor.

Described rotor shaft body structure portion is made up of rotor shaft, the horizontal axle sleeve of rotor shaft, rotor shaft upper end locking nut, pitch change axes Limit screw, pitch change axes, pitch change axes lower end connecting pins axle, double end spherical plain bearing rod end, displacement cantilever, pitch change axes bearing, pitch change axes bearing flange, pitch change axes bearing flange tie bolt, displacement spherical plain bearing rod end screw rod, pitch change axes upper end captive nut.

Rotor shaft is a rotor shaft in inversion T-shaped outward appearance, rotor shaft main body forms by by the vertical shaft of a hollow and the vertical shaft root lateral shaft that both sides are stretched out to the left and right, the vertical shaft upper end of rotor shaft is the cylindrical vertical shaft erectting extension upward, rotor shaft lower end main shaft root is thicker bulk four prismatic, between former and later two roots of main shaft root, inclined-plane is processed in lower surface, aft end face is slightly long and to downward-extension, main shaft root front/rear end upper end is processed with a pre-and post perforative caging bolt hole near circular vertical shaft root place, face, main side, two sides, left and right is plane, center, face, main side, left and right respectively to left and right separately level stretch out a lateral shaft, two lateral shafts are segmented from inside to outside and are processed in step-like tapered three parts, light over glaze body is divided near a lateral shaft root part and center section part, lateral shaft stage casing light over glaze body divides the spline being processed with tiltedly below rotor shaft lateral shaft spline forward, the outwardly directed end section of lateral shaft is processed with screw thread.

Four parts are from bottom to top processed in the outside of the vertical shaft part for rotor shaft that rotor shaft four prismatic main shaft root upwards extends, close main shaft root one section is polished rod axial plane, middle part is processed with the limited step of the double-range ball bearing of an evagination, double-range ball bearing limited step is upwards processed with the bearing installation position of the double-range ball bearing in one section of light face, and the bearing installation position vertical shaft top end part upwards of double-range ball bearing omits thin and is processed with outside thread.

The installation axle hole of the pitch change axes processing hollow light face circle is run through up and down from vertical shaft operative tip to main shaft root bottom, the circular shaft bore being wherein positioned at main shaft root portion is slightly thick, and with upwards in the junction of the circular shaft bore portion U-shaped that is processed into an interior pitch change axes lower end be connected the mounting limit step of the upper surface of pawl

Pitch change axes is a middle part main shaft is polished rod axle, the U-shaped that bottom is processed with down connects pawl, top is be threaded the pitch change axes bearing installation position of rod end head and the axle of setting use, bottom it, be divided into U-shaped to top connect pawl, main shaft polished rod axial plane, three, the installation position part of pitch change axes bearing 48, U-shaped connects pawl, main shaft polished rod axial plane, two steps processed between pitch change axes bearing installation position are divided in tapered three parts, it is excessively step-like between boundary bottom polished rod axle that U-shaped connects in the middle part of upper end, radix unguis portion and slightly thin pitch change axes, the lower end of its main shaft polished rod shaft portion connects the axle root place of pawl transition shoulder near its U-shaped, with U-shaped connect two connecting bores corresponding on pawl towards in the position of 90 degree of angles, be processed with an elongate in shape along a pitch change axes above-below direction pre-and post perforative spacing hole corresponding near the caging bolt hole at circular vertical shaft root place with rotor shaft main shaft root front/rear end upper end, main shaft polished rod axle both sides axial plane is processed with an oil resevoir from top to down separately, step between pitch change axes bearing installation position, top and main shaft polished rod axial plane is the mounting limit step of pitch change axes bearing inner sleeve lower port, polished rod shaft portion on the mounting limit step of pitch change axes bearing inner sleeve lower port is the installation site of pitch change axes bearing inner sleeve, top is slightly thin thread rod.

Two connection pawls that U-shaped connection pawl in pitch change axes takes the shape of the letter U down, bottom pitch change axes, U-shaped down connects between two connecting bores corresponding on pawl, be installed into a spherical plain bearing rod end nut and dock with a spherical plain bearing rod end bolt upper end forming displacement double end spherical plain bearing rod end, by penetrate one to be connected the isometric pitch change axes lower end connecting pins axle of connecting bore olo on pawl with pitch change axes U-shaped while, also through the upper end bearing hole connecting the double end spherical plain bearing rod end upper end of the displacement two connecting bores corresponding on pawl at U-shaped, displacement is connected with double end spherical plain bearing rod end upper end and is suspended on pitch change axes lower end U-shaped and connects two that pawl takes the shape of the letter U and connect between pawls.

Pitch change axes upper end penetrates in the pitch change axes mounting hole in the rotor shaft in inverted T-shaped from bottom to top, pitch change axes bottom U-shaped connect radix unguis portion bottom upper surface and pitch change axes main shaft between transition shoulder spacing by the limited step of the pitch change axes U-shaped pawl in rotor shaft main shaft root, the connecting pins axle two ends, pitch change axes lower end that pitch change axes lower end U-shaped connects between pawl are spacing by rotor shaft main shaft root circular shaft bore inwall, load the pitch change axes main shaft polished rod axial plane part of rotor shaft inside and U-shaped connect the lower port of pre-and post perforative strip shape spacing hole between the step-like root of pawl and rotor shaft main shaft root front/rear end upper end corresponding near pre-and post perforative caging bolt hole, circular vertical shaft root place, and the strip spacing hole lower port penetrated by pitch change axes Limit screw in the pitch change axes in face, rotor shaft rear and front end and rotor shaft adds in case turn round and move up and down the spacing of amplitude to pitch change axes, pitch change axes Limit screw makes to penetrate pitch change axes in rotor shaft and can not twist, and make the limited field of pitch change axes using the spacing between the upper and lower port of the strip spacing hole on it as its upper and lower displacement movement, loading the transverse axis center that on the pitch change axes lower end U-shaped connection pawl in the middle of rotor shaft, two corresponding connecting bore centers and rotor shaft main shaft root extend towards the left and right sides is that concentric arranges, connect the U-shaped being suspended on pitch change axes and to connect between pawl that the other end of double end spherical plain bearing rod end is sagging stretches out rotor shaft bottom.

The pitch change axes bearing installation position part axis body penetrating the pitch change axes top of rotor shaft from bottom to top stretches out for connection displacement cantilever from rotor shaft upper end.

The horizontal axle sleeve of rotor shaft is the round sleeve that two termination external process have raised annular limited step, the horizontal endoporus of axle sleeve of rotor shaft is identical near the light over glaze diameter of main shaft root portion with the lateral shaft of the rotor shaft both sides of inverted T-shaped, is socketed on the lateral shaft of inverted T-shaped rotor shaft both sides towards the mode inside rotor shaft main shaft root with the horizontal axle sleeve bottom protrusion annular stop step one end of rotor shaft.

The combination of rotor shaft main body and clamping plate type propeller hub is protruded upward from trepanning in the double-range ball bearing at clamping plate type propeller hub center by the screwed upper end of its vertical shaft part by rotor shaft, double-range ball bearing limited step in rotor shaft is by spacing towards lower port for the double-range ball bearing inner sleeve at clamping plate type propeller hub center, rotor shaft vertical shaft stretches out the double-range ball bearing inner sleeve threaded end upwards at clamping plate type propeller hub center, fix double-range ball bearing inner sleeve upper port by rotor shaft upper end locking nut, the clamping plate type propeller hub of rotor shaft and fixing double-range ball bearing is linked together.

In rotor shaft, protrude upward the termination, pitch change axes bearing installation position, pitch change axes upper end at rotor shaft top, be used for being connected with displacement cantilever.

Displacement cantilever is one and has the symmetrical bearing seat stretching out two cantilevers below two skew backs, the cantilever termination of stretching out to both sides is processed with downward tapped bore, the bolt hole of two cantilever terminations at right angle setting displacement spherical plain bearing rod end screw rod from bottom to top separately, bearing seat between its two cantilevers is provided with a pitch change axes bearing mounting hole, pitch change axes bearing mounting hole periphery has the bolt connecting hole of pitch change axes bearing flange, pitch change axes bearing mounting hole lower port has the limited step of pitch change axes bearing outside lower port, after pitch change axes bearing is fit into the pitch change axes bearing mounting hole in displacement cantilever centre, by the top of displacement cantilever center pitch change axes bearing mounting hole, a pitch change axes bearing flange be installed and be connected and fixed by pitch change axes bearing flange tie bolt, the pitch change axes bearing inner sleeve being arranged on displacement cantilever centre is socketed in pitch change axes from the top down and stretches out on the pitch change axes bearing installation position of the upper end of rotor shaft, pitch change axes bearing inner sleeve lower port is spacing by the step between the pitch change axes bearing installation position on pitch change axes top and the main shaft polished rod axle of pitch change axes, after the slightly thin thread rod in pitch change axes top stretches out pitch change axes bearing inner sleeve upper port, be locked by pitch change axes upper end captive nut, the oblique front side that the displacement spherical plain bearing rod end screw rod that two cantilever terminations of displacement cantilever are installed overhangs displacement oscillating bearing position on clamping plate type propeller hub respectively to.

Described rotor connection part is waved buffer shaft nut by rotary wing changing form apart from pole socket, rotor, rotor clamping plate, rotor check screw, rotor.

Rotor clamping plate are one group of horizontal use with two pieces and the L-shaped strip shape connecting cleat of main body outward appearance, for being connected vertical between the upper and lower end face of each termination of clamping plate type propeller hub and the upper and lower end face of rotor, every group leader's bar shaped clamping plate are made up of clamping plate type propeller hub connection end and rotor connection end two parts, correspondingly on the vertical bar shaped end face of wherein rotor connection end part be processed with the bolt mounting holes connecting rotor, clamping plate type propeller hub connection end waves the installation axle hole of buffer shaft two-thread screw except possessing the rotor pitch change axes corresponding with clamping plate type propeller hub and rotor, and have the correspondence of face toward the outer side extend one less of installing the strip connecting arm of a rotary wing changing apart from pole socket.

Rotary wing changing is main body apart from pole socket is strip and block, the strip connecting arm area that main body upper and lower end face area and rotor clamping plate extend laterally is suitable, its height and rotor waves buffer shaft stage casing axle sleeve two ends Flat-end and the spacing that is arranged between displacement oscillating bearing inner covering two the external end head end faces in displacement oscillating bearing is contour, and upper and lower end face is processed with the corresponding bolt connecting hole of the strip connecting arm of organizing rotor clamping plate with each and is bolted to be supported on often to be organized between strip connecting arm corresponding on rotor clamping plate, at rotary wing changing apart from pole socket end face centre toward the outer side, there is the displacement spherical plain bearing rod end screw flight pipe link for being mounted on displacement cantilever termination stretched out outside Xiang Yigen.

The upper and lower end face correspondence of each termination of clamping plate type propeller hub installs one group of rotor clamping plate, often organize the upper and lower being arranged on the upper and lower end face of clamping plate type propeller hub termination between two pieces of clamping plate type propeller hub connection ends in the rotor clamping plate be arranged above and below respectively, often organizing the mounting hole of the rotor pitch change axes on rotor clamping plate front end and rotor, to wave the mounting hole of buffer shaft corresponding with the axis hole that the mounting hole of the rotor pitch change axes on the every one end of clamping plate type propeller hub and rotor wave round sleeve two ends, buffer shaft stage casing, the spindle nose that each rotor waves the double-threaded screw bar axle of buffer shaft waves axle sleeve two ends, buffer shaft stage casing through the rotor that the every one end of clamping plate type propeller hub rotor clamping plate is installed and the threaded shank portion of double-threaded screw bar spindle nose two ends is stretched out from often organizing rotor clamping plate end face and down upward, then wave buffer shaft nut by rotor to be connected and fixed.

Often organize the rotor being all subject to every one end of clamping plate type propeller hub of rotary wing changing distance pole socket and correspondence thereof is installed between rotor clamping plate to wave buffer shaft stage casing axle sleeve two ends Flat-end and be arranged on the common support of displacement oscillating bearing inner covering two the external end head end faces in displacement oscillating bearing.

The rotary wing changing of bolt shank from the upper surface rotor clamping plate being positioned at clamping plate type propeller hub as rotor pitch change axes penetrates in an upright manner apart from axis hole, through two displacement oscillating bearing inner coverings opposed in trepanning in displacement oscillating bearing in clamping plate type propeller hub, the rotary wing changing of bolt shank lower end from the lower surface rotor clamping plate being positioned at clamping plate type propeller hub as rotor pitch change axes passes apart from axis hole, and is fixed by the nut of this bolt shank.

Apart from pole socket, end-face helical pipe link termination is corresponding toward the outer side with being fixed on the rotary wing changing often organizing between strip connecting arm corresponding to rotor clamping plate for the ball-and-socket joint endoporus being arranged on two the displacement spherical plain bearing rod end screw rod lower ends sagging to front, clamping plate type propeller hub oblique side, displacement cantilever two ends, rotary wing changing after stretching out, and to be fixed apart from the pole socket threaded shank portion of nut to the ball-and-socket joint bore section stretching out displacement spherical plain bearing rod end screw rod lower end that whorl brace rod termination is mated toward the outer side by rotary wing changing through the ball-and-socket joint endoporus being arranged on two displacement spherical plain bearing rod end screw rod lower ends sagging to its front upper place, displacement cantilever two ends end-face helical pipe link termination toward the outer side apart from pole socket.

The rotor connection end of rotor clamping plate is arranged on the two sides up and down of rotor with the end face correspondence of rotor tie bolt mounting hole, and after being connected and fixed by rotor check screw, is linked together respectively by two groups of rotors with clamping plate type propeller hub two terminations.

What clamping plate type propeller hub mechanism adopted is that rotor pitch change axes erects arrangement, the radial direction of displacement oscillating bearing is as Impact direction, while utilizing oscillating bearing can bear larger radial weight, its spherical joint inner sleeve can make the characteristic that inclination aligning by a relatively large margin rotates in the oscillating bearing overcoat with Internal Spherical Surface, the rotor pitch change axes of displacement oscillating bearing in clamping plate type propeller hub is inserted with the horizontal centrifugal tension born when rotor works of the two ends of its connection rotor clamping plate to erect attitude, make the spherical joint inner sleeve tilt slide amplitude in the displacement oscillating bearing of arrangement like this can meet the demand that rotor pitch change axes is waved up and down and lateral tilting transformation distance is movable simultaneously, rotor wave the curved recessed part in buffer shaft round sleeve stage casing be installed in two, each termination of clamping plate type propeller hub arranged side by side displacement buffering gum cover between gap in, rotor is waved buffer shaft and is utilized the curved recessed part in its round sleeve stage casing to wave up and down and in side shake process, displacement arranged side by side with two, its both sides all the time cushions gum cover and keeps the contact of squash type and realize rotor by the contact of squash type waving up and down and the buffering of side shake at rotor.

Owing to can make tilt slide by a relatively large margin in self in ball-type overcoat up and down as self outer spherical inner sleeve of displacement oscillating bearing, while meeting rotary wing changing distance needs, because displacement buffering gum cover diameter be greater than propeller hub face combines with lower propeller hub face external end head after thickness be still slightly less than between the thicker external end head end face of displacement oscillating bearing inner covering two in the spherical joint inner sleeve of two opposed insertion displacement oscillating bearings and spacing, be less than too and be arranged on that displacement oscillating bearing inner covering two external end head end faces in displacement oscillating bearing are contour and rotor that is common support rotor clamping plate waves spacing between the Flat-end of axle sleeve two ends, buffer shaft stage casing, point centered by the outer spherical inner sleeve of the displacement oscillating bearing that the rotor clamping plate of connection rotor can be connected by rotor pitch change axes, thus while leeway rotor being had wave up and down, rotor can also be made to wave in process up and down, the crimp utilizing displacement to cushion the outer face of gum cover is able to flexible buffer, thus reach when meeting rotor work and wave up and down and the needs of yaw.

Described rotor shaft cantilever structure of verting is made up of vert base holder portion, displacement return mechanism, anteversion and retroversion rotation mechanism three part of left and right.

The described left and right base holder portion that verts is made up of lateral tilting rotating shaft, lateral tilting rotating shaft axle sleeve, the pedestal front frame that verts, the pedestal after poppet that verts, the pedestal left and right clamping plate that vert, the clamping plate studdle that verts, the clamping plate studdle captive nut that verts, vert pedestal clamping plate and the tie bolt of base seat support of verting, displacement reset tension spring spacing limit shaft sleeve, displacement reset tension spring, the pedestal left and right clamping plate tie bolt that verts that has bracing wire adjusting base concurrently.

Lateral tilting rotating shaft main body is square bulk and the polished rod spindle nose of two concentrics is stretched out at center, face, rear and front end to two ends, the width of the gap ratio fuselage column front/rear end between lateral tilting rotating shaft left and right sides end face is slightly wide, the side end face, two, left and right of lateral tilting rotating shaft is all processed with one up and down between two row bolts hole and the two row bolts hole sunk coak laterally processed be connected with the cantilever that verts about clamping plate type, the outside face of the polished rod spindle nose of lateral tilting rotating shaft is socketed with termination, one end external process separately and becomes raised annular limited step and center is processed with the lateral tilting rotating shaft axle sleeve with the polished rod spindle nose equal diameter centre hole of lateral tilting rotating shaft, lateral tilting rotating shaft axle sleeve is socketed on the polished rod spindle nose of the lateral tilting rotating shaft that center, face, lateral tilting rotating shaft rear and front end is stretched out with one end of protruding limited step towards the form in face, lateral tilting rotating shaft rear and front end, be socketed in left and right vert the protruding limited step of lateral tilting rotating shaft axle sleeve on polished rod spindle nose towards front and back outer face between spacing between spacing with fuselage column front/rear end identical.

Vert pedestal front frame and the pedestal after poppet that verts is that two pieces of upper ends are semicircular end and centered by the center of circle of semicircular end-face, are processed with the mounting hole of lateral tilting rotating shaft axle sleeve and the lower end width strip shape plate identical with the left and right spacing width of fuselage column front/rear end, vert pedestal front frame forward strip shape plate end face the latter half and pedestal after poppet strip shape plate end face the latter half backwards of verting on be processed to long recess, vert pedestal front frame end face forward and vert in the recess sidewall of pedestal after poppet end face backwards, correspondence is processed with the tie bolt mounting hole of the pedestal left and right clamping plate that vert, the pedestal front frame that verts one in front and one in back is placed on the front/rear end on fuselage column top with the form that pedestal after poppet stretches out upper surface, fuselage column top with its upper end semicircular end part respectively of verting, vert pedestal front frame and the mounting hole at upper end semicircular end center between pedestal after poppet that verts is that concentric arranges, two spindle noses that two ends is socketed with the lateral tilting rotating shaft of lateral tilting rotating shaft axle sleeve are installed into the mounting hole at vert pedestal front frame and semicircular end center, pedestal after poppet upper end of verting respectively, lateral tilting rotating shaft is connected and is supported on above vert pedestal front frame and the fuselage column that verts between pedestal after poppet.

The pedestal left and right clamping plate that vert are two pieces of connecting cleats with the symmetry towards back boom, on the right opposed left and right end face being arranged on fuselage column top of one the first from left, vert clamping plate front end, pedestal left and right and middle part surface is processed with the tie bolt mounting hole corresponding with the pedestal front frame that verts on the front/rear end being placed in fuselage column top, pedestal after poppet side of verting, and every block to vert in the middle of pedestal left and right clamping plate cantilever backward with the mounting hole of a distance-variable rocker arm lateral shaft lining and is processed with the mounting hole of the clamping plate studdle that verts in cantilever follower head position.

The clamping plate studdle that verts is the double-threaded screw bars of two two ends with limited support step, the clamping plate studdle two ends limited support step that verts is identical with the width of the distance between left and right of fuselage column front/rear end, vert the two ends thread rod of clamping plate studdle for penetrating the mounting hole of the clamping plate studdle that verts verted on pedestal left and right clamping plate two cantilever follower heads, clamping plate studdle two ends of verting are supported verting between pedestal left and right clamping plate two cantilever terminations backward with limited support step, pedestal left and right clamping plate end face outside of verting is stretched out in the vert thread rod termination of clamping plate studdle, and fixed by the captive nut of the clamping plate studdle that verts.

Vert pedestal front frame, vert pedestal after poppet, verting between the clamping plate of pedestal left and right can be connected to each other with the tie bolt of the base seat support that verts by the pedestal left and right clamping plate that vert is fixed on the end face of four, fuselage column top, vert after the front end that has the pedestal left and right clamping plate tie bolt that verts of bracing wire adjusting base concurrently by one between the bolt hole corresponding with bottommost on the pedestal left and right clamping plate that vert of both sides, pedestal front frame front end face recess sidewall bottom is inserted to the right on the left of fuselage column and be connected and fixed, the follower head having the pedestal left and right clamping plate tie bolt that verts of bracing wire adjusting base concurrently is thicker, thereafter termination by under a hollow bracing wire adjusting screw(rod) is installed upward.

To vert between the bolt hole corresponding with bottommost on the pedestal left and right clamping plate that vert of both sides, pedestal after poppet aft end face recess sidewall bottom when penetrating the pedestal left and right clamping plate that vert and being connected with the tie bolt of the base seat support that verts, it is the displacement reset tension spring spacing limit shaft sleeve of hollow thin-wall pipe spreader by a main body, be placed in and vert between the bolt hole of pedestal after poppet groove bottom on two sidewalls, displacement reset tension spring spacing limit shaft sleeve two ends and vert between pedestal after poppet groove two sidewalls and keep certain interval, this gap is for installing the lower end of two two ends with the displacement reset tension spring of loop-hook, and fixed spacing to the loop-hook of displacement reset tension spring lower end.

The pedestal left and right clamping plate that vert are installed by its cantilever termination and are connected displacement return mechanism.

Described displacement return mechanism is made up of distance-variable rocker arm, distance-variable rocker arm lateral shaft lining, displacement shifting fork bar, displacement shifting fork bar spline, horizontal pitch change axes captive nut, distance-variable rocker arm pin axle.

Distance-variable rocker arm is the double end rocking arm of a horizontal use, a rectangular through holes is processed with between rocking arm main body upper and lower end face, rocking arm main body is made to form a strip shape square frame, distance-variable rocker arm using strip shape square frame both sides strip plate face as rocking arm end face, the follower head in distance-variable rocker arm strip plate face and midway location respectively have two to stretch out circular lateral shaft to both sides correspondence level, the slightly thin lateral shaft in distance-variable rocker arm follower head position is crossed strip resetting shaft, two spindle noses of crossed strip resetting shaft run through the strip plate surface rear end head left and right sides of strip shape square frame both sides, spindle nose end is respectively processed with a ring annular groove, and to be used for mounting two two ends spacing to it with the upper end of the displacement reset tension spring of loop-hook.

What outside two strip plate faces of the strip shape square frame distance-variable rocker arm, middle part was stretched out to both sides is horizontal pitch change axes, horizontal pitch change axes root is slightly thick, main body is polished rod axle, shaft end is comparatively thin and be processed with screw thread, thinner shaft end and thicker root are processed with transition shoulder, wherein the polished rod shaft portion of the horizontal pitch change axes in left side compares the horizontal pitch change axes slightly length of opposite side, it compares the slightly longer part polished rod axle of the horizontal pitch change axes of opposite side towards on the surface of front end, be processed with one for being connected and fixed the installation groove of the horizontal pitch change axes spline of displacement shifting fork bar, near the position in horizontal pitch change axes front, correspondence is processed with the mounting hole of the distance-variable rocker arm pin axle that is connected for the double end spherical plain bearing rod end lower end ball-and-socket joint axis hole of same pitch change axes lower end connecting pins axle connection.

When the lower end of the double end spherical plain bearing rod end lower end ball-and-socket joint of pitch change axes lower end connection stretches out below rotor shaft, after in the strip shape square frame of reeve distance-variable rocker arm hollow, by the distance-variable rocker arm pin axle of the two ends length polished rod axial plane identical with the spacing of the strip shape square frame lateral surface of distance-variable rocker arm hollow while the strip plate face, strip shape square frame both sides through distance-variable rocker arm hollow, be also fixed in the strip shape square frame of distance-variable rocker arm hollow through the axis hole and connecting of double end spherical plain bearing rod end lower end simultaneously.

Distance-variable rocker arm lateral shaft lining is that two bottoms are with protruding outer ring step and the isodiametric round sleeve of horizontal pitch change axes polished rod axle of interior axis hole and distance-variable rocker arm both sides, the distance-variable rocker arm lateral shaft liner sleeve length horizontal pitch change axes polished rod partial-length shorter with distance-variable rocker arm is identical, distance-variable rocker arm lateral shaft lining is socketed in the horizontal pitch change axes of distance-variable rocker arm both sides in its protruding outer ring step mode to the inside, bottom it, ring-shaped step termination is to the inside close on distance-variable rocker arm strip shape square frame outer wall, distance-variable rocker arm pin axle two ends are limited in distance-variable rocker arm strip shape square frame, distance-variable rocker arm lateral shaft lining towards both sides ring-shaped step outer face between spacing and the both sides of fuselage column front/rear end width identical, distance-variable rocker arm lateral shaft lining towards the external end head of both sides end face between spacing be arranged on the fuselage column end face left and right sides vert pedestal left and right clamping plate towards outside end face between width spaces identical.

When being arranged on the pedestal left and right clamping plate that vert on fuselage column top, vert pedestal front frame, when the pedestal after poppet that verts connects, distance-variable rocker arm with its one end with crossed strip resetting shaft backwards and overall horizontal form is installed between two cantilevers that two pieces of pedestal left and right clamping plate that vert extend to fuselage column rear, in the middle of distance-variable rocker arm, two are socketed with the horizontal pitch change axes spindle nose end of distance-variable rocker arm lateral shaft lining, protruding from the mounting hole of two pieces of distance-variable rocker arm lateral shaft linings pedestal left and right clamping plate cantilever backwards that vert respectively, the distance-variable rocker arm lateral shaft lining outer face that distance-variable rocker arm both sides are socketed in horizontal pitch change axes flushes with the pedestal left and right clamping plate outer face that verts after penetrating the distance-variable rocker arm lateral shaft bush hole of verting on the clamping plate cantilever of pedestal left and right, longer this one end polished rod shaft portion of horizontal pitch change axes on the left of distance-variable rocker arm is after stretching out the pedestal left and right clamping plate outer face that verts, to be arranged in the displacement shifting fork bar termination of installing from the left-external side of the pedestal left and right clamping plate that vert in axis hole in the way to insert.

Displacement shifting fork bar is the cantilever that a left-external side from the pedestal left and right clamping plate that vert is installed, its front end free end headband has the displacement bracing wire of U-shaped to connect pawl, termination side straps is fixed in rear end has the axis hole identical with the polished rod axle external diameter of horizontal pitch change axes longer on the left of distance-variable rocker arm and the installation groove accordingly with horizontal pitch change axes spline forward, displacement shifting fork bar connects pawl termination towards fuselage column front with the displacement bracing wire of U-shaped, connect spacing horizontal pitch change axes spline insertion displacement shifting fork bar rear end as radial direction to fix in spline groove corresponding between axis hole with pitch change axes horizontal on the left of distance-variable rocker arm in termination.

The horizontal pitch change axes two ends threaded portion of distance-variable rocker arm is stretching out on vert pedestal left and right clamping plate outer face and displacement shifting fork bar after axis hole respectively, fixed respectively by two horizontal pitch change axes captive nuts, displacement shifting fork bar distance-variable rocker arm and outside thereof connected is arranged on the cantilever that two pieces of pedestal left and right clamping plate that vert extend to fuselage column rear in horizontal mode.

Distance-variable rocker arm defines between the spindle nose of crossed strip resetting shaft and the distance-variable rocker arm pin axle near horizontal pitch change axes front position and is mounted on distance-variable rocker arm both sides two Length discrepancy lever arm of force that the horizontal pitch change axes of verting on the clamping plate of pedestal left and right is a dot center, wherein the spacing of distance-variable rocker arm rear end crossed strip resetting shaft and horizontal pitch change axes is equivalent to horizontal pitch change axes and the several times near spacing between the distance-variable rocker arm pin axle below it, lever arm of force as by the horizontal pitch change axes of distance-variable rocker arm a centered by fulcrum same with the displacement shifting fork bar that termination on the left of the horizontal pitch change axes on distance-variable rocker arm links together, its lever length is the several times of the lever arm of force between the horizontal pitch change axes on distance-variable rocker arm to the lever arm of force and horizontal pitch change axes to distance-variable rocker arm pin axle of two spindle noses of crossed strip resetting shaft.

The loop-hook of two displacement reset tension spring lower ends is connected to pedestal after poppet aft end face groove bottom of verting, two displacement reset tension spring upper end loop-hooks are connected on the crossed strip resetting shaft of distance-variable rocker arm rear end, two displacement reset tension springs, under the effect of autogenous shrinkage pulling force, remain the distance-variable rocker arm pin thrust axially to connecting double end spherical plain bearing rod end lower end axis hole in distance-variable rocker arm.

The same side being arranged on displacement shifting fork bar vert pedestal front frame front lower end on have bracing wire adjusting base concurrently the hollow bracing wire adjusting screw(rod) centre hole installed of the pedestal left and right clamping plate tie bolt root that verts and the displacement bracing wire of the U-shaped on displacement shifting fork bar to connect pawl corresponding, the end of displacement bracing wire is through this hollow bracing wire adjusting screw(rod) centre hole, and the displacement bracing wire being connected to the U-shaped on displacement shifting fork bar connects on pawl.

Described anteversion and retroversion rotation mechanism part is made up of the cantilever that verts about clamping plate type, left and right cantilever rear end bracing frame, left and right cantilever rear end bracing frame tie bolt, rotor shaft arm, rotor shaft lateral shaft stage casing spline, rotor shaft vert cantilever bolt of rear end plate, the pull bar that verts of arm captive nut, left and right that vert that vert that vert that vert.

Vert pedestal front frame with vert pedestal after poppet by the connection with the pedestal left and right clamping plate that vert lateral tilting rotating shaft connected be supported on above fuselage column time, lateral tilting rotating shaft is all connected with the cantilever that verts about clamping plate type with the sunk coak of the bolt hole connected corresponding to the cantilever that verts about clamping plate type with transverse direction by two side end faces about it.

The cantilever that verts about clamping plate type is two pieces of edge-on uses of transverse direction and the oblong strip board of symmetry, the side surface of side surface and lateral tilting rotating shaft main body is between the upper and lower apart from wide, two pieces of strip board front ends are the connection end of lateral tilting rotating shaft, except being processed with the bolt connecting hole corresponding with side, lateral tilting rotating shaft main body both sides at side surface on connection end, and on the inner surface corresponded to each other, be processed with the horizontal tenon step that sunk coak horizontal with lateral tilting rotating shaft main body both sides is corresponding and isometric, the side surface middle position center of strip board rear end cantilever is provided with the mounting hole of the horizontal axle sleeve of rotor shaft, and near this termination along mounting hole cross cut end (of a beam) upper-lower position being processed with about two the cantilever rear end bracing frame tie bolts that vert.

The cantilever that verts about clamping plate type is inwardly connected and fixed the two with the form of clamping plate from lateral tilting rotating shaft and rotor shaft both sides, the cantilever that verts about clamping plate type utilizes the horizontal tenon step of its front end connection end inner surface to embed in the horizontal sunk coak in lateral tilting rotating shaft main body both sides, and bolt connecting hole corresponding with side, lateral tilting rotating shaft main body both sides for cantilever front end of verting about clamping plate type is connected and fixed by the cantilever bolt of rear end plate that verts about utilizing, cantilever front end of verting about clamping plate type is mounted on lateral tilting rotating shaft both sides, the left and right sides end distance ratio of the square block-shaped main body of lateral tilting rotating shaft verts pedestal front frame, the pedestal after poppet end face that verts is slightly wide, the end face part that the cantilever that verts about making the two clamping plates formula be connected with lateral tilting rotating shaft oblong block-shaped main body both sides is downward and vert and keep certain between the end face of pedestal after poppet side left and right and vert gap, this gap makes lateral tilting rotating shaft rear and front end spindle nose distance to bear 8 degree and vert about vert pedestal front frame and pedestal after poppet upper end of verting be realizes centered by the axis hole that arrange of concentric, and the side end face of the end face that the cantilever that verts about driving two clamping plates formula is downward and pedestal after poppet both sides of verting comes in contact, realize verting the spacing of amplitude towards left and right sides to lateral tilting rotating shaft.

The cantilever that verts about two clamping plates formula utilizes the horizontal axle sleeve mounting hole of the rotor shaft of its rear end central authorities to be socketed in rotor shaft from rotor shaft both sides to stretch out to both sides and be set with the lateral shaft of the horizontal axle sleeve of rotor shaft, annular stop step also identical with the width of lateral tilting rotating shaft front/rear end towards width between end face outside of the horizontal axle sleeve projection of rotor shaft on the lateral shaft being arranged on rotor shaft both sides, vert about the outer face of rotor shaft horizontal axle sleeve raised annular limited step supports two clamping plates formula cantilever inner side end, vert after cantilever about rotor shaft lateral shaft cover penetrates two clamping plates formula, the end face of the horizontal axle sleeve of two rotor shaft side outwardly flushes with the cantilever outer face that verts about two clamping plates formula,

Two lateral shaft stage casings of rotor shaft are protruding from the horizontal axle sleeve mounting hole of rotor shaft of cantilever rear end central authorities of verting about clamping plate type with the polished rod shaft portion of spline and end thread bar part, vert about clamping plate type the left and right of termination, cantilever rear end vert cantilever rear end bracing frame tie bolt mounting hole between, clamp one piece of vertically-arranged and use and vert in the left and right of the square plate bulk identical with lateral tilting rotating shaft front/rear end length and width cantilever rear end bracing frame, left and right bracing frame both sides, the cantilever rear end end face that verts is processed with the bolt connecting hole corresponding with the cantilever follower head that verts about clamping plate type, utilize left and right vert cantilever rear end bracing frame tie bolt is verted in left and right cantilever rear end bracing frame clamp be fixed on clamping plate type about vert between termination, cantilever rear end.

The left and right cantilever rear end bracing frame that verts verts the rear of rotor shaft main shaft root aft end face between cantilever about being installed in two clamping plates formula equally, and maintain the spacing gap of verting before and after rotor shaft between rotor shaft root aft end face, when verting before and after rotor shaft, rotor shaft main shaft root aft end face and bottom contact towards the axial end face of rotor with the cantilever rear end bracing frame that verts about clamping plate type, and the amplitude of verting before and after rotor shaft is limited between 0 degree ~ 18 degree.

Vert about clamping plate type cantilever by with lateral tilting rotating shaft, rotor shaft, vert the connection of cantilever rear end bracing frame in left and right, vert on cantilever cantilever termination backwards about the clamping plate type propeller hub connect rotor shaft and rotor shaft upper end and rotor are fastened on clamping plate type, having of verting about clamping plate type that cantilever front end connects left and right laterally verts that the spindle nose axial line at lateral tilting rotating shaft front/rear end center of function is connected with cantilever rear end of verting about clamping plate type have before and after the central axis of longitudinal lateral shaft in the rotor shaft of function that verts contour and on intermediate point between the lateral shaft of giving rotor shaft root to stretch out to both sides mutually, rotor shaft can realize verting all around by laterally vert rotor shaft that function and self both sides lateral shaft have an anteversion and retroversion rotating function of lateral tilting rotating shaft centered by this axial line intersection point.

From the external end head part of two lateral shafts of the outwardly directed rotor shaft of the horizontal axle sleeve mounting hole of rotor shaft of cantilever rear end central authorities of verting about clamping plate type for and two symmetries be arranged on clamping plate type about the rotor shaft of verting outside cantilever rear end vert between arm and connected.

The rotor shaft arm that verts is two horizontal uses and two the oblique cantilevers of termination not in same plane, the rotor shaft arm rear end fixed end headband that verts has the mounting hole of rotor shaft lateral shaft, and rotor shaft mounting hole is processed with the groove installing rotor shaft lateral shaft stage casing spline towards direction, free termination, rotor shaft vert arm front end free end headband have U-shaped connect pawl, the rotor shaft of the every side of cantilever of verting about clamping plate type is verted between free termination that arm straps has the fixing termination of rotor shaft lateral shaft mounting hole to be connected pawl with U-shaped and is connected each via the connecting arm stretched out sideling to front lateral direction after.

The vert rotor shaft lateral shaft mounting hole of arm rear end of rotor shaft is socketed in polished rod axle outside the cantilever that to vert about rotor shaft lateral shaft stretches out clamping plate type and rotor shaft lateral shaft end thread bar part, and by rotor shaft lateral shaft stage casing spline insert from outside to inside rotor shaft lateral shaft and rotor shaft vert spline corresponding to arm spacing after, stretch out the vert rotor shaft lateral shaft end thread bar part of arm rear end mounting hole of rotor shaft to be fixed by the rotor shaft arm captive nut that verts, vert between cantilever about two of rotor shaft root lateral shaft outer ends are fastened on two clamping plates formula,

The vert U-shaped of arm front end of two rotor shaft connects pawl respectively from two side direction fuselage stud sides fronts of the cantilever that verts about two clamping plates formula to stretching out, the vert U-shaped of arm of two rotor shaft is connected pawl and is fastened on by bolt on the upper end spherical plain bearing rod end of two pull bars that vert of fuselage column both sides respectively, the pull bar that verts to be two main bodys be tubulose two ends with spherical plain bearing rod end, for the connecting rod of the clamping plate type hub tilting work of push-and-pull rotor shaft and connection thereof.

Described full manual mechanism is by both hands control stalk mechanism and turn to combining mechanism to form.

Described both hands control stalk mechanism by composition control rod base, U-shaped draw-in groove bolt of rear end plate, the rotating shaft of control stalk lateral tilting, the rotating shaft of control stalk anteversion and retroversion, T-shaped vert trailing arm, U-shaped control stalk mount pad, control stalk steering bearing, turn to connector loop, control stalk steering bearing captive nut, left control stalk, right control stalk, left and right control stalk bolt of rear end plate, brake transition bracing wire, displacement bracing wire to form.

The rotating shaft of control stalk lateral tilting reverses faying face by the annular termination be connected, left and right and anticreep termination three part forms, annular termination, control stalk lateral tilting rotating shaft front end is the button-head that flat horizontal surface is processed in larger two side end faces, the flat end face center of control stalk lateral tilting rotating shaft annular termination is processed with one for installing the axis hole of control stalk anteversion and retroversion rotating shaft, and the rotating shaft of control stalk anteversion and retroversion is a horizontal use and is used as bolt shank and the nut thereof of the flat end face center shaft of the annular termination of control stalk lateral tilting rotating shaft.

Control stalk lateral tilting rotating shaft stage casing is that to reverse the part of faying face as left and right be one section of polished rod axle, the axial line of polished rod axle axial line and side end face, annular termination central shaft hole intersects vertically, transition shoulder is processed with between annular termination and stage casing polished rod axle, anticreep termination be two from stage casing polished rod shaft end at right angles to the anticreep limiting stopper that bilateral symmetry lateral projection is stretched out, anticreep limiting stopper stretches out direction and becomes 90 degree with the axis hole direction at center, annular termination to both sides, the stage casing of control stalk lateral tilting rotating shaft and rear end are used for being arranged in control stalk pedestal with the form inserted.

Control stalk pedestal is a pedestal being connected and fixed the rotating shaft of control stalk lateral tilting, its main body is two inner side ends long strip-board shape column connecting arm composition in opposite directions that a block control stalk Connection Block of front end and the rear end level backward that is connected with it are stretched out, formed between the aft end face plane of control stalk Connection Block part and control stalk Connection Block part two long strip-board shape column connecting arms that level is stretched out backward and can block fuselage column front end face and left and right end face U-shaped draw-in groove, two long strip-board shape column connecting arm ends omit the corresponding connecting bore being processed with two U-shaped draw-in groove bolt of rear end plates between long and longer end section than fuselage column left and right sides end face width, control stalk pedestal is stuck in from fuselage column front end face the top turning to linking pedestal that column stage casing is connected and fixed lateral support bar upper end backward, control stalk pedestal rear end stretch out two long strip-board shape column connecting arm ends between be connected and fixed by two U-shaped draw-in groove bolt of rear end plates, the control stalk lateral tilting rotating shaft axis hole longitudinally running through block control stalk Connection Block is processed with between the front/rear end of the control stalk Connection Block part of control stalk pedestal front end, before and after this axis hole, the end face of two sections is processed to different shapes, the axis hole end surface shape of control stalk lateral tilting rotating shaft axis hole front section is identical with the rear end end face that the control stalk lateral tilting shaft end left and right sides has two anticreep limiting stoppers, and the left and right sides of the leading portion axis hole of control stalk lateral tilting rotating shaft is processed with the corresponding long recess in the anticreep limiting stopper cross section protruding with two, control stalk lateral tilting rotating shaft rear end, the front segment length of control stalk pedestal front-end control bar lateral tilting rotating shaft axis hole and the polished rod axle in control stalk lateral tilting rotating shaft stage casing isometric, and the hindfoot portion of axis hole, in the position isometric with the polished rod shaft portion in control stalk lateral tilting rotating shaft stage casing, axis hole back segment by with spacing between the protruding anticreep limiting stopper end face outside of control stalk lateral tilting shaft end end face two for diameter, and with the anticreep limiting stopper of control stalk anteversion and retroversion shaft end anticreep termination towards the end face of control stalk anteversion and retroversion rotating shaft front end for plane, be processed into a larger circular shaft bore, a recessed step cutting pattern face is formed between this part circular shaft bore and axis hole leading portion, this recessed step cutting pattern face is used for after the rotating shaft of control stalk lateral tilting is inserted and reversed in addition spacing to the end face towards its annular termination of the protruding anticreep limiting stopper of control stalk lateral tilting shaft end two.

The annular end of control stalk lateral tilting rotating shaft is headfirst inserted in the control stalk lateral tilting rotating shaft axis hole of control stalk pedestal front end face backwards in anticreep termination, because the polished rod axle in control stalk lateral tilting rotating shaft axis hole leading portion and control stalk lateral tilting rotating shaft stage casing is isometric, transition shoulder end face between the annular termination of control stalk lateral tilting rotating shaft and its polished rod axle is close to control stalk pedestal front end face, control stalk lateral tilting rotating shaft stage casing polished rod axle axial plane combines with the control stalk lateral tilting rotating shaft axis hole leading portion inner hole wall of control stalk pedestal, the step cutting pattern face that control stalk lateral tilting shaft end anticreep limiting stopper end face forward can be close to control stalk lateral tilting rotating shaft axis hole back segment recessed is rotated, after in the control stalk lateral tilting rotating shaft axis hole that the rotating shaft of control stalk lateral tilting is inserted into control stalk pedestal front end face, the normal use angle turning 90 degrees and reach its design need be turned round in the annular termination of control stalk lateral tilting rotating shaft front end, and the protruding anticreep limiting stopper of control stalk lateral tilting shaft end two turn round turn 90 degrees after be positioned at the upper and lower of former insertion position, the protruding anticreep limiting stopper of control stalk lateral tilting shaft end two is in by the spacing state in the recessed step cutting pattern face of control stalk lateral tilting rotating shaft axis hole back segment, the work torsional amplitude that the rotating shaft of normality lower control arm lateral tilting only has 8 degree, left and right can be met, and make the rotating shaft of control stalk lateral tilting be unlikely to deviate from the control stalk lateral tilting rotating shaft axis hole of control stalk pedestal front end face, the control stalk anteversion and retroversion rotating shaft axis hole reversing the flat end face central authorities of annular termination, later control stalk lateral tilting rotating shaft front end towards control stalk pedestal both sides and for connecting T-shaped to vert trailing arm by being laterally fit into a bolt as the rotating shaft of control stalk anteversion and retroversion.

The T-shaped trailing arm that verts to be connected with U backward by a two ends and to stretch out downward vertically in the middle of the horizontal trailing arm of pawl and horizontal trailing arm and the control stalk steering shaft be connected forms, the vert control stalk axle of trailing arm of T-shaped becomes T-shaped profile with horizontal trailing arm, vert horizontal trailing arm two ends two U backward of trailing arm of T-shaped connect pawls respectively towards the both sides of fuselage column, T-shaped is verted and is provided with the lateral connection bolt hole of the pull bar lower end spherical plain bearing rod end that verts between the horizontal trailing arm two ends of trailing arm each U connection pawl backward, vert horizontal trailing arm two ends two U backward of trailing arm of T-shaped connect the spacing of pawl and two side direction fuselage columns, two rotor shaft, two U-shapeds verted on arm that lateral direction is stretched out forward of the cantilever that verts from about two clamping plates formula to connect spacing between pawl identical and corresponding up and down, what T-shaped verted that trailing arm two U backward connect respectively by the bolt rotor shaft be connected to above its same side correspondence, pawls vert that U-shaped on arm connects that pawl connects verts on pull bar lower end spherical plain bearing rod end, the vert termination, control stalk steering shaft upper end of trailing arm and horizontal trailing arm mesophase spherule of T-shaped links into an integrated entity, control stalk steering shaft stage casing is processed with one for being installed into the long trough through hole of flat, annular termination in the control stalk lateral tilting rotating shaft being torqued into normal use angle with the form of socket towards fore-and-aft direction, on the wall middle position of the long trough through hole left and right sides, correspondence is processed with one for penetrating by horizontal the axis hole that the rotating shaft of control stalk anteversion and retroversion comes end face center, annular termination in the rotating shaft of connection control bar lateral tilting, the vert control stalk steering shaft hypomere of trailing arm of T-shaped is grouped into by the polished rod shaft portion for inserting control stalk steering bearing and the hypomere tip thread rod part for connection control bar steering bearing captive nut.

The long trough through hole that T-shaped is verted on trailing arm is socketed on the annular termination of control stalk lateral tilting rotating shaft front end, T-shaped vert the control stalk anteversion and retroversion rotating shaft corresponding with on the flat end face in annular termination in the rotating shaft of control stalk lateral tilting of the two side of control stalk steering shaft stage casing long trough through hole of trailing arm axis hole between, after being passed by the bolt shank being used as the rotating shaft of control stalk anteversion and retroversion as, be connected and fixed with the same nut as a control stalk anteversion and retroversion rotating shaft part, T-shaped is verted trailing arm with the downward stateful connection of the threaded end of its control stalk steering shaft hypomere tip in the front of control stalk pedestal.

Because control stalk lateral tilting rotating shaft stage casing intersects vertically as the vert axial line of control stalk anteversion and retroversion rotating shaft that the polished rod axle axial line of faying face and control stalk lateral tilting rotating shaft annular side end face, termination central shaft hole install of left and right, the T-shaped being connected to the front of control stalk pedestal vert trailing arm can vert using the control stalk anteversion and retroversion rotating shaft of its stage casing lateral connection as T-shaped the lateral shaft of trailing arm realize before and after vert, and T-shaped is verted trailing arm can vert using the polished rod axle of control stalk lateral tilting rotating shaft as T-shaped trailing arm longitudinal axis realize left and right vert, being common center of verting as the control stalk lateral tilting rotating shaft of longitudinal axis and the axial line intersection point of flat end face RC control stalk anteversion and retroversion rotating shaft that penetrates longitudinal axis control stalk lateral tilting rotating shaft annular termination as lateral shaft, the T-shaped trailing arm that verts is made to have possessed and realize the function of verting all around for support with control stalk pedestal.

Be connected for the U-shaped control stalk mount pad installed by two control stalk steering bearings and its underpart as the vert control stalk steering shaft part of trailing arm hypomere of T-shaped.

U-shaped control stalk mount pad front appearance is U-shaped, above the bearing seat of the control stalk steering bearing used by vertically-arranged and the bearing seat left and right sides, two protruding corresponding engaging lugs form, the center, bearing seat upper and lower end face of control stalk steering bearing is processed with the mounting hole of the control stalk steering bearing running through upper and lower, control stalk steering bearing mounting hole inwall stage casing is processed with the limited step of the control stalk steering bearing of inside annular protrusion, above the bearing seat both sides of control stalk steering bearing, on two corresponding engaging lugs, correspondence is processed with the axis hole that is installed left control stalk and right control stalk separately, axis hole between two engaging lugs is that concentric is transversely arranged, the all corresponding mounting hole being processed with about two control stalk bolt of rear end plates in both sides before and after the axis hole wall of every side engaging lug, U-shaped control stalk mount pad two engaging lugs are used for the corresponding end installing fixing left control stalk and right control stalk, and use left and right control stalk bolt of rear end plate to be fixed through the end of U-shaped control stalk mount pad two engaging lugs to left control stalk and right control stalk.

Two control stalk steering bearings are installed into the mounting hole of control stalk steering bearing from the two ends up and down of U-shaped control stalk mount pad respectively, between the bearing outside of two control stalk steering bearings, end face is in opposite directions stuck in the both ends of the surface up and down of the limited step of the control stalk steering bearing of the mounting hole stage casing annular protrusion of control stalk steering bearing, after the bearing inner sleeve hole of two control stalk steering bearings is socketed in the control stalk steering shaft hypomere termination that T-shaped verts on trailing arm from bottom to top, the vert threaded end of the control stalk steering shaft hypomere tip on trailing arm of T-shaped stretches out downwards from the bearing inner sleeve hole of two control stalk steering bearings and is fixed by control stalk steering bearing captive nut, U-shaped control stalk mount pad is connected to T-shaped to vert the bottom of trailing arm, axial line between the engaging lug that two, both sides, U-shaped control stalk mount pad upper end are transversely arranged in concentric, contour with the vert axial line of control stalk anteversion and retroversion rotating shaft that trailing arm installs through control stalk lateral tilting rotating shaft annular side end face, termination central shaft hole of T-shaped, two, both sides, U-shaped control stalk mount pad upper end engaging lug and the T-shaped trailing arm that verts is made to have the common center-point that verts all around, and U-shaped control stalk mount pad can vert the downward control stalk steering shaft axle center of trailing arm for left and right center of twist left-right rotation with the T-shaped be attached thereto.

Left control stalk and right control stalk are the control stalk of two the body shape symmetries be arranged in engaging lug corresponding above U-shaped control stalk mount pad both sides, left control stalk and right control stalk rear end curve inwardly with arc level, left control stalk and right control stalk rear end tip all have and corresponding left and right control stalk bolt of rear end plate mounting hole on U-shaped control stalk mount pad engaging lug, left control stalk and right control stalk front end extend forward and lean out, left control stalk and right control stalk front end are respectively connected a handle bar bent respectively to front lower place, side, wherein the handle bar of right control stalk front end be provided with control engine speed can constant speed throttle, the handle bar upper end of left control stalk front end raises up on the termination of stretching out, with the form be arranged above and below, the hollow bracing wire adjusting screw(rod) of two terminations towards left control stalk front is housed, the hollow bracing wire adjusting screw(rod) that the handle bar upper end top position being positioned at left control stalk front end is installed is as brake transition bracing wire adjusting bolt, the hollow bracing wire adjusting screw(rod) that the handle bar upper end lower position being positioned at left control stalk front end is installed is as displacement bracing wire adjusting bolt, the wisp mounting groove waiting the U-shaped of brachium dual control wisp for being connected and fixed is stretched out before the handle bar stage casing of left control stalk front end is provided with one, the bolt connecting hole that a correspondence such as to be connected and fixed at the brachium dual control wisp is provided with between U-shaped wisp mounting groove both sides.

On the lever that brachium dual control wisp is the brachiums such as two ends, on conventional handle, wisp controls on the Length discrepancy lever construction basis of bracing wire, the intimate isometric arm of force will be designed to by the wisp part that holds controls with the resistance arm being connected and fixed bracing wire termination as power arm, bolt connecting hole corresponding between the wisp mounting groove both sides of U-shaped is provided with Deng in the middle of brachium dual control wisp, erect in the wisp mounting groove of the U-shaped be installed on the handle bar of left control stalk front end Deng in the middle of brachium dual control wisp with the part of bolt connecting hole, between the bolt connecting hole that brachium dual control wisp is corresponding with the wisp mounting groove both sides of the U-shaped on the handle bar of left control stalk front end, penetrated by a bolt as fulcrum shaft and be connected and fixed,

Using the power arm waiting brachium dual control wisp lower end wisp to control as driver with the form of holds, the handle bar upper end of resistance arm upper end towards left control stalk front end of bracing wire termination is fixed Deng brachium dual control wisp, owing to will connect brake transition bracing wire and displacement bracing wire as resistance arm upper end simultaneously, the transition bracing wire of wherein braking is the connecting stay wire between the brake wisp end head on the brachium dual control wisp upper ends such as connection and one drag two water brake pump, and displacement bracing wire is that the connection pawl of the displacement bracing wire connecting displacement shifting fork bar front end U-shaped is to the connecting stay wire waited between brachium dual control wisp upper end, because it is different that the wisp that during rotary wing changing distance, displacement shifting fork bar reaches the amplitude range of stirring needed for action effect and controls one drag two water brake pump reaches the amplitude range of moving needed for action effect, brake transition bracing wire termination and the displacement bracing wire termination of fixing the resistance arm upper end connection of bracing wire termination Deng brachium dual control wisp are respectively according to the difference of the size of its movable amplitude, be mounted on respectively using the form be arranged above and below and wait the top of termination, brachium dual control wisp upper end and the position of lower end, adjacent top as resistance arm.

Left control stalk and right control stalk are with arc level aduncate rear end tip, corresponding insertion respectively engaging lug axis hole above U-shaped control stalk mount pad both sides, and the mounting hole being each passed through the left and right control stalk bolt of rear end plate of the axis hole wall of U-shaped control stalk mount pad every side engaging lug by left and right control stalk bolt of rear end plate is fixed, left control stalk and right control stalk are separately fixed at above the U-shaped control stalk mount pad left and right sides, be arranged on the tiller grip that left control stalk above the U-shaped control stalk mount pad left and right sides and right control stalk stretch out forward, lay respectively at the front, the left and right sides of operator's saddle, hold with the mode both hands facilitating driver's wing to control motor bike, left control stalk, lateral connection auxiliary control rod between the handle, at its lower end head of two, right control stalk front end.

Wherein left control stalk rear end tip be installed on the left of U-shaped control stalk mount pad engaging lug in before, need first to be inserted by left control stalk rear end tip after of being positioned at below U-shaped control stalk mount pad turn to the long trough connector loop upwards erect on the cantilever termination of connector loop, left control stalk rear end tip loads and installed again in the lateral of engaging lug on the left of U-shaped control stalk mount pad to be fixed.

With the synchronous course changing control of caudal wing shaft spindle arm on the spindle arm of the front steering wheel shaft on front steering wheel shaft and caudal wing shaft during for realizing left control stalk and the operation of right control stalk, as both hands control stalk mechanism control to possess while rotor head part is verted turn to converged functionality turn to connector loop be arranged on below control stalk pedestal on turn on linking pedestal.

Connector loop is turned to be that its fixed end headband has spindle nose mounting hole on the steering shaft that runs through up and down, the horizontal cantilever of the long trough connector loop that free end headband has upwards to erect, its overall side is L-shaped, the annular through-hole of the long trough connector loop turning to the free termination of connector loop upwards to erect is towards side, turn to the annular through-hole insied width of the long trough connector loop of connector loop identical with left control stalk diameter, lower-upper length in the annular through-hole of the long trough connector loop of connector loop is turned to be the several times of left control stalk diameter, connector loop is turned to fix on termination with spindle nose mounting hole on the steering shaft run through up and down, turn to the elongated slot vias direction of the long trough connector loop on connector loop cantilever free end head towards side and vertical with the hole axis direction of spindle nose mounting hole on the steering shaft on fixing termination, turn to connector loop with the fixing termination of spindle nose mounting hole on steering shaft towards the below of the control stalk steering bearing mounting hole of U-shaped control stalk mount pad, the free termination of connector loop connector loop elongated slot through hole is upwards turned to be placed in the outside of U-shaped control stalk mount pad upper left side engaging lug and to be connected with left control stalk after penetrating via left control stalk end, what be connected with left control stalk turns to connector loop with the fixing termination of spindle nose mounting hole on steering shaft down, by with the fixing of spindle nose upper end on steering shaft and be connected to turn to and be connected above pedestal.

Described to turn to combining mechanism to turn to be above connected on pedestal, steering shaft on spindle nose, steering shaft on spindle nose bearing, steering shaft spindle nose under spindle nose bearing spring card, central steering shaft, steering shaft, steering shaft lower shaft head bearing, steering shaft lower shaft head bearing Spring Card, under turn to and be connected pedestal, one drag two water brake pump, column lower end connecting strap, turn to commutation shift fork, turn to commutation shift fork captive nut, front-wheel steering pull bar, empennage to turn to pull bar to form.

On turn to that to be connected Base body by a front end be that the bearing seat of spindle nose bearing on block steering shaft and the level backward that is connected with it are stretched out two inner side ends long strip-board shape column connecting arm in opposite directions and formed, on turn to and be connected pedestal and formed between two long strip-board shape column connecting arms stretching out of level backward and can block fuselage column front end face and left and right end face U-shaped draw-in groove, on turn to two long strip-board shape column connecting arm ends being connected pedestal slightly long and longer than fuselage column left and right sides end face end section between the corresponding connecting bore being processed with two U-shaped draw-in groove bolt of rear end plates, on turn to be connected pedestal be stuck in fuselage column front end face and left and right end face backward, on turn to and be connected between pedestal two long strip-board shape column connecting arm ends, after being connected by U-shaped draw-in groove bolt of rear end plate by turn to and be connected pedestal and be fixed on the below of control stalk pedestal on fuselage column, on turn to the back being connected the front end face of pedestal and being close to operator's saddle oil tank type backrest top, on turn to be connected pedestal front end steering shaft on the front end surface of spindle nose bearing seat be provided with the bolt connecting hole corresponding with operator's saddle oil tank type backrest top and linked together by bolt and operator's saddle.

On turn to be connected pedestal front end steering shaft on the front end of bearing seat of spindle nose bearing run through the mounting hole being processed with spindle nose bearing on a steering shaft up and down, on steering shaft, the mounting hole upper port of spindle nose bearing is processed with the draw-in groove of spindle nose bearing spring card on steering shaft and lower port is provided with the limited step of spindle nose bearing outer shaft lower surface on steering shaft, above turns to be connected pedestal front end and to be each side provided with the U-shaped engaging lug that is used for being connected and fixed by penetrating bolt the lateral support bar upper end of the fuselage column left and right sides.

On the bearing seat that on steering shaft, spindle nose bearing is arranged on spindle nose bearing on the steering shaft that turns to and be connected pedestal front end from top to bottom on the steering shaft installed spindle nose bearing mounting hole in, on the steering shaft that on steering shaft, the outer face upper surface of the outer bearing sleeve of spindle nose bearing is installed in the mounting hole upper port draw-in groove of spindle nose bearing on steering shaft by, spindle nose bearing spring card is in addition spacing.

On steering shaft, spindle nose is one and erects the hollow tubular that uses and centre is processed with the double end polished rod axle of annular protrusion limited step, its upper end tubular shafts is upwards inserted into and turns to connector loop with being fixed by bolt lateral connection in the termination of spindle nose mounting hole on steering shaft, on steering shaft, the lower end of spindle nose is inserted downwards and stretches out spindle nose bearing internal axle sleeve on steering shaft, in addition spacing to spindle nose bearing internal axle sleeve upper surface on steering shaft by the annular stop step on steering shaft in the middle of spindle nose, be horizontally through the two by bolt and be fixedly connected with in the central steering shaft upper port that the end portion that on steering shaft, spindle nose stretches out spindle nose bearing internal axle sleeve on steering shaft is downwards inserted into the hollow tubular that one, below is erect, central authorities steering shaft as one its upper end is connected turn to the left control stalk penetrated in connector loop about reverse strength by the transition axis be delivered to above fuselage column below fuselage column, central authorities' steering shaft lower port is fixed on down to turn to by being connected with spindle nose under a steering shaft and is connected above pedestal.

The T-shaped of spindle nose entirety in horizontal side under steering shaft, the double end polished rod vertical shaft of raised annular limited step is processed in the stage casing used by a setting and the annular stop step midway location of projection forms to the flat commutation shifting fork bar stretching out a polished rod of side transverse direction, laterally be fixed together by bolt after the upper spindle nose end that under steering shaft, spindle nose is erect upwards inserts central steering shaft lower port, the lower shaft head end that under steering shaft, spindle nose is erect is for installing downwards in the steering shaft lower shaft head bearing inner sleeve being inserted in down and turning to and be connected and pedestal is installed.

Under turn to be connected pedestal by a bearing seat being processed with vertical steering shaft lower shaft head bearing mounting hole and one through two engaging lugs corresponding to left and right below bearing seat and the transverse axis stretched out to both sides form, under turn to and be connected the left and right sides, pedestal rear and be provided with and fix with two panels fuselage column lower end connecting strap and be connected the bolt hole of use, and be bolted and be fixed between fuselage column lower end connecting strap.

Under turn to the lower port of the mounting hole of the steering shaft lower shaft head bearing be connected on pedestal to be provided with steering shaft lower shaft head bearing outer shaft lower surface limited step and upper port is processed with the draw-in groove of steering shaft lower shaft head bearing Spring Card, when the mounting hole of steering shaft lower shaft head bearing is after being fit into steering shaft lower shaft head bearing, the draw-in groove in the mounting hole of steering shaft lower shaft head bearing is installed into by a steering shaft lower shaft head bearing Spring Card, in addition spacing to the outer shaft upper surface of steering shaft lower shaft head bearing, be connected to the commutation shifting fork bar that spindle nose under the steering shaft of central steering shaft lower port crosses out with it to put towards left side, and the termination, bottom of spindle nose under steering shaft is arranged on downwards in the internal axle sleeve hole of steering shaft lower shaft head bearing.

Under turn to and be connected the transverse axis that both sides, direction are stretched out under pedestal and be used for respectively brake transition bracing wire is installed, one drag two water brake pump and turn to commutation shift fork, under turn to be connected spindle nose end that pedestal lower right stretches out be equipped with one settle forward for installing the hollow bracing wire adjusting screw(rod) regulating brake transition bracing wire, under turn to be connected stretch out to the left below pedestal be one and turn to commutation declutch shift shaft, the root of commutation declutch shift shaft is turned to be provided with the mounting interface of one drag two water brake pump forward, commutation declutch shift shaft stage casing is turned to be polished rod axial plane, commutation declutch shift shaft end is outwardly turned to be processed into thread rod.

Turn to commutation shift fork and one drag two water brake pump to be all arranged on down and turn to turning to of the bearing seat lower left being connected pedestal to commutate on declutch shift shaft.

Wherein one drag two water brake pump is the brake wisp oil pump that a conventional atv motorcycle right hand handle uses and the water brake master cylinder that simultaneously can be controlled two water brakes pincers by shunt oil pipe, its mounting interface is mounted on down backward and turns to the bearing seat lower left being connected pedestal to turn on the mounting interface of the root one drag two water brake pump forward of commutation declutch shift shaft, the brake wisp end of one drag two water brake pump is towards the front of right side fuselage column bottom, as oil pump lever brake wisp end head be arranged on down turn to the bearing seat lower right being connected pedestal to stretch out spindle nose on the hollow bracing wire adjusting screw(rod) of brake transition bracing wire installed corresponding, brake wisp end head be processed with the connection end of a brake transition bracing wire and be connected by the termination that brake transition bracing wire is corresponding with waiting brachium dual control wisp upper end.

Turn to commutation shift fork to be that a setting uses and be arranged on down the strip shape bipitch connecting rod turned on commutation declutch shift shaft turning to and be connected pedestal lower left from the side, turn to commutation middle, shift fork side have turn to commutation declutch shift shaft mounting hole and two ends be processed with towards fore-and-aft direction U-shaped connect pawl, turn to commutation shift fork upper end to be provided with a width near the position of U-shaped connection pawl to be enough to insert the long trough convergence hole that steering shaft lower shaft centriciput laterally puts down the commutation shifting fork bar termination of stretching out, this long trough convergence hole is broadened gradually by Inside To Outside and forms certain taper, turn to commutation shift fork on turning to commutation shift fork axis hole and long trough convergence hole perforate direction identical.

Turn to commutation shift fork by its middle have turn to commutation shift fork axis hole ecto-entad to be arranged on down to turn to be connected pedestal lower left turn on the polished rod axle of commutation declutch shift shaft stage casing while, turn to the long trough convergence hole on commutation shift fork also ecto-entad installation sleeve be connected on down on the commutation shifting fork bar crossed out to the left of spindle nose under the steering shaft turning to and be connected and install above pedestal, under turn to the commutation declutch shift shaft end thread termination that turns to being connected pedestal lower left turning to that commutation shift fork axis hole is to the left to be stretched out and by turning to the shift fork captive nut that commutates to be fixed from turning in the middle of commutation shift fork.

Be arranged on down and turn to the U-shaped of side direction in commutation shift fork two ends that turns to be connected on the left of pedestal to connect the front and back end of U-lag gap towards fuselage of pawl, turn to the upper end U-shaped of commutation shift fork connect pawl and steering front wheel axially left side stretch out steering front wheel axle steer arm between be bolted the front-wheel steering pull bar that self two ends is provided with shaft-like oscillating bearing, the empennage being provided with shaft-like oscillating bearing by being bolted self two ends between the caudal wing shaft spindle arm turning to the lower end U-shaped connection pawl of commutation shift fork and caudal wing shaft to stretch out to the left turns to pull bar.

Useful good effect of the present invention:

1 single manual cyclogyro of the present invention, in conjunction with two-wheel power vehicle driving habit in people's daily life, for the driving demand of cyclogyro, adopts full Non-follow control, greatly reduces the driving difficulty grasping cyclogyro.

2 single manual cyclogyros of the present invention adopt variable-distance propeller hub control mechanism, utilize oscillating bearing can bear larger radial weight and its spherical joint inner sleeve can make the characteristic that inclination aligning by a relatively large margin rotates in the oscillating bearing overcoat with Internal Spherical Surface, simplify conventional variable apart from the structure of propeller hub and control mechanism and weight.

3 single manual cyclogyros of the present invention adopt the synchro control of brake and displacement, make the rotor that can braking state kept simultaneously to reduce the angle of attack in operating, under pusher propeller wake flow brushes effect, rotor can enter spin rotating speed with low resistance and the low lift-to-drag ratios angle of attack quickly, shorten taking off of ground run distance, and in cyclogyro descent, while making rotor can reduce lift instantaneously, therefore contact surface between the tire that quick acquisition is larger and earth's surface also produces and larger grabs ground friction force, under braking action, enter halted state as early as possible simultaneously, reach and shorten the time of cyclogyro landing run and the object of distance.

The Air Reverse application force that 4 single manual cyclogyros of the present invention produce when being and overcoming and reduce screw propeller forward traveling, and devise the reverse balance auxiliary device of a set of screw propeller, the antagonistic force centered by prop shaft when balancing and cut down propeller works, fuselage produced, greatly strengthen stationarity that complete machine self rises and falls simultaneously, the driver that is more convenient for easily controls.

Accompanying drawing explanation

Fig. 1 is the complete machine schematic appearance under driving condition of the present invention

Fig. 2 is the major part schematic layout pattern of fuselage sections of the present invention

Fig. 3 is the fuselage main bracket structure schematic diagram of fuselage sections of the present invention

Fig. 4 is 3 framework type independence shock-absorbing support schematic diagrams with propeller reaction thrust balancing device of fuselage sections of the present invention

Fig. 5 is that the propeller reaction thrust balancing device structure of fuselage sections of the present invention uses principle schematic

Fig. 6 is the structure composition schematic diagram of clamping plate type propeller hub mechanism of the present invention and rotor shaft body structure portion

Fig. 7 is after clamping plate type propeller hub mechanism of the present invention is connected with rotor shaft agent structure, the schematic diagram be connected with all parts of rotor connection part

Fig. 8 verts the composition schematic diagram of base holder portion structure and displacement return mechanism in the vert left and right of structure division of rotor shaft cantilever of the present invention

Fig. 9 is that the vert left and right of structure division of rotor shaft cantilever of the present invention is verted after base holder portion structure and displacement return mechanism combine, the schematic diagram be connected with all parts of anteversion and retroversion rotation mechanism

Figure 10 is the operating diagram that verts after rotor head mechanism of the present invention and rotor shaft cantilever inclining rotary mechanism combine

Figure 11 is the both hands control stalk mechanism section of the full manual mechanism of the present invention and turns to the structure of combining mechanism part to form schematic diagram

Figure 12 is that the wisp such as dual control such as brachium such as grade of the both hands control stalk mechanism section of the full manual mechanism of the present invention is to rotor variable pitch contro l schematic diagram

Figure 13 is that the wisp such as dual control such as brachium such as grade of the both hands control stalk mechanism section of the full manual mechanism of the present invention is to the control principle schematic diagram of one drag two water brake pump

Figure 14 is the both hands control stalk mechanism section of the full manual mechanism of the present invention and turns to the linking of combining mechanism part to control schematic diagram

In figure, the sequence number of all parts is:

1 2 3 and 4 liang dashboard before the post column 5 6 back rest 7 dashboard engine bracket beam support beams before 8 9 10 11 pusher propeller engines support column 12 arm length, such as dual control small turned to 13 14 15 can be turned to the reversing shift fork connecting ring constant speed throttle return wheel around 16 17 18 before the front steering wheel steering wheel (front steering wheel steering arm) 19 20 tail tail shaft (tail shaft steering arm) 21 tail wheel 22 rotor rotated push rod 23 24 25 driver's cooling water tank 26 27 balance balance wing wing axis 28 balance wing axis seat before 29 support beam bottom to connect splint splint 30 engine support column bottom 31 double thread rod 32 levels before the support bar rod end joint bearing nut 33 34 level after level support bar support bar around 35 lateral support bar 36 return wheel around 37 support shaft and hydraulic brake clamps around 39 return roller fixed horizontal shaft sleeve nut 40 rotor shaft and rotor shaft and rotor shaft 43 variable pitch axis limit upper lock nut screw 45 variable pitch and variable pitch axis 46 double shaft bottom connection pin shaft rod end joint bearing 48 variable pitch and variable pitch cantilever shaft bearing flange 50 variable pitch and variable pitch axis bearing shaft bearing flange bolt 51 with variable pitch screw rod end joint bearing, 52 fixed nut 53 end on variable pitch axis hub surface under 54 hub surface 55 double row ball bearing 57 variable pitch and variable pitch joint bearing joint bearing liner 58 variable pitch buffer rubber set of 59 Variable pitch buffer rubber 60 sets of shaft rotor with buffer shaft 61 rotor hub surface connection bolt 62 variable pitch screw rotor variable pitch axis 63 63 65 rotor rotor nut variable pitch axis splint 67 66 rotor fixed screw rotor with buffer shaft nut rotated 68 base stents after 69 were rotated base before 70 were rotated around the base plate 71 rotated splint supported screw 72 rotated splint fixed nut screw 73 rotated base plate and rotated base bracket joint bolt 74 tilt rotor tilting shaft collar around 75 76 variable pitch rocker arm 77 variable pitch radial horizontal shaft bushing 78 variable pitch fork rod 79 lateral variable pitch spline shaft 80 lateral variable pitch axis fixed nut 81 variable pitch reset tension spring 82 variable pitch reset tension spring spacing limit shaft sleeve 83 variable pitch rocker arm 84 pin shaft with arrows to adjust base rotated around the base of the splint connection bolt 85 rotor shaft rotated arm 86 rotor axis transverse axis middle spline 87 rotor shaft rotated arm fixed nut rotated around 88 plate type cantilever around 89 rotated cantilever retaining bolt around 90 after rotated cantilever end brace around 91 after rotated cantilever end brace connection bolt 92 lever base 93 u-shaped card slot fixed bolt 94 control rod around a shaft 95 control rod tilt rotor before and after 96 t pour to pass on a task arm 97 u-shaped control lever installed 98 control rod steering bearing 99 control rod steering bearings fixed nut about 100 left lever 101 right control lever 102 control rod fixed bolt 103 yi tuo 2 hydraulic brake pump 104 brake transition pull 105 variable pitch pull 106 to ring on the central steering shaft 108 107 to cohesion base on the steering shaft axis 109 head 110 head on the steering shaft axis bearing of 111 head on the steering shaft axis bearing retainer of 112 under the steering shaft axis under the first 113 steering shaft axis head bearing 114 steering shaft axis bearing retainer of 115 to join a pedestal pillar bottom connection piece of 117 to 116 the reversing shift fork 118 turned to the reversing shift fork fixed nut 119 front wheel steering push rod 120 tail to push rod 121 auxiliary control rod

Detailed description of the invention

Embodiment one: as Fig. 1, shown in Fig. 2, the single manual cyclogyro of the present invention is by fuselage sections, rotor shaft cantilever verts structure, full manual mechanism and possess inner variable-distance rotor head mechanism composition, adopt positive 3 the alighting gear fuselages of high center of gravity, adopt wheel flutter in dead ahead, empennage is rearmounted, operator's saddle and driving engine are placed in column front and back respectively, using pusher propeller as power, 3 framework type independence shock-absorbing support mechanisms with propeller reaction thrust balancing device carry out the antagonistic force that when symmetric screw propeller works, air produces fuselage, strengthen the smoothness that rises and falls of complete machine self, the full manual mechanism of converged functionality is turned to enable driver as controlling the rotary wing changing distance completed motor bike cyclogyro by possessing, rotor shaft is verted, dogled, the full manual mode operation of brake.

As shown in Figure 2, be positioned at column 1 upper end of fuselage central authorities for installing rotor head mechanism, rotor shaft cantilever inclining rotary mechanism, full manual mechanism, the T-shaped connecting two pull bar 23 lower ends that vert trailing arm 96 lower end of verting is connected and installed with a U-shaped control stalk mount pad 97, be arranged on the tiller grip that the left control stalk 100 above U-shaped control stalk mount pad 97 left and right sides stretches out forward with right control stalk 101, lay respectively at the front, the left and right sides of operator's saddle 25, hold with the mode both hands facilitating driver's wing to control motor bike, lateral connection auxiliary control rod 121 between the handle, at its lower end head that left control stalk 100 and right control stalk 101 stretch out forward, wherein right control stalk 101 front end handle bar can be used for controlling the rotating speed of pusher propeller 10 that driving engine 9 drives by constant speed throttle 15, the control of wisp such as dual control such as brachium such as grade 12 for braking to rotor 22 displacement and left and right support wheel 16 of left control stalk 100 front end, left control stalk 100, the auxiliary control rod 121 of lateral connection between two the handle, at its lower end heads in right control stalk 101 front end, when can make to occur temporary needs in driver's normal flight, only middle to keep flight attitude at auxiliary control rod 121 with any grasped, operator's saddle 25 and be placed in column 1 front and back respectively using major diameter pusher propeller 10 backward as the driving engine 9 of power, the lateral support point position of lateral support bar 35 is higher, lateral support bar 35 towards the upper end decoupling rod top of inner side engaging lug connect be supported on fuselage column 1 is connected with operator's saddle 25 fuel tank backrest upper end on turn to the U-shaped being connected pedestal 108 both sides to connect on pawl, be in equal height bottom operator's saddle 25 and driving engine 9 and lay respectively at the front and back of column 1, radiator-water box 24 is fastened on the top turning to and be connected pedestal 108 rear end, driving engine 9 is placed on the engine bed beam 7 that stretches out at column 1 rear, flight gauge panel 5 is installed in gauge panel column 4 upper end, stage casing, front-axle beam 2 front end of front end test, the full dynamic formula empennage 22 of connection above the caudal wing shaft 20 that the back rest 6 follower head is installed, the tailplane on empennage 22 top and the center of thrust line of pusher propeller 10 contour, the central steering shaft 107 turning to connector loop 106 lower end to connect being socketed in left control stalk 100 rear end turns to linking pedestal 108 to extend to below fuselage as a long steering shaft erect from above, what side direction was installed turns to the termination up and down of commutation shift fork 117 to connect front-wheel steering pull bar 119 respectively and empennage turns to pull bar 120.

Embodiment two: as shown in Fig. 3, Fig. 4, Fig. 5, the fuselage sections of the single manual cyclogyro of the present embodiment forms primarily of fuselage main support and 3 framework type independence shock-absorbing support mechanism two parts with propeller reaction thrust balancing device,

As shown in Figure 3, fuselage main support adopts positive 3 the alighting gear fuselages of high center of gravity, adopt and settle a steering front wheel 17 in dead ahead, by both sides, middle part by presylvian fissure strut 33, rear horizontal support bar 34, 3 framework type independence shock-absorbing support mechanisms that lateral support bar 35 and left and right support wheel 16 form are as lateral support, lateral support bar 35 support and connection of its both sides on top position, column 1 stage casing on turn to and be connected pedestal 108 both sides, column 1 occupies fuselage central authorities and erects and omit hypsokinesis, its upper end is for installing rotor head mechanism, rotor shaft cantilever inclining rotary mechanism, full manual mechanism, column 1 lower end turns to the column lower end connecting strap 116 of the bolt connecting hole being connected pedestal 115 to be connected on the back rest 6 front end position more rearward with clamping plate form under being had by two pieces of front ends, column 1 stage casing upper position, be connected and fixed forward the front-axle beam 2 of a test forward, be fixedly connected with the engine bed beam 7 of a level backward, connected by a motor support column 11 erect between the fuselage back rest 6 stage casing of engine bed beam 7 rear end and below thereof and support, termination, the back rest 6 front end connects the front support beam 8 that stretches out of oblique upper forward, front support beam 8 upper end by clamping plate connecting strap with to be fixedly connected with in the middle part of front-axle beam 2 and supplemental support front-axle beam 2, a gauge panel column 4 is upwards installed by clamping plate connecting strap in the stage casing, front-axle beam 2 front end of front end test, gauge panel column 4 upper end is for installing flight gauge panel 5, gauge panel column 4 bottom front is horizontally installed with a pedal 3, because the design's body nodal point is higher, it is upper and lower that the front-axle beam 2 front end pedal 3 of test is convenient to driver, front-axle beam 2 front end installs the front steering wheel shaft 18 that a bottom adopts trailing arm type shock-absorbing support downwards, steering front wheel 17 is arranged on the towing arm lower end of front steering wheel shaft 18 bottom, in the middle part of steering front wheel wheel shaft 18, side is provided with the spindle arm of the cantilevered steering front wheel 17 that is stretched out on the left of fuselage, a small-sized support tail wheel 21 is installed with by connecting strap below the back rest 6 follower head, and upwards install one by clamping plate connecting strap and have and stretch out cantilevered spindle arm and self vertically rotating caudal wing shaft 20 to the left.

As shown in Figure 4,3 framework type independence shock-absorbing support mechanisms with propeller reaction thrust balancing device are made up of with different according to screw propeller the hand of rotation on this basis and propeller reaction thrust balancing device being arranged separately in fuselage side 3 framework type independence shock-absorbing support mechanisms with independent shock-absorbing function, front support beam lower end connecting cleat 29 lower end of current support beam 8 lower end and the back rest 6 front end and motor support column lower end connecting cleat 30 lower end be connected with the back rest 6 two side backward under stretch out formation two for installing the clamping plate shape space of balance wing axle bed 28, two balance wing axle beds 28 embed between the clamping plate space of front support beam lower end connecting cleat 29 and motor support column lower end connecting cleat 30 lower end stretching out and being formed respectively with respective two sides, a balance wing axle 27 two terminations penetrate the mounting hole at two balance axle bed 28 centers respectively, be arranged on after between two balance wing axle beds 28 below the back rest 6, balance wing axle bed 28 both sides of installing below front support beam lower end connecting cleat 29 and motor support column lower end connecting cleat 30 are run through respectively from the side by two double-threaded screw bars 31, after the threaded portion of two double-threaded screw bar 31 terminations is protruding through the both sides of two balance wing axle beds 28, be connected with the spherical plain bearing rod end nut 32 of two horizontal support bars of the same side respectively and fixed, nut 32 top, the rod end joint ball-and-socket joint centre hole of two horizontal support bars becomes two horizontal connecting hole of the bikini framework bottom of every side, it is presylvian fissure strut 33 that left and right supports wheel shaft 37, rear horizontal support bar 34, the common connection strong point of lateral support bar 35 termination toward the outer side, left and right supports wheel shaft 37 and is connected by penetrating in rear horizontal support bar 34 tubulose termination outwardly towards fuselage inner opposite end polished rod spindle nose, left and right supports the spindle nose of wheel shaft 37 one end toward the outer side through after the left and right support wheel 36 possessing brake disc wheel hub, fixed by left and right support wheel captive nut 39, left and right supports the stage casing of wheel shaft 37 to be possessed and is respectively used to be connected presylvian fissure strut 33 and lateral support bar 35 engaging lug toward the outer side with the U-shaped engaging lug of two upward forward, left and right supports the water brake pincers 38 that wheel shaft 37 connection pawl is towards the rear used for fixing left and right support wheel 36, the presylvian fissure strut 33 of the both sides of fuselage column 1 both sides and rear horizontal support bar 34 are connected pawl towards the U-shaped of inner side and are connected as bikini framework lower horizontal connecting bore with nut 32 top, the rod end joint ball-and-socket joint centre hole of two horizontal support bars below the fuselage back rest 6 both sides front end and stage casing respectively by bolt, lateral support bar 35 towards the engaging lug on the upper end decoupling rod top of inner side connect be supported on fuselage column 1 on turn to the U-shaped being connected pedestal 108 both sides to connect on pawl, presylvian fissure strut 33, rear horizontal support bar 34 and lateral support bar 35 termination toward the outer side are all fastened on left and right and support on wheel shaft 37, form 3 framework type independence shock-absorbing support mechanisms with independent shock-absorbing function.

For the opposition centered by the oar axle of pusher propeller 10 that balance and abatement pusher propeller 10 operation produce, design with the addition of the propeller reaction thrust balancing device be made up of a leg-of-mutton balance wing 26, balance wing 26 is one piece of triangular fibre aerofoil, its principal plane and balance wing axle 27, presylvian fissure strut 33, the level triangle frame area that rear horizontal support bar 34 is formed is identical, three limits of triangle aerofoil are processed to hollow sleeve tubular, can as required corresponding be enclosed within any side of fuselage by balance wing axle 27, presylvian fissure strut 33, on the triangle horizontal frame that rear horizontal support 34 bar is formed, form a leg-of-mutton horizontal aerofoil.

As shown in Figure 5, according to the difference of pusher propeller 10 hand of rotation, balance wing 26 is arranged on and pusher propeller 10 hand of rotation opposite side, with the dead ahead that single manual cyclogyro head steering front wheel 17 is complete machine, what be equipped with when driving engine 9 is the pusher propeller 10 of levoform, the namely pusher propeller 10 of left-hand revolution to the right on the left of fuselage, then balance wing 26 is placed on the left of fuselage, because pusher propeller 10 is left-hand revolution operation from left to right, air squeese pressure N can be given when rotating acting in pusher propeller 10 oar face, air can give pusher propeller 10 1 antagonistic force F, this force reaction power F can be delivered on the fuselage of single manual cyclogyro by the oar axle of pusher propeller 10, fuselage can be made centered by the oar axle of pusher propeller 10 by right side, cw to occur left vert, and cover on the left of fuselage by balance wing axle 27, presylvian fissure strut 33, the balance wing 26 covered in the triangle frame that rear horizontal support bar 34 is formed is positioned at the front lower place, left side of pusher propeller 10, when pusher propeller 10 operation, large quantity of air flows through rapidly from the top airfoil of balance wing 26, produce stronger wall attachment effect, the top airfoil of balance wing 26 can be made to form a negative high voltage region, balance wing 26 lower aerofoil do not affected by pusher propeller 10 working air current then forms a barotropic field, certain lift can be produced thus lift whole leg-of-mutton aerofoil and raise up, this lift raised up is delivered to close to column 1 upper end turning to the U-shaped be connected on the left of pedestal 108 connect on pawl by lateral support bar 35 top, and on passing through, turn to linking pedestal 108 to be delivered on column 1, because the strong point of lateral support bar 35 upper end is near fuselage column 1 upper end, far above the oar axle center height of driving engine 9 and pusher propeller 10, what balance wing 26 produced under wall attachment effect raise up, and lift is delivered to column 1 upper part by lateral support bar 35 upper end, left side, and form the thrust of side direction from left to right above a column 1, for balancing and cut down the antagonistic force from right to left centered by the oar axle of pusher propeller 10 that pusher propeller 10 operation produces fuselage, simultaneously pusher propeller 10 operation produces to balance wing 26 upper surface the auxiliary lifting that wall attachment effect produces simultaneously, because balance wing 26 is placed near body nodal point, this auxiliary lifting can not fuselage state of flight to this single manual cyclogyro time center of gravity produce larger negative effect, even if under single manual cyclogyro is in rotation glide descent state after driving engine 9 in-flight failure, because balance wing 26 is horizontal setting, area is little, just can produce stronger wall attachment effect when pusher propeller 10 works, after pusher propeller 10 is because of the stopping of driving engine 9 fault, the unfavorable windage that balance wing 26 causes complete machine in natural tobogganing process is also less.

Embodiment three: as shown in Fig. 6, Fig. 7, the rotor head mechanism of the single manual cyclogyro of the present embodiment by possessing the clamping plate type propeller hub mechanism of inner variable-distance and rotor shaft agent structure, rotor connection part three part forms.

As shown in Figure 6, upper propeller hub face 53 and lower propeller hub face 54 are two symmetrical strip shape clamping plate, the two periphery is provided with bolt connecting hole corresponding to each other, the two center is processed with the mounting hole of a double-range ball bearing vertically run through 55, centered by the mounting hole of double-range ball bearing 55, along upper propeller hub face 53 with lower propeller hub face 54 towards on the line of centers of each termination, each correspondence be processed with a mounting hole vertically running through propeller hub face 53 and the displacement oscillating bearing 56 of end face outside in lower propeller hub face 54 and one near termination, the rectangle elongated hole that displacement cushions gum cover 58 is installed, the mounting hole of each displacement oscillating bearing 56 is for installing an oscillating bearing as displacement oscillating bearing 56, the upper propeller hub face 53 cushioning the rectangle elongated hole of gum cover 58 for installing displacement in upper propeller hub face 53 and lower propeller hub face 54 on two ends position is processed to inclined-plane with the outer face in lower propeller hub face 54 to end portion, upper propeller hub face 53 and lower propeller hub face 54 near each corresponding rectangle elongated hole in two ends position in inner side in conjunction with end face being respectively processed with in two rectangular edges in double-row bearing 55 mounting hole and external end head direction two recessed mounting grooves, when upper propeller hub face 53 is connected to become a complete propeller hub shell with the inner side binding end in lower propeller hub face 54 in the face of detaining installation, the groove of these correspondences just defines one by one independently axle head location and installation hole, this rectangle elongated hole is used for being installed into two displacement cushion compound sleeves 59 having penetrated polished rod shape side by side towards the form in upper propeller hub face 53 and two ends direction, lower propeller hub face 54 and the displacement retaining certain interval to each other cushions gum cover 58 and one erects vertical folder and be contained in the displacement that two displacements that level arranged side by side installs cushion between gum cover 58 gap and wave buffer shaft 60.

Displacement oscillating bearing 56 is arranged on double-range ball bearing 55 both sides using radial direction as Impact direction, the two-port up and down of trepanning each opposed installation displacement oscillating bearing inner covering 57 in each displacement oscillating bearing 56 spherical joint, displacement oscillating bearing inner covering 57 is the outside round sleeve being provided with protruding annular stop step, one end that two displacement oscillating bearing inner coverings 57 are slightly thin and displacement oscillating bearing 56 inner sleeve endoporus equal diameter, two displacement oscillating bearing inner coverings 57 are respectively from the spherical joint inner sleeve of the two ends opposed insertion displacement oscillating bearing 56 of displacement oscillating bearing 56 spherical inner sleeve endoporus, the limited step of displacement oscillating bearing inner covering 56 outer face is stuck on two ports of displacement oscillating bearing 56 spherical joint inner sleeve endoporus, displacement oscillating bearing inner covering 57 endoporus is used for penetrating rotor pitch change axes 63, the thicker external end head end face of displacement oscillating bearing inner covering 57 two is for supporting rotor clamping plate 65.

Rotor pitch change axes 63 and rotary wing changing are a nut through the bolt shank the two linked together while the displacement oscillating bearing inner covering 57 in rotor clamping plate 65 and displacement oscillating bearing 56 endoporus and coupling thereof apart from spindle nut 64.

Displacement buffering gum cover 58 is limit and cushion the circular tube shaped rubber coating that rotor 22 waves shimmy amplitude, displacement buffering gum cover 58 diameter be greater than propeller hub face 53 be combined with lower propeller hub face 54 external end head after thickness, but displacement buffering gum cover 58 diameter is slightly less than spacing between the thicker external end head end face of displacement oscillating bearing inner covering 57 two in the spherical joint inner sleeve of two opposed insertion displacement oscillating bearings 56, the displacement cushion compound sleeve 59 being slightly longer than the polished rod shape axial plane of displacement buffering gum cover 58 by one in two end face center holes of its tubular penetrates and outside two ends, stretches out two spindle noses,

The displacement that after upper propeller hub face 53 is combined with lower propeller hub face 54, two penetrate displacement cushion compound sleeve 59 on each side head cushion gum cover 58 and is arranged in the rectangle elongated hole that upper propeller hub face 53 is combined with lower propeller hub face 54 on each side head afterwards side by side, two spindle noses of the displacement cushion compound sleeve 59 stretched out outside each displacement buffering gum cover 58 two ends, upper propeller hub face 53 and lower propeller hub face 54 in conjunction with time embed recessed mounting groove corresponding to two ends rectangle elongated hole two rectangular edges in conjunction with time the axle head location and installation hole that formed in.

The round sleeve of to be thick and face, termination, curved recessed two ends, a stage casing be plane that rotor waves buffer shaft 60 and one penetrate the double-threaded screw bar composition of axle sleeve, and rotor is waved between the Flat-end of axle sleeve two ends, buffer shaft 60 stage casing and is arranged between displacement oscillating bearing inner covering 57 two the external end head end faces in displacement oscillating bearing 56 contour.

Rotor is waved in the gap that the curved recessed part in buffer shaft 60 round sleeve stage casing is installed between two displacement buffering gum covers 58 arranged side by side, rotor waves the end face outside of double-threaded screw bar two ends towards upper propeller hub face 53 with lower propeller hub face 54 that buffer shaft 60 center penetrates axle sleeve, the upper and lower end face that rotor waves round sleeve two terminations in buffer shaft 60 stage casing is plane, use for supporting rotor clamping plate 65, the double-threaded screw bar that the round sleeve center that rotor waves buffer shaft 60 stage casing penetrates is supported and fixed between rotor clamping plate 65 for the round sleeve connection of rotor being waved buffer shaft 60.

Upper propeller hub face and lower propeller hub face are installed in the face of detaining by the inner side binding end of upper propeller hub face 53 with lower propeller hub face 54, and installed by the face of the propeller hub up and down link bolt hole that upper propeller hub face 53 is corresponding with lower propeller hub face 54 periphery and penetrate upper and lower propeller hub face tie bolt 61 and fixed, double-range ball bearing 55, displacement oscillating bearing 56, displacement buffering gum cover 58, displacement cushion compound sleeve 59, rotor are waved buffer shaft 60 and be arranged on wherein, forms the clamping plate type propeller hub that can connect two panels rotor 22.

Rotor shaft 40 is a rotor shaft in inversion T-shaped outward appearance, rotor shaft 40 main body forms by by the vertical shaft of a hollow and the vertical shaft root lateral shaft that both sides are stretched out to the left and right, the vertical shaft upper end of rotor shaft 40 is the cylindrical vertical shaft erectting extension upward, rotor shaft 40 lower end main shaft root is thicker bulk four prismatic, between former and later two roots of main shaft root, inclined-plane is processed in lower surface, aft end face is slightly long and to downward-extension, main shaft root front/rear end upper end is processed with a pre-and post perforative caging bolt hole near circular vertical shaft root place, face, main side, two sides, left and right is plane, center, face, main side, left and right respectively to left and right separately level stretch out a lateral shaft, two lateral shafts are segmented from inside to outside and are processed in step-like tapered three parts, light over glaze body is divided near a lateral shaft root part and center section part, lateral shaft stage casing light over glaze body divides the spline being processed with tiltedly below rotor shaft lateral shaft spline 86 forward, the outwardly directed end section of lateral shaft is processed with screw thread.

Four parts are from bottom to top processed in the outside of the vertical shaft part for rotor shaft 40 that rotor shaft 40 4 prismatic main shaft root upwards extends, close main shaft root one section is polished rod axial plane, middle part is processed with the limited step of the double-range ball bearing 55 of an evagination, double-range ball bearing 55 limited step is upwards processed with the bearing installation position of the double-range ball bearing 55 in one section of light face, the bearing installation position vertical shaft top end part upwards of double-range ball bearing 55 omits thin and is processed with outside thread, the installation axle hole of the pitch change axes 44 processing hollow light face circle is run through up and down from vertical shaft operative tip to main shaft root bottom, the circular shaft bore being wherein positioned at main shaft root portion is slightly thick, and with upwards in the junction of the circular shaft bore portion U-shaped that is processed into interior pitch change axes 44 lower end be connected the mounting limit step of the upper surface of pawl,

Pitch change axes 44 is a middle part main shaft is polished rod axle, the U-shaped that bottom is processed with down connects pawl, top is the installation position of the pitch change axes bearing 48 being threaded rod end head and erects the axle used, bottom it, be divided into U-shaped to top connect pawl, main shaft polished rod axial plane, three, the installation position part of pitch change axes bearing 48, U-shaped connects pawl, main shaft polished rod axial plane, two steps processed between the installation position of pitch change axes bearing 48 are divided in tapered three parts, it is step-like transition between boundary bottom polished rod axle that U-shaped connects in the middle part of upper end, radix unguis portion and slightly thin pitch change axes 44, the lower end of its main shaft polished rod shaft portion connects the axle root place of pawl transition shoulder near its U-shaped, with U-shaped connect two connecting bores corresponding on pawl towards in the position of 90 degree of angles, be processed with an elongate in shape along a pitch change axes above-below direction pre-and post perforative spacing hole corresponding near the caging bolt hole at circular vertical shaft root place with rotor shaft 40 main shaft root front/rear end upper end, main shaft polished rod axle both sides axial plane is processed with an oil resevoir from top to down separately, step between the installation position of top pitch change axes bearing 48 and main shaft polished rod axial plane is the mounting limit step of pitch change axes bearing 48 inner sleeve lower port, polished rod shaft portion above pitch change axes bearing 48 mounting limit step is the installation site of pitch change axes bearing 48 inner sleeve, top is slightly thin thread rod.

Two connection pawls that U-shaped connection pawl in pitch change axes 44 takes the shape of the letter U down, bottom pitch change axes 44, U-shaped down connects between two connecting bores corresponding on pawl, be installed into a spherical plain bearing rod end nut and dock with a spherical plain bearing rod end bolt upper end forming displacement double end spherical plain bearing rod end 46, by penetrate one to be connected the isometric pitch change axes lower end connecting pins axle 45 of connecting bore olo on pawl with the U-shaped of pitch change axes 44 while, also through the upper end bearing hole connecting double end spherical plain bearing rod end 46 upper end of the displacement two connecting bores corresponding on pawl at U-shaped, displacement is connected with double end spherical plain bearing rod end 46 upper end and is suspended on pitch change axes 44 lower end U-shaped and connects two that pawl takes the shape of the letter U and connect between pawls.

Pitch change axes 44 upper end penetrates in pitch change axes 44 mounting hole in the rotor shaft 40 in inverted T-shaped from bottom to top, pitch change axes 44 bottom U-shaped connect radix unguis portion bottom upper surface and pitch change axes 44 main shaft between transition shoulder spacing by the limited step of the U-shaped pawl of the pitch change axes 44 in rotor shaft 40 main shaft root, connecting pins axle 45 two ends, pitch change axes lower end that pitch change axes 40 lower end U-shaped connects between pawl are spacing by rotor shaft 40 main shaft root circular shaft bore inwall, load the pitch change axes 44 main shaft polished rod axial plane part of rotor shaft 40 inside and U-shaped connect the lower port of pre-and post perforative strip shape spacing hole between the step-like root of pawl and rotor shaft 40 main shaft root front/rear end upper end corresponding near pre-and post perforative caging bolt hole, circular vertical shaft root place, and the strip spacing hole lower port penetrated by pitch change axes Limit screw 43 in the pitch change axes 44 in face, rotor shaft 40 rear and front end and rotor shaft 40 adds pitch change axes 44 in case turn round and move up and down the spacing of amplitude, pitch change axes Limit screw 43 makes to penetrate pitch change axes 44 in rotor shaft 40 and can not twist, and make the limited field of pitch change axes 44 using the spacing between the upper and lower port of the strip spacing hole on it as its upper and lower displacement movement, loading the transverse axis center that on the pitch change axes 44 lower end U-shaped connection pawl in the middle of rotor shaft 40, two corresponding connecting bore centers and rotor shaft 40 main shaft root extend towards the left and right sides is that concentric arranges, connect the U-shaped being suspended on pitch change axes 44 and to connect between pawl that the other end of double end spherical plain bearing rod end 46 is sagging stretches out rotor shaft 40 bottom.

The installation position part axis body penetrating the pitch change axes bearing 48 on pitch change axes 44 top of rotor shaft 40 from bottom to top stretches out for connection displacement cantilever 47 from rotor shaft 40 upper end.

The horizontal axle sleeve 41 of rotor shaft is the round sleeve that two termination external process have raised annular limited step, the horizontal endoporus of axle sleeve 41 of rotor shaft is identical near the light over glaze diameter of main shaft root portion with the lateral shaft of rotor shaft 40 both sides of inverted T-shaped, is socketed on the lateral shaft of inverted T-shaped rotor shaft 40 both sides towards the mode inside rotor shaft 40 main shaft root with the horizontal axle sleeve 41 bottom protrusion annular stop step one end of rotor shaft.

The combination of rotor shaft 40 main body and clamping plate type propeller hub is protruded upward from trepanning in the double-range ball bearing 55 at clamping plate type propeller hub center by the screwed upper end of its vertical shaft part by rotor shaft 40, the limited step of the double-range ball bearing 55 in rotor shaft 40 is by spacing towards lower port for double-range ball bearing 55 inner sleeve at clamping plate type propeller hub center, rotor shaft 40 vertical shaft stretches out the double-range ball bearing 55 inner sleeve threaded end upwards at clamping plate type propeller hub center, double-range ball bearing 55 inner sleeve upper port is fixed by rotor shaft upper end locking nut 42, the clamping plate type propeller hub of rotor shaft 40 with fixing double-range ball bearing 55 is linked together.

In rotor shaft 40, protrude upward the termination, installation position of the pitch change axes 44 upper end pitch change axes bearing 48 at rotor shaft 40 top, be used for being connected with displacement cantilever 47.

Displacement cantilever 47 is that the symmetry below two skew backs that has of a horizontal use stretches out two rotary wing changings apart from cantilever, the cantilever termination of stretching out to both sides is processed with downward tapped bore, the bolt hole of two cantilever terminations at right angle setting displacement spherical plain bearing rod end screw rod 51 from bottom to top separately, centre between its two cantilevers is the bearing seat being provided with pitch change axes bearing 48 mounting hole, pitch change axes bearing 48 mounting hole periphery has the bolt connecting hole of pitch change axes bearing flange 49, pitch change axes bearing 48 mounting hole lower port has the limited step of pitch change axes bearing 48 overcoat lower port, after a pitch change axes bearing 48 is fit into the mounting hole of the pitch change axes bearing 48 in displacement cantilever 47 centre, from the top of displacement cantilever 47 center pitch change axes bearing 48 mounting hole, a pitch change axes bearing flange 49 is installed, pitch change axes bearing flange 49 is connected and fixed by pitch change axes bearing flange tie bolt 50, the upper port of pitch change axes bearing 48 overcoat is fixed in the bearing seat of the pitch change axes bearing 48 at displacement cantilever 47 center, pitch change axes bearing 48 inner sleeve being arranged on displacement cantilever 47 centre is socketed in pitch change axes 44 from the top down and stretches out on pitch change axes bearing 48 installation position of the upper end of rotor shaft 40, pitch change axes bearing 48 inner sleeve lower port is spacing by the step between pitch change axes bearing 48 installation position on pitch change axes 44 top and the main shaft polished rod axle of pitch change axes 44, after the slightly thin thread rod in pitch change axes 44 top stretches out pitch change axes bearing 48 inner sleeve upper port, after being locked by pitch change axes upper end captive nut 52, the cantilever termination that two of displacement cantilever 47 are provided with displacement spherical plain bearing rod end screw rod 51 is respectively towards the front, oblique side of displacement oscillating bearing 56 position on clamping plate type propeller hub to stretching out.

As shown in Figure 7, rotor clamping plate 65 are one group of horizontal use with two pieces and the L-shaped strip shape connecting cleat of main body outward appearance, for to the lateral connection between the upper and lower end face of each termination of clamping plate type propeller hub and the upper and lower end face of rotor 22, every group leader's bar shaped clamping plate are corresponding on the rear end vertical bar shaped end face connecting rotor 22 is processed with the bolt mounting holes connecting rotor 22, often organize front end that rotor clamping plate 65 strip shape end face is used for clamping plate type propeller hub except possessing the rotor pitch change axes 63 corresponding with clamping plate type propeller hub and rotor and wave the installation axle hole of buffer shaft 67 two-thread screw, and have the correspondence of face toward the outer side extend one less of installing the strip connecting arm of a rotary wing changing apart from pole socket 62.

Rotary wing changing apart from pole socket 62 for main body be strip and block, the strip connecting arm area that main body upper and lower end face area and rotor clamping plate 65 extend laterally is suitable, its height and rotor waves buffer shaft 60 stage casing axle sleeve two ends Flat-end and the spacing that is arranged between displacement oscillating bearing inner covering 57 two the external end head end faces in displacement oscillating bearing 56 is contour, and upper and lower end face is processed with the corresponding bolt connecting hole of the strip connecting arm of organizing rotor clamping plate 65 with each and is bolted to be supported on often to be organized between strip connecting arm corresponding on rotor clamping plate 65, at rotary wing changing apart from pole socket 62 end face centre toward the outer side, there is the whorl brace rod of the displacement spherical plain bearing rod end screw rod 51 for being mounted on displacement cantilever 47 termination stretched out outside Xiang Yigen.

Being combined through of clamping plate type propeller hub and rotor 22 connection part correspondingly in the upper and lower end face of each termination of clamping plate type propeller hub is installed one group of rotor clamping plate 65 and is connected, often organize two pieces in the upper and lower being arranged on the upper and lower end face of clamping plate type propeller hub termination between rotor clamping plate 65 front end be arranged above and below respectively, often organizing the mounting hole of the rotor pitch change axes 63 on rotor clamping plate 65 front end and rotor, to wave the mounting hole of buffer shaft 60 corresponding with the axis hole that the mounting hole of the rotor pitch change axes 63 on the every one end of clamping plate type propeller hub and rotor wave round sleeve two ends, buffer shaft 60 stage casing, the spindle nose that each rotor waves the double-threaded screw bar axle of buffer shaft 60 waves axle sleeve two ends, buffer shaft 60 stage casing through the rotor that the every one end of clamping plate type propeller hub rotor clamping plate 65 is installed and the threaded shank portion of double-threaded screw bar spindle nose two ends is stretched out from often organizing rotor clamping plate 65 end face and down upward, then wave buffer shaft nut 67 by rotor to be connected and fixed.

Often organize the rotor being all subject to every one end of clamping plate type propeller hub of rotary wing changing distance pole socket 62 and correspondence thereof is installed between rotor clamping plate 65 to wave buffer shaft 60 stage casing axle sleeve two ends Flat-end and be arranged on the common support of displacement oscillating bearing inner covering 57 two the external end head end faces in displacement oscillating bearing 56.

Mounting hole as the rotor pitch change axes 63 of bolt shank from the upper surface rotor clamping plate 65 being positioned at clamping plate type propeller hub of rotor pitch change axes 63 penetrates, through two displacement oscillating bearing inner coverings 57 opposed in trepanning in displacement oscillating bearing 56 in clamping plate type propeller hub, the rotary wing changing of bolt shank lower end from the lower surface rotor clamping plate 65 being positioned at clamping plate type propeller hub as rotor pitch change axes 63 passes apart from axis hole, and is fixed apart from spindle nut 64 by rotary wing changing.

Apart from pole socket 62, end-face helical pipe link termination is corresponding toward the outer side to the rotary wing changing between the ball-and-socket joint endoporus of sagging two displacement spherical plain bearing rod end screw rod 51 lower ends, front, the clamping plate type propeller hub oblique side strip connecting arm corresponding with being fixed on two panels rotor clamping plate 65 to be arranged on displacement cantilever 47 two ends, rotary wing changing after stretching out, and to be fixed apart from pole socket 62 threaded shank portion of nut to the ball-and-socket joint bore section stretching out displacement spherical plain bearing rod end screw rod 51 lower end that whorl brace rod termination is mated toward the outer side by rotary wing changing through the ball-and-socket joint endoporus being arranged on two displacement spherical plain bearing rod end screw rod 51 lower ends sagging to its front upper place, side, displacement cantilever 47 two ends end-face helical pipe link termination toward the outer side apart from pole socket 62.

Two panels rotor 22 with the corresponding two sides being up and down arranged on rotor 22 of end face of rotor tie bolt mounting hole, and after being connected and fixed by rotor check screw 66, is linked together with clamping plate type propeller hub two terminations by rotor clamping plate 65 rear end respectively.

What clamping plate type propeller hub mechanism adopted is that rotor pitch change axes 63 is erect longitudinal, the radial direction of the displacement oscillating bearing 56 between above propeller hub face 53 and lower propeller hub face 54 is as Impact direction, while utilizing oscillating bearing can bear larger radial weight, its spherical joint inner sleeve can make the characteristic that inclination aligning by a relatively large margin rotates in the oscillating bearing overcoat with Internal Spherical Surface, the rotor pitch change axes 63 of displacement oscillating bearing 56 in propeller hub is inserted with the horizontal centrifugal tension born when rotor works of the two ends of its connection rotor clamping plate 65 to erect attitude, make the spherical joint inner sleeve tilt slide amplitude in the displacement oscillating bearing 56 of arrangement like this can meet the demand that rotor pitch change axes about 63 is waved and lateral tilting transformation distance is movable simultaneously, rotor wave the curved recessed part in buffer shaft 60 round sleeve stage casing be installed in two, each termination of clamping plate type propeller hub arranged side by side displacement buffering gum cover 58 between gap in, rotor is waved buffer shaft 60 and is utilized the curved recessed part in its round sleeve stage casing to wave and in side shake process, displacement arranged side by side with two, its both sides all the time cushions gum cover 58 and keeps the contact of squash type and realize rotor about 22 by the contact of squash type waving and the buffering of side shake at rotor about 22.

Embodiment four: as shown in Fig. 8, Fig. 9, Figure 10, the rotor shaft cantilever of the single manual cyclogyro of the present embodiment structure of verting is made up of vert base holder portion, displacement return mechanism, anteversion and retroversion rotation mechanism three part of left and right.

As shown in Figure 8, vert lateral tilting rotating shaft 74 main body of base holder portion of left and right is two concentrics are stretched out at polished rod spindle nose from the block and center, face, rear and front end of horizontal oblong to two ends, the width of gap ratio fuselage column 1 front/rear end between lateral tilting rotating shaft 74 left and right sides end face is slightly wide, the side end face, two, left and right of lateral tilting rotating shaft 74 is all processed with the bolt hole and a sunk coak laterally processed that are connected with the cantilever 88 that verts about clamping plate type, the outside face of the polished rod spindle nose of lateral tilting rotating shaft 74 is socketed with termination, one end external process separately and becomes raised annular limited step and center is processed with the lateral tilting rotating shaft axle sleeve 75 with the polished rod spindle nose equal diameter centre hole of lateral tilting rotating shaft 74, lateral tilting rotating shaft axle sleeve 75 is socketed in the left and right of stretching out at center, face, lateral tilting rotating shaft 74 rear and front end with one end of protruding limited step towards the form in face, lateral tilting rotating shaft 74 rear and front end and verts on polished rod spindle nose, be socketed in the protruding limited step of lateral tilting rotating shaft axle sleeve 75 on the polished rod spindle nose of lateral tilting rotating shaft 74 towards front and back outer face between spacing between spacing with fuselage column 1 front/rear end identical

The pedestal front frame 68 that verts is that two pieces of upper ends are semicircular end and centered by the center of circle of semicircular end-face, are processed with the mounting hole of lateral tilting rotating shaft axle sleeve 75 with the pedestal after poppet 69 that verts, the strip shape plate that the pedestal front frame 68 that verts is identical with the left and right spacing width of fuselage column 1 front/rear end with pedestal after poppet 69 lower end width that verts, vert on pedestal front frame 68 semicircular end-face forward bar shaped plate end face once and the pedestal after poppet 69 semicircular end-face backwards bar shaped plate end face once that verts and be processed to long recess, vert pedestal front frame 68 end face forward and vert in the recess sidewall of pedestal after poppet 69 end face backwards, correspondence is processed with the tie bolt mounting hole of the pedestal left and right clamping plate 70 that vert,

The pedestal front frame 68 that verts one in front and one in back is placed on the front/rear end on fuselage column 1 top with the pedestal after poppet 69 that verts, the pedestal front frame 68 that verts stretches out upper surface, fuselage column 1 top with the upper end semicircular end part of the pedestal after poppet 69 that verts, vert pedestal front frame 68 and the mounting hole of the lateral tilting rotating shaft axle sleeve 75 of upper end semicircular end part between pedestal after poppet 69 that verts be concentric arrange and two spindle noses two ends being socketed with the lateral tilting rotating shaft 74 of lateral tilting rotating shaft axle sleeve 75 be installed into vert pedestal front frame 68 with vert in the mounting hole of the lateral tilting rotating shaft axle sleeve 75 in the semicircular end of pedestal after poppet 69 upper end, lateral tilting rotating shaft 74 is connected and is supported on above vert pedestal front frame 68 and the fuselage column 1 that verts between pedestal after poppet 69.

The pedestal left and right clamping plate 70 that vert are two pieces of connecting cleats with the symmetry towards back boom, on the right opposed left and right end face being arranged on fuselage column 1 top of one the first from left, vert clamping plate 70 front end, pedestal left and right and middle part surface is processed with and the pedestal front frame 68 that verts be placed on the front/rear end on fuselage column 1 top, vert the corresponding tie bolt mounting hole in pedestal after poppet 69 side, a cantilever with the mounting hole of distance-variable rocker arm lateral shaft lining 77 and the pedestal left and right clamping plate 70 that vert extend back, the vert cantilever follower head position of pedestal left and right clamping plate 70 is processed with the mounting hole of the clamping plate studdle 71 that verts.

The clamping plate studdle 71 that verts is the double-threaded screw bars of two two ends with limited support step, the clamping plate studdle 71 two ends limited support step that verts is identical with the width of the distance between left and right of fuselage column 1 front/rear end, vert clamping plate studdle 71 two ends thread rod for penetrate that the pedestal left and right clamping plate 70 that vert stretch out backward two cantilever terminations on the mounting hole of the clamping plate studdle 71 that verts, clamping plate studdle 71 two ends of verting are supported verting between pedestal left and right clamping plate 70 two cantilever terminations backward with limited support step, pedestal left and right clamping plate 70 end face outside of verting is stretched out in the vert thread rod termination of clamping plate studdle 71, and fixed by the captive nut 72 of the clamping plate studdle that verts.

Vert pedestal front frame 68, vert pedestal after poppet 69, to vert between pedestal left and right clamping plate 70 and can be connected to each other to square frame shape by vert pedestal left and right clamping plate and the tie bolt 73 of the base seat support that verts and be fixed on fuselage column 1 top all around on four end faces, vert after the front end that has the pedestal left and right clamping plate tie bolt 84 that verts of bracing wire adjusting base concurrently by one between the bolt hole corresponding with bottommost on the pedestal left and right clamping plate 70 that vert of both sides, pedestal front frame 68 front end face recess sidewall bottom is inserted to the right on the left of fuselage column 1 and be connected and fixed, the follower head having the pedestal left and right clamping plate tie bolt 84 that verts of bracing wire adjusting base concurrently is thicker, thereafter termination by under a hollow bracing wire adjusting screw(rod) is installed upward.

To vert between the bolt hole corresponding with bottommost on the pedestal left and right clamping plate 70 that vert of both sides, pedestal after poppet 69 aft end face recess sidewall bottom when penetrating the pedestal left and right clamping plate that vert and being connected with the tie bolt 73 of the base seat support that verts, it is the displacement reset tension spring spacing limit shaft sleeve 82 of hollow thin-wall pipe spreader by a main body, be placed in and vert between the bolt hole of pedestal after poppet 69 groove bottom on two sidewalls, displacement reset tension spring spacing limit shaft sleeve 82 two ends and vert between pedestal after poppet 69 groove two sidewalls and keep certain interval, this gap is for installing the lower end of two two ends with the displacement reset tension spring 81 of loop-hook, and fixed spacing to the loop-hook of displacement reset tension spring 81 lower end.

The pedestal front frame 68 that verts, the pedestal after poppet 69 that verts, vert and be connected to each other with the tie bolt 73 of base seat support of verting by the pedestal left and right clamping plate that vert between pedestal left and right clamping plate 70 while, also displacement return mechanism is installed be connected to vert pedestal left and right clamping plate 70 and stretch out backward two cantilever terminations on.

The distance-variable rocker arm 76 of displacement return mechanism is the double end rocking arm of a horizontal use, a rectangular through holes is processed with between rocking arm main body upper and lower end face, rocking arm main body is made to form a strip shape square frame, for being mounted on double end spherical plain bearing rod end 46 lower end of pitch change axes 44 lower end in the way to insert in the strip shape square frame of this hollow, distance-variable rocker arm 76 using strip shape square frame both sides strip plate face as rocking arm end face, the follower head in distance-variable rocker arm 76 strip plate face and midway location respectively have two to stretch out circular lateral shaft to both sides correspondence level, the slightly thin lateral shaft in distance-variable rocker arm 76 follower head position is crossed strip resetting shaft, two spindle noses of crossed strip resetting shaft run through the strip plate surface rear end head left and right sides of strip shape square frame both sides, spindle nose end is respectively processed with a ring annular groove.

Annular groove in crossed strip resetting shaft two ends on distance-variable rocker arm 76 is used for the upper end of mounting two two ends with the displacement reset tension spring 81 of loop-hook, and fixes spacing to the loop-hook of two displacement reset tension spring 81 upper ends.

What outside two strip plate faces of the strip shape square frame distance-variable rocker arm 76, middle part was stretched out to both sides is horizontal pitch change axes, horizontal pitch change axes root is slightly thick, main body is polished rod axle, shaft end is comparatively thin and be processed with screw thread, thinner shaft end and thicker root are processed with transition shoulder, the polished rod shaft portion of the horizontal pitch change axes on the left of the strip shape square frame wherein on distance-variable rocker arm 76 compares the horizontal pitch change axes slightly length of opposite side, it compares the slightly longer part polished rod axle of the horizontal pitch change axes of opposite side towards on the surface of front end, be processed with one for being connected and fixed the installation groove of the horizontal pitch change axes spline 79 of displacement shifting fork bar 78, near the front of horizontal pitch change axes position on two strip plate faces of distance-variable rocker arm 76 strip shape square frame, correspondence is processed with the mounting hole of the distance-variable rocker arm pin axle 83 that is connected for the double end spherical plain bearing rod end 46 lower end ball-and-socket joint axis hole of same pitch change axes lower end connecting pins axle 45 connection.

When the lower end of the double end spherical plain bearing rod end 46 lower end ball-and-socket joint of pitch change axes 44 lower end connection stretches out below rotor shaft 40, after in the strip shape square frame of reeve distance-variable rocker arm 76 hollow, by the distance-variable rocker arm pin axle 83 of the two ends length polished rod axial plane identical with the spacing of the strip shape square frame lateral surface of distance-variable rocker arm 76 hollow while the strip plate face, strip shape square frame both sides through distance-variable rocker arm 76 hollow, also simultaneously through double end spherical plain bearing rod end 46 lower end axis hole and connect in the strip shape square frame being fixed on distance-variable rocker arm 76 hollow.

Distance-variable rocker arm lateral shaft lining 77 is that two bottoms are with protruding outer ring step and the isodiametric round sleeve of horizontal pitch change axes polished rod axle of interior axis hole and distance-variable rocker arm 76 both sides, the distance-variable rocker arm lateral shaft lining 77 length horizontal pitch change axes polished rod partial-length shorter with distance-variable rocker arm 76 is identical, distance-variable rocker arm lateral shaft lining 77 is socketed in the horizontal pitch change axes of stretching out to both sides in the middle of distance-variable rocker arm 76 in its protruding outer ring step mode to the inside, bottom it, ring-shaped step termination is to the inside close on the strip shape square frame outer wall of distance-variable rocker arm 76 hollow, distance-variable rocker arm pin axle 83 two ends through spherical hole, double end spherical plain bearing rod end 46 lower end are limited in the strip shape square frame of distance-variable rocker arm 76 hollow, distance-variable rocker arm lateral shaft lining 77 towards both sides ring-shaped step outer face between spacing and the both sides of fuselage column 1 front/rear end width identical, distance-variable rocker arm lateral shaft lining 77 towards the external end head of both sides end face between spacing be arranged on the fuselage column 1 end face left and right sides vert pedestal left and right clamping plate 70 towards outside end face between width spaces identical.

When verting, pedestal left and right clamping plate 70 correspondence is arranged on the left and right end face on fuselage column 1 top, with the pedestal front frame 68 that verts, when the pedestal after poppet 69 that verts links into an integrated entity, distance-variable rocker arm 76 with its one end with crossed strip resetting shaft backwards and overall horizontal form is installed between two cantilevers that two pieces of pedestal left and right clamping plate 70 that vert extend to fuselage column 1 rear, in the middle of distance-variable rocker arm 76, two are socketed with the horizontal pitch change axes spindle nose end of distance-variable rocker arm lateral shaft lining 77, protruding from the mounting hole of two pieces of distance-variable rocker arm lateral shaft linings 77 pedestal left and right clamping plate 70 cantilever backwards that vert respectively.

Distance-variable rocker arm 76 defines two Length discrepancy lever arm of force that the horizontal pitch change axes being mounted on the pedestal left and right clamping plate that vert 70 with distance-variable rocker arm 76 both sides is a dot center between two spindle noses of crossed strip resetting shaft and the distance-variable rocker arm pin axle 83 near horizontal pitch change axes front position.

Distance-variable rocker arm lateral shaft lining 77 outer face that distance-variable rocker arm 76 both sides are socketed in horizontal pitch change axes flushes with the pedestal left and right clamping plate outer face that verts after penetrating the distance-variable rocker arm lateral shaft bush hole of verting on clamping plate 70 cantilever of pedestal left and right, longer this one end polished rod shaft portion of horizontal pitch change axes on the left of distance-variable rocker arm 76, after stretching out pedestal left and right clamping plate 70 outer face that verts, to be arranged in displacement shifting fork bar 78 termination of installing from the left-external side of the pedestal left and right clamping plate 70 that vert in axis hole in the way to insert.

The loop-hook of two displacement reset tension spring 81 lower ends is connected to pedestal after poppet 69 aft end face groove bottom of verting, two displacement reset tension spring 81 upper end loop-hooks are connected on the crossed strip resetting shaft of distance-variable rocker arm 76 rear end, two displacement reset tension springs 81, under the effect of autogenous shrinkage pulling force, remain distance-variable rocker arm pin axle 83 thrust upwards to connecting double end spherical plain bearing rod end 46 lower end axis hole in distance-variable rocker arm 76.

Displacement shifting fork bar 78 is the cantilever that a left-external side from the pedestal left and right clamping plate 70 that vert is installed, its front end free end headband has the connection pawl of the displacement bracing wire 105 of U-shaped, termination side straps is fixed in rear end has the axis hole identical with the polished rod axle external diameter of horizontal pitch change axes longer on the left of distance-variable rocker arm 76 and the installation groove accordingly with horizontal pitch change axes spline 79 forward, displacement shifting fork bar 78 with the free termination of connection pawl of the displacement bracing wire 105 of U-shaped towards fuselage column 1 front, connect spacing horizontal pitch change axes spline 79 as radial direction to insert displacement shifting fork bar 78 rear end and fix in spline groove corresponding between axis hole with horizontal pitch change axes on the left of distance-variable rocker arm 76 in termination.

The horizontal pitch change axes two ends threaded portion of distance-variable rocker arm 76 is stretching out on vert pedestal left and right clamping plate 70 outer face and displacement shifting fork bar 78 after axis hole respectively, fixed respectively by two horizontal pitch change axes captive nuts 80, the displacement shifting fork bar 78 distance-variable rocker arm 76 and outside thereof connected is arranged on the cantilever that two pieces of pedestal left and right clamping plate 70 that vert extend to fuselage column 1 rear in horizontal mode.

Pedestal left and right clamping plate tie bolt 84 root that verts having bracing wire adjusting base concurrently is equipped with one end of hollow bracing wire adjusting screw(rod), the same side being arranged on displacement shifting fork bar 78 is verted on the front lower end of pedestal front frame 68, pedestal left and right clamping plate tie bolt 84 root that verts having bracing wire adjusting base concurrently installs one for regulating the hollow bracing wire adjusting screw(rod) of displacement bracing wire 105 upper end, the hollow bracing wire adjusting screw(rod) centre hole of its bolt root is installed towards the connection pawl of the displacement bracing wire 105 of the U-shaped on displacement shifting fork bar 78, the end of displacement bracing wire 105 is through this hollow bracing wire adjusting screw(rod) centre hole, the displacement bracing wire being connected to the U-shaped on displacement shifting fork bar 78 connects on pawl,

As shown in Figure 9, vert pedestal front frame 68 with vert pedestal after poppet 69 by the connection with the pedestal left and right clamping plate 70 that vert lateral tilting rotating shaft 74 connected be supported on above fuselage column 1 time, lateral tilting rotating shaft 74 is all connected with the cantilever 88 that verts about the bolt hole connected corresponding to the cantilever 88 that verts about clamping plate type and the sunk coak of transverse direction and the clamping plate type of anteversion and retroversion rotation mechanism part by two side end faces about it.

The cantilever 88 that verts about clamping plate type is two pieces of edge-on uses of transverse direction and the oblong strip board of symmetry, the side surface of side surface and lateral tilting rotating shaft main body is between the upper and lower apart from wide, two pieces of strip board front ends are the connection end of lateral tilting rotating shaft 74, except being processed with the bolt connecting hole corresponding with side, lateral tilting rotating shaft 74 main body both sides at side surface on connection end, and on the inner surface corresponded to each other, be processed with the horizontal tenon step that sunk coak horizontal with lateral tilting rotating shaft 74 main body both sides is corresponding and isometric, the side surface middle position center of strip board rear end cantilever is provided with the mounting hole of the horizontal axle sleeve 41 of rotor shaft, and near this termination along mounting hole cross cut end (of a beam) upper-lower position being processed with about two the cantilever rear end bracing frame tie bolts 91 that vert.

The cantilever 88 that verts about clamping plate type is inwardly connected and fixed the two with the form of clamping plate from lateral tilting rotating shaft 74 and rotor shaft 40 both sides, the cantilever 88 that verts about clamping plate type utilizes the horizontal tenon step of its front end connection end inner surface to embed in the horizontal sunk coak in lateral tilting rotating shaft 74 main body both sides, and bolt connecting hole corresponding with side, lateral tilting rotating shaft 74 main body both sides for cantilever 88 front end of verting about clamping plate type is connected and fixed by the cantilever bolt of rear end plate 89 that verts about utilizing, cantilever 88 front end of verting about clamping plate type is mounted on lateral tilting rotating shaft 74 both sides, the left and right sides end distance ratio of the square block-shaped main body of lateral tilting rotating shaft 74 verts pedestal front frame 68, pedestal after poppet 69 end face that verts is slightly wide, the end face part that the cantilever 88 that verts about making the two clamping plates formula be connected with lateral tilting rotating shaft 74 oblong block-shaped main body both sides is downward and vert and keep certain between the end face of pedestal after poppet 69 side left and right and vert gap, this gap makes lateral tilting rotating shaft 74 rear and front end spindle nose distance to bear 8 degree and vert about vert pedestal front frame 68 and pedestal after poppet 69 upper end of verting be realizes centered by the axis hole that arrange of concentric, and the side end face of the end face that the cantilever 88 that verts about driving two clamping plates formula is downward and pedestal after poppet 69 both sides of verting comes in contact, realize verting the spacing of amplitude towards left and right sides to lateral tilting rotating shaft 74.

The cantilever 88 that verts about two clamping plates formula utilizes the mounting hole of the horizontal axle sleeve 41 of the rotor shaft of its rear end central authorities to be socketed in rotor shaft 40 from rotor shaft 40 both sides to stretch out to both sides and be set with the lateral shaft of the horizontal axle sleeve 41 of rotor shaft, annular stop step also identical with the width of lateral tilting rotating shaft 74 front/rear end towards width between end face outside of horizontal axle sleeve 41 projection of rotor shaft on the lateral shaft being arranged on rotor shaft 40 both sides, vert about the outer face of rotor shaft horizontal axle sleeve 41 raised annular limited step supports two clamping plates formula cantilever 88 inner side end, vert after cantilever 88 about the horizontal axle sleeve 41 of rotor shaft penetrates two clamping plates formula, the horizontal axle sleeve 41 of two rotor shaft flushes towards the end face in outside with cantilever 88 outer face that verts about two clamping plates formula,

Two lateral shaft stage casings of rotor shaft 40 are with tiltedly the polished rod shaft portion of the spline of the rotor shaft lateral shaft spline 86 of below and end thread bar part are protruding from the mounting hole of the horizontal axle sleeve 41 of rotor shaft of cantilever 88 rear end central authorities of verting about clamping plate type forward, vert about clamping plate type the left and right of termination, cantilever 88 rear end vert cantilever rear end bracing frame tie bolt 91 mounting hole between, clamp one piece of vertically-arranged and use and vert in the left and right of the square plate bulk identical with lateral tilting rotating shaft 74 front/rear end length and width cantilever rear end bracing frame 90, left and right bracing frame 90 both sides, the cantilever rear end end face that verts is processed with the corresponding bolt connecting hole of the mounting hole of the cantilever rear end bracing frame tie bolt 91 that to vert with cantilever 88 follower head about two that verts about clamping plate type, utilize left and right vert cantilever rear end bracing frame tie bolt 91 is verted in left and right cantilever rear end bracing frame 90 clamp be fixed on clamping plate type about vert between termination, cantilever 88 rear end.

The left and right cantilever rear end bracing frame 90 that verts verts rotor shaft 40 main shaft root aft end face between cantilever 88 about being installed in two clamping plates formula equally, and keep certain gap between rotor shaft 40 root aft end face, this gap is as the spacing gap of amplitude of verting before and after rotor shaft 40, when verting before and after rotor shaft 40, rotor shaft 40 main shaft root aft end face and bottom contact with the end face of cantilever 88 rear end bracing frame towards rotor shaft 40 direction that vert about clamping plate type, and the amplitude of verting before and after rotor shaft 40 is limited between 0 degree ~ 18 degree.

From the external end head part of two lateral shafts of the outwardly directed rotor shaft 40 of mounting hole of the horizontal axle sleeve 41 of the rotor shaft of cantilever 88 rear end central authorities of verting about clamping plate type for and two symmetries be arranged on clamping plate type about the rotor shaft of verting outside cantilever 88 rear end vert between arm 85 and connected.

The rotor shaft arm 85 that verts is two horizontal uses and two the oblique cantilevers of termination not in same plane, the rotor shaft arm 85 rear end fixed end headband that verts has the mounting hole of the lateral shaft in rotor shaft 40, and rotor shaft 40 mounting hole is processed with the groove installing rotor shaft lateral shaft stage casing spline 86 towards direction, free termination, rotor shaft vert arm 85 front end free end headband have U-shaped connect pawl, the rotor shaft of the every side of the cantilever 88 that verts about clamping plate type is verted between the fixing termination of arm 85 with rotor shaft 40 transverse axis mounting hole be connected pawl free termination with U-shaped and is connected each via the connecting arm stretched out sideling to front lateral direction after,

The rotor shaft arm 85 that verts has the fixing termination of the mounting hole of rotor shaft 40 transverse axis backwards, stage casing outside the mounting hole that the mounting hole of rotor shaft 40 lateral shaft rotor shaft verted on arm 85 is socketed in the horizontal axle sleeve 41 of rotor shaft on the cantilever 88 that to vert about rotor shaft 40 lateral shaft stretches out clamping plate type is with forward tiltedly in the polished rod axle of below spline and rotor shaft 40 transverse axis end thread bar part, and by rotor shaft lateral shaft stage casing spline 86 insert from outside to inside the rotor shaft 40 lateral shaft mounting hole spline corresponding with rotor shaft 40 lateral shaft spacing after, the rotor shaft 40 lateral shaft end thread bar part of stretching out the rotor shaft 40 lateral shaft mounting hole that rotor shaft is verted on arm 85 is fixed by the rotor shaft arm captive nut 87 that verts, vert between cantilever 88 about two lateral shaft outer ends of rotor shaft 40 root are fastened on two clamping plates formula,

As shown in Figure 10, the left and right sides end distance ratio of the square block-shaped main body of lateral tilting rotating shaft 74 verts pedestal front frame 68, pedestal after poppet 69 end face that verts is slightly wide, the end face part that the cantilever 88 that verts about making the two clamping plates formula be connected with lateral tilting rotating shaft 74 oblong block-shaped main body both sides is downward and vert and keep certain between the end face of pedestal after poppet 69 side left and right and vert gap, this gap makes lateral tilting rotating shaft 74 rear and front end spindle nose to be realize positive and negative 8 degree of left and right centered by the axis hole that arranges of concentric to vert by vert pedestal front frame 68 and pedestal after poppet 69 upper end of verting, and the side end face of the end face that the cantilever 88 that verts about driving two clamping plates formula is downward and pedestal after poppet 69 both sides of verting comes in contact, realize verting the spacing of amplitude towards left and right sides to lateral tilting rotating shaft 74.

The left and right cantilever rear end bracing frame 90 that verts verts rotor shaft 40 main shaft root aft end face between cantilever 88 about being installed in two clamping plates formula equally, and keep certain gap between rotor shaft 40 root aft end face, this gap is as the spacing gap of amplitude of verting before and after rotor shaft 40, when verting before and after rotor shaft 40, rotor shaft 40 main shaft root aft end face and bottom and the left and right cantilever rear end bracing frame 90 that verts contacts towards the end face in rotor shaft 40 direction, and the amplitude of verting before and after rotor shaft 40 is limited between 0 degree ~ 18 degree.

Vert about clamping plate type cantilever 88 by with lateral tilting rotating shaft 74, rotor shaft 40, vert the connection of cantilever rear end bracing frame 90 in left and right, vert on cantilever 88 cantilever termination backwards about the clamping plate type propeller hub connect rotor shaft 40 and rotor shaft 40 upper end and rotor 22 are fastened on clamping plate type, having of verting about clamping plate type that cantilever 88 front end connects left and right laterally verts that the spindle nose axial line at lateral tilting rotating shaft 74 front/rear end center of function is connected with cantilever 88 rear end of verting about clamping plate type have before and after the central axis of longitudinal lateral shaft in the rotor shaft 40 of function that verts contour and on intermediate point M between the lateral shaft of giving rotor shaft 40 root to stretch out to both sides mutually, under cantilever 88 coupled condition of verting about clamping plate type, verting all around can be realized centered by this axial line intersection point M by laterally vert rotor shaft 40 that function and self both sides lateral shaft have an anteversion and retroversion rotating function of lateral tilting rotating shaft 74.

The U-shaped that the rotor shaft of verting cantilever 88 both sides about being arranged on clamping plate type is verted on free termination, arm 85 front end connects pawl, respectively from two fronts, side direction fuselage column 1 side of the cantilever 88 that verts about two clamping plates formula to stretching out, two rotor shaft, two U-shapeds verted on the free termination of arm 85 connect pawls and vert on the upper end spherical plain bearing rod end of pull bar 23 in front, fuselage column 1 both sides by bolt two of being fastened on fuselage column 1 both sides respectively, the pull bar 23 that verts is two main bodys is the connecting rod of tubulose two ends with spherical plain bearing rod end, pull bar 23 lower end that verts connect full manual mechanism for upper and lower push-and-pull rotor shaft vert arm 85 and drive rotor shaft 40 and connect clamping plate type propeller hub complete action of verting.

Embodiment five: as shown in Figure 11, Figure 12, Figure 13, Figure 14, the full manual mechanism of the single manual cyclogyro of the present embodiment is by both hands control stalk mechanism and turn to combining mechanism to form.

As shown in figure 11, control stalk lateral tilting rotating shaft 94 is by the annular termination be connected, faying face and anticreep termination three part composition are reversed in left and right, annular termination, control stalk lateral tilting rotating shaft 94 front end is the button-head that flat horizontal surface is processed in larger two side end faces, the flat end face center of the annular termination of control stalk lateral tilting rotating shaft 94 is processed with one for installing the axis hole of control stalk anteversion and retroversion rotating shaft 95, control stalk anteversion and retroversion rotating shaft 95 is a horizontal use and is used as bolt shank and the nut thereof of the flat end face center shaft of the annular termination of control stalk lateral tilting rotating shaft 94.

Control stalk lateral tilting rotating shaft 94 stage casing is that to reverse the part of faying face as left and right be one section of polished rod axle, the axial line of polished rod axle axial line and side end face, annular termination central shaft hole intersects vertically, transition shoulder is processed with between annular termination and stage casing polished rod axle, anticreep termination be two from stage casing polished rod shaft end at right angles to the anticreep limiting stopper that bilateral symmetry lateral projection is stretched out, anticreep limiting stopper stretches out direction and becomes 90 degree with the axis hole direction on annular termination to both sides, the stage casing of control stalk lateral tilting rotating shaft 94 and rear end are used for being arranged in control stalk pedestal 92 with the form inserted.

Control stalk pedestal 92 is a pedestal being connected and fixed control stalk lateral tilting rotating shaft 94, its main body is two inner side ends long strip-board shape column connecting arm composition in opposite directions that a block control stalk Connection Block of front end and the rear end level backward that is connected with it are stretched out, formed between the aft end face plane of control stalk Connection Block part and control stalk Connection Block part two long strip-board shape column connecting arms that level is stretched out backward and can block fuselage column 1 front end face and left and right end face U-shaped draw-in groove, two long strip-board shape column connecting arm ends are slightly longer than fuselage column 1 left and right sides end face width, the corresponding connecting bore being processed with two U-shaped draw-in groove bolt of rear end plates 93 between the end section that two long strip-board shape column connecting arms grow than fuselage column left and right sides end face width, control stalk pedestal 92 rear end is connected and fixed and is arranged on fuselage column 1 front end on the position of the backrest type fuel tank back upper place of operator's saddle 25, the U-shaped draw-in groove formed between the aft end face plane of its control stalk Connection Block part and control stalk Connection Block part two long strip-board shape column connecting arms that level is stretched out backward, the top turning to linking pedestal 108 that column 1 stage casing is connected and fixed lateral support bar 35 upper end is stuck in backward from fuselage column 1 front end face, the rear end of control stalk Connection Block part stretch out two long strip-board shape column connecting arm ends on corresponding U-shaped draw-in groove bolt of rear end plate 93 connecting bore between, be connected and fixed by two U-shaped draw-in groove bolt of rear end plates 93.

The axis hole longitudinally running through the control stalk lateral tilting rotating shaft 94 of block control stalk Connection Block is processed with between the front/rear end of the control stalk Connection Block part of control stalk pedestal 92 front end, before and after this axis hole, the end face of two sections is processed to different shapes, the end surface shape of the axis hole front section of control stalk lateral tilting rotating shaft 94 is identical with the rear end end face that the control stalk lateral tilting rotating shaft 94 end left and right sides has two anticreep limiting stoppers, and the left and right sides of the axis hole of control stalk lateral tilting rotating shaft 94 is processed with the corresponding long recess in the anticreep limiting stopper cross section protruding with two, control stalk lateral tilting rotating shaft 94 rear end, the front segment length of the axis hole of control stalk pedestal 92 front-end control bar lateral tilting rotating shaft 94 and the polished rod axle in control stalk lateral tilting rotating shaft 94 stage casing isometric, and the hindfoot portion of axis hole, in the position isometric with the polished rod shaft portion in control stalk lateral tilting rotating shaft 94 stage casing, axis hole back segment by with spacing between the protruding anticreep limiting stopper end face outside of control stalk lateral tilting rotating shaft 94 distal end faces two for diameter, and with the anticreep limiting stopper of control stalk anteversion and retroversion rotating shaft 94 end anticreep termination towards the end face of control stalk anteversion and retroversion rotating shaft 94 front end for plane, be processed into a larger circular shaft bore, a recessed step cutting pattern face is formed between this part circular shaft bore and axis hole leading portion, this recessed step cutting pattern face is used for after control stalk lateral tilting rotating shaft 94 is inserted and reversed in addition spacing to the end face towards its annular termination of the protruding anticreep limiting stopper of control stalk lateral tilting rotating shaft 94 end two.

The annular end of control stalk lateral tilting rotating shaft 94 is headfirst inserted in the axis hole of control stalk lateral tilting rotating shaft 94 of control stalk pedestal 92 front end face backwards in anticreep termination, due to the axis hole leading portion of control stalk lateral tilting rotating shaft 94 and the polished rod axle in control stalk lateral tilting rotating shaft 94 stage casing isometric, transition shoulder end face between the annular termination of control stalk lateral tilting rotating shaft 94 and its polished rod axle is close to control stalk pedestal 92 front end face, control stalk lateral tilting rotating shaft 94 stage casing polished rod axle axial plane combines with the axis hole leading portion inner hole wall of the control stalk lateral tilting rotating shaft 94 of control stalk pedestal 92, the step cutting pattern face that control stalk lateral tilting rotating shaft 94 end anticreep limiting stopper end face forward can be close to the axis hole back segment of control stalk lateral tilting rotating shaft 94 recessed is rotated, after in the axis hole that control stalk lateral tilting rotating shaft 94 is inserted into the control stalk lateral tilting rotating shaft 94 of control stalk pedestal 92 front end face, the annular termination of control stalk lateral tilting rotating shaft 94 front end need turn round turn 90 degrees reach its design apart from normal use angle, and the protruding anticreep limiting stopper of control stalk lateral tilting rotating shaft 94 end two turn round turn 90 degrees after be positioned at the upper and lower of former insertion position, the protruding anticreep limiting stopper of control stalk lateral tilting rotating shaft 94 end two is in by the spacing state in the recessed step cutting pattern face of the axis hole back segment of control stalk lateral tilting rotating shaft 94, the work torsional amplitude that normality lower control arm lateral tilting rotating shaft 94 only has 8 degree, left and right can be met, and make control stalk lateral tilting rotating shaft 94 be unlikely to deviate from the axis hole of the control stalk lateral tilting rotating shaft 94 of control stalk pedestal 92 front end face, the axis hole reversing the control stalk anteversion and retroversion rotating shaft 95 of the flat end face central authorities of annular termination, later control stalk lateral tilting rotating shaft 94 front end towards control stalk pedestal 92 both sides and for connecting T-shaped to vert trailing arm 96 by being laterally fit into a bolt as control stalk anteversion and retroversion rotating shaft 95.

The T-shaped trailing arm 96 that verts to be connected with U backward by a two ends and to stretch out downward vertically in the middle of the horizontal trailing arm of pawl and horizontal trailing arm and the control stalk steering shaft be connected forms, the vert control stalk axle of trailing arm 96 of T-shaped becomes T-shaped profile with horizontal trailing arm, vert horizontal trailing arm two ends two U backward of trailing arm 96 of T-shaped connect pawls respectively towards the both sides of fuselage column, T-shaped is verted and is provided with the lateral connection bolt hole of the pull bar 23 lower end spherical plain bearing rod end that verts between trailing arm 96 horizontal trailing arm two ends each U connection pawl backward, vert horizontal trailing arm two ends two U backward of trailing arm 96 of T-shaped connect the spacing of pawl and two side direction fuselage columns 1, two rotor shaft, two U-shapeds verted on arm 85 that lateral direction is stretched out forward of the cantilever 88 that verts from about two clamping plates formula to connect spacing between pawl identical and corresponding up and down, what T-shaped verted that trailing arm 96 two U backward connect respectively by the bolt rotor shaft be connected to above its same side correspondence, pawls vert that U-shaped on arm 85 connects that pawl connects verts on pull bar 23 lower end spherical plain bearing rod end.

The vert termination, control stalk steering shaft upper end of trailing arm 96 and horizontal trailing arm mesophase spherule of T-shaped links into an integrated entity, control stalk steering shaft stage casing is processed with one for being installed into the long trough through hole of flat, annular termination in control stalk lateral tilting rotating shaft 94 with the form of socket towards fore-and-aft direction, on the wall middle position of the long trough through hole left and right sides, correspondence is processed with one for penetrating by horizontal the axis hole that control stalk anteversion and retroversion rotating shaft 95 comes end face center, annular termination in connection control bar lateral tilting rotating shaft 94, the vert control stalk steering shaft hypomere of trailing arm 96 of T-shaped is grouped into by the polished rod shaft portion for inserting control stalk steering bearing 98 and the hypomere tip thread rod part for connection control bar steering bearing captive nut 99.

Vert control stalk steering shaft stage casing long trough through hole that trailing arm 96 stretches out downwards of T-shaped is socketed in and is inserted into control stalk pedestal 92 front end and is torqued on the annular termination of control stalk lateral tilting rotating shaft 94 front end of normal use angle, T-shaped vert the control stalk anteversion and retroversion rotating shaft 95 corresponding with on the flat end face in annular termination in control stalk lateral tilting rotating shaft 94 of the two side of control stalk steering shaft stage casing long trough through hole of trailing arm 96 axis hole between, after being passed by the bolt shank being used as control stalk anteversion and retroversion rotating shaft 95 as, be connected and fixed with the same nut as control stalk anteversion and retroversion rotating shaft 95 part, T-shaped is verted trailing arm 96 with the downward stateful connection of the threaded end of its control stalk steering shaft hypomere tip in the front of control stalk pedestal 92,

Because control stalk lateral tilting rotating shaft 94 stage casing intersects vertically as the vert axial line of control stalk anteversion and retroversion rotating shaft 95 that the polished rod axle axial line of faying face and control stalk lateral tilting rotating shaft annular side end face, termination central shaft hole install of left and right, the T-shaped being connected to the front of control stalk pedestal 92 vert trailing arm 96 can vert using the control stalk anteversion and retroversion rotating shaft 95 of its stage casing lateral connection as T-shaped the lateral shaft of trailing arm 96 realize before and after vert, and T-shaped is verted trailing arm 96 can vert using the polished rod axle of control stalk lateral tilting rotating shaft 94 as T-shaped trailing arm 96 longitudinal axis realize left and right vert, be common center of verting using the axial line intersection point as the control stalk lateral tilting rotating shaft 94 of longitudinal axis and the flat end face RC control stalk anteversion and retroversion rotating shaft 95 that penetrates the annular termination of longitudinal axis control stalk lateral tilting rotating shaft 94 as lateral shaft, the T-shaped trailing arm 96 that verts is made to have possessed and realize the function of verting all around for support with control stalk pedestal.

Be connected for the U-shaped control stalk mount pad 97 installed by two control stalk steering bearings 98 and its underpart as the vert control stalk steering shaft part of trailing arm 96 hypomere of T-shaped.

U-shaped control stalk mount pad 97 front appearance is U-shaped, above the bearing seat of the control stalk steering bearing 98 used by vertically-arranged and the bearing seat left and right sides, two protruding corresponding engaging lugs form, the center, bearing seat upper and lower end face of control stalk steering bearing 98 is processed with the mounting hole of the control stalk steering bearing 98 running through upper and lower, the mounting hole inwall stage casing of control stalk steering bearing 98 is processed with the limited step of the control stalk steering bearing 98 of inside annular protrusion, above the bearing seat both sides of control stalk steering bearing 98, on two corresponding engaging lugs, correspondence is processed with the axis hole that is installed left control stalk 100 and right control stalk 101 separately, axis hole between two engaging lugs is that concentric is transversely arranged, the all corresponding mounting hole being processed with about two control stalk bolt of rear end plates 102 in both sides before and after the axis hole wall of every side engaging lug, U-shaped control stalk mount pad 97 two engaging lugs are used for the corresponding end installing fixing left control stalk 100 and right control stalk 101, and use left and right control stalk bolt of rear end plate 102, through U-shaped control stalk, the end of 97 two engaging lugs to left control stalk 100 and right control stalk 101 is installed to be fixed

When two control stalk steering bearings 98 are installed into the mounting hole of control stalk steering bearing 98 from the two ends up and down of U-shaped control stalk mount pad 97 respectively, between the bearing outside of two control stalk steering bearings 98, end face is in opposite directions stuck in the both ends of the surface up and down of the limited step of the control stalk steering bearing 98 of the mounting hole stage casing annular protrusion of control stalk steering bearing 98, after the bearing inner sleeve hole of two control stalk steering bearings 98 is socketed in the control stalk steering shaft hypomere termination that T-shaped verts on trailing arm 96 from bottom to top, the vert threaded end of the control stalk steering shaft hypomere tip on trailing arm 96 of T-shaped stretches out downwards from the bearing inner sleeve hole of two control stalk steering bearings 98 and is fixed by control stalk steering bearing captive nut 99, U-shaped control stalk mount pad 97 is connected to T-shaped to vert the bottom of trailing arm 96, be arranged on T-shaped and vert two, the both sides, U-shaped control stalk mount pad 97 upper end of bottom of trailing arm 96 in the axial line between the transversely arranged engaging lug of concentric, contour with the vert axial line of control stalk anteversion and retroversion rotating shaft 95 that trailing arm 96 installs through side end face, control stalk lateral tilting rotating shaft 94 annular termination central shaft hole of T-shaped, U-shaped control stalk mount pad 97 upper end two, both sides engaging lug and the T-shaped trailing arm 96 that verts is made to have the common center-point that verts all around, U-shaped control stalk mount pad 97 not only can forwards, backwards left and right vert, and on this basis, U-shaped control stalk mount pad 97 can also vert by the T-shaped be attached thereto and realize left and right centered by the downward control stalk steering shaft axle center of trailing arm 96 and reverse, in the process reversed, axial line between the engaging lug of two, both sides, U-shaped control stalk mount pad 97 upper end pass with the flat end face center of control stalk lateral tilting rotating shaft 94 and annular termination thereof in twist process the axial line intersection point of control stalk anteversion and retroversion rotating shaft 95 remain consistent.

Left control stalk 100 and right control stalk 101 are for being arranged on the control stalk of two body shape symmetries in engaging lug corresponding above U-shaped control stalk mount pad 97 both sides, left control stalk 100 curves inwardly with arc level with right control stalk 101 rear end, left control stalk 100 and right control stalk 101 rear end tip all have and corresponding left and right control stalk bolt of rear end plate 102 mounting hole on U-shaped control stalk mount pad 97 engaging lug, left control stalk 100 and right control stalk 101 front end extend forward and lean out, left control stalk 100 and right control stalk 101 front end are respectively connected a handle bar bent respectively to front lower place, side, wherein right control stalk 101 front end handle bar for install control engine speed can constant speed throttle 15, what the handle bar of left control stalk 100 front end was used for being connected and fixed waits brachium dual control wisp 12.

Left control stalk 100 and right control stalk 101 are with arc level aduncate rear end tip, corresponding insertion respectively engaging lug axis hole above U-shaped control stalk mount pad 97 both sides, and the mounting hole being each passed through the left and right control stalk bolt of rear end plate 102 of the axis hole wall of U-shaped control stalk mount pad 97 every side engaging lug by left and right control stalk bolt of rear end plate 102 is fixed, left control stalk 100 is separately fixed at above U-shaped control stalk mount pad 97 left and right sides with right control stalk 101, be arranged on the tiller grip that the left control stalk 100 above U-shaped control stalk mount pad 97 left and right sides stretches out forward with right control stalk 101, lay respectively at the front, the left and right sides of operator's saddle 25, (see Fig. 2) is held with the mode both hands facilitating driver's wing to control motor bike.

Wherein left control stalk 100 rear end tip be installed on the left of U-shaped control stalk mount pad 97 engaging lug in before, need first to be inserted by left control stalk 100 rear end tip after of being positioned at below U-shaped control stalk mount pad 97 turn to the long trough connector loop upwards erect on the cantilever termination of connector loop 106, left control stalk 100 rear end tip loads and installed again in the lateral of engaging lug on the left of U-shaped control stalk mount pad 97 to be fixed.

For realize when left control stalk 100 and right control stalk 101 operate with the synchronous course changing control of caudal wing shaft spindle arm on the spindle arm of the front steering wheel shaft 18 on front steering wheel shaft 18 and caudal wing shaft 20, as both hands control stalk mechanism control to possess while rotor head part is verted turn to converged functionality turn to connector loop 106 be arranged on below control stalk pedestal 92 on turn to and be connected on pedestal 108.

Connector loop 106 is turned to be that its fixed end headband has spindle nose mounting hole on the steering shaft that runs through up and down, the horizontal cantilever of the long trough connector loop that free end headband has upwards to erect, its overall side is L-shaped, the annular through-hole of the long trough connector loop turning to the free termination of connector loop 106 upwards to erect is towards side, turn to the annular through-hole insied width of the long trough connector loop of connector loop 106 identical with left control stalk 100 diameter, lower-upper length in the annular through-hole of the long trough connector loop of connector loop 106 is turned to be the several times of left control stalk 100 diameter, with spindle nose 109 mounting hole on the steering shaft run through up and down on the fixing termination turning to connector loop 106, turn to the elongated slot vias direction of the long trough connector loop on connector loop 106 cantilever free end head towards side and vertical with the hole axis direction of spindle nose 109 mounting hole on the steering shaft on fixing termination, turn to connector loop 106 with the fixing termination of spindle nose on steering shaft 109 mounting hole towards the below of the control stalk steering bearing mounting hole of U-shaped control stalk mount pad 97, the free termination of connector loop 106 connector loop elongated slot through hole is upwards turned to be placed in the outside of U-shaped control stalk mount pad 97 upper left side engaging lug and to be connected with left control stalk 100 after penetrating via left control stalk 100 end, what be connected with left control stalk 100 turns to connector loop 106 with the fixing termination of spindle nose 109 mounting hole on steering shaft down, by with the fixing of spindle nose on steering shaft 109 upper end and be connected to turn to and be connected above pedestal 108.

On turn to that to be connected pedestal 108 main body by a front portion be that the bearing seat of spindle nose bearing 110 on block steering shaft and the level backward that is connected with it are stretched out two inner side ends long strip-board shape column connecting arm in opposite directions and formed, on turn to and be connected pedestal 108 and formed between two long strip-board shape column connecting arms stretching out of level backward and can block fuselage column 1 front end face and left and right end face U, shape draw-in groove, on turn to two the long strip-board shape column connecting arm ends being connected pedestal 108 slightly longer than fuselage column 1 left and right sides end face, the corresponding connecting bore being processed with two U-shaped draw-in groove bolt of rear end plates 93 between the end section that two long strip-board shape column connecting arms grow than fuselage column 1 left and right sides end face width, on turn to be connected column connecting arm from pedestal 108 to latter two long strip-board shape between the U-shaped draw-in groove that formed be stuck in fuselage column 1 front end face and left and right end face backward, on turn to the U-shaped draw-in groove bolt of rear end plate 93 be connected on pedestal 108 two long strip-board shape column connecting arm ends slightly longer than fuselage column 1 left and right sides end face connecting bore between, by U-shaped draw-in groove bolt of rear end plate 93 connect after by turn to be connected pedestal 108 be fixed on fuselage column 1, on turn to and be connected pedestal 108 and be arranged on the below of control stalk pedestal 92, on turn to the back being connected the front end face of pedestal 108 and being close to operator's saddle 25 oil tank type backrest top, on turn to be connected pedestal 108 front portion steering shaft on the front end surface of bearing seat of spindle nose bearing 110 be provided with the connecting bore corresponding with operator's saddle 25 oil tank type backrest top, linked together by bolt and operator's saddle 25 for above turning to the front end surface of linking pedestal 108 connecting bore corresponding with operator's saddle 25 oil tank type backrest top.

On turn to be connected pedestal 108 front portion steering shaft on the front end of bearing seat of spindle nose bearing 110 run through the mounting hole being processed with spindle nose bearing 110 on a steering shaft up and down, and the mounting hole upper port of spindle nose bearing 110 is processed with the draw-in groove of spindle nose bearing spring card 111 on steering shaft on steering shaft, on steering shaft, the mounting hole lower port of spindle nose bearing 110 is provided with the limited step of spindle nose bearing 110 outer shaft lower surface on steering shaft, on turn to be connected pedestal 108 front portion steering shaft on the bearing seat of spindle nose bearing 110 be each side provided with the U-shaped engaging lug that is used for being connected and fixed lateral support bar 35 upper end of fuselage column 1 left and right sides, on turn to be connected pedestal 108 front end steering shaft on the U-shaped engaging lug of the bearing seat left and right sides of spindle nose bearing 110 be bolted fixing with lateral support bar 35 upper end of fuselage column 1 left and right sides respectively.

On steering shaft, spindle nose bearing 110 is arranged in the mounting hole of spindle nose bearing 110 on the steering shaft that turns to and be connected pedestal 108 front end from top to bottom, and on the steering shaft that on steering shaft, the outer face upper surface of spindle nose bearing 110 outer bearing sleeve is installed in the mounting hole upper port draw-in groove of spindle nose bearing 110 on steering shaft by, spindle nose bearing spring card 111 is in addition spacing.

On steering shaft, spindle nose 109 is one and erects the hollow tubular that uses and centre is processed with the double end polished rod axle of annular protrusion limited step, its upper end tubular shafts is upwards inserted into and turns to connector loop 106 with being fixed by bolt lateral connection in the termination of spindle nose on steering shaft 109 mounting hole, on steering shaft, the lower end of spindle nose 109 is inserted downwards and stretches out spindle nose bearing 110 internal axle sleeve on steering shaft, in addition spacing to spindle nose bearing internal axle sleeve upper surface on steering shaft by the annular stop step in the middle of spindle nose on steering shaft 109, on steering shaft, spindle nose 109 lower end tubular shafts stretches out the end section of spindle nose bearing 110 internal axle sleeve on steering shaft, on downward insertion steering shaft below spindle nose bearing 110 hollow tubular that is erect central steering shaft 107 upper port in and be horizontally through the two by bolt and be fixedly connected with, central authorities' steering shaft 107 reverses strength by the transition axis be delivered to above fuselage column 1 below fuselage column 1 as the left control stalk about 101 penetrated that turns in connector loop 106 that its upper end connects by, central authorities' steering shaft 107 lower port is fixed on down to turn to by being connected with spindle nose 112 under a steering shaft and is connected above pedestal 115.

The T-shaped of spindle nose 112 entirety in horizontal side under steering shaft, the horizontal flat commutation shifting fork bar stretching out a polished rod of annular stop step midway location erectting the double end polished rod vertical shaft and projection that raised annular limited step is processed in the stage casing used by one forms, laterally be fixed together by bolt after the upper spindle nose end that under steering shaft, spindle nose 112 is erect upwards inserts central steering shaft 107 lower port, the lower shaft head end that under steering shaft, spindle nose 112 is erect is used for downward installation in steering shaft lower shaft head bearing 113 inner sleeve being inserted in down and turning to and be connected and pedestal 115 is installed.

Under turn to be connected pedestal 115 be a bearing seat being arranged on fuselage column 1 bottom front face, main body by a bearing seat being processed with the mounting hole of the steering shaft lower shaft head bearing 113 run through up and down and one through two engaging lugs corresponding to left and right below bearing seat and the transverse axis stretched out to both sides form, under turn to and be connected the left and right sides, pedestal 115 rear and be provided with fixing with two panels fuselage column lower end connecting strap 116 and be connected the bolt hole used, and be bolted and be fixed between fuselage column lower end connecting strap 116.

Under turn to the lower port of the mounting hole of the steering shaft lower shaft head bearing 113 be connected on pedestal 115 to be provided with steering shaft lower shaft head bearing 113 outer shaft lower surface limited step, the mounting hole upper port of steering shaft lower shaft head bearing 113 is processed with the draw-in groove of steering shaft lower shaft head bearing Spring Card 114, when the mounting hole of steering shaft lower shaft head bearing 113 is after installation steering shaft lower shaft head bearing 113, the draw-in groove of steering shaft lower shaft head bearing Spring Card 114 in the mounting hole being installed into steering shaft lower shaft head bearing 113 by a steering shaft lower shaft head bearing Spring Card 114, in addition spacing to the outer shaft upper surface of steering shaft lower shaft head bearing 113, under being connected to the steering shaft of central steering shaft 107 lower port, spindle nose 112 is with the form of its commutation shifting fork bar crossed out towards left side, be arranged in the way to insert from the top down in the internal axle sleeve hole of steering shaft lower shaft head bearing 113 by the termination, bottom of spindle nose under steering shaft 112.

Under turn to be connected pedestal 115 bearing seat below a transverse axis stretched out towards both sides that two engaging lugs stretching out of the downward correspondence in the left and right sides connect, the spindle nose end wherein stretched out to the right is equipped with a hollow bracing wire adjusting screw(rod) for installing adjustment brake transition bracing wire 104 settled forward, the centre hole of hollow bracing wire adjusting screw(rod) towards under turn to the front being connected pedestal 115, under turn to be connected pedestal 115 bearing seat below stretch out to the left be one and turn to commutation declutch shift shaft, the root of commutation declutch shift shaft is turned to be provided with the mounting interface of one drag two water brake pump 103 forward, commutation declutch shift shaft stage casing is turned to be polished rod axial plane, commutation declutch shift shaft end is outwardly turned to be processed into thread rod.

Turn to commutation shift fork 117 and one drag two water brake pump 103 to be all arranged on down and turn to turning to of the bearing seat lower left being connected pedestal 115 to commutate on declutch shift shaft.

Wherein one drag two water brake pump 103 is the brake wisp oil pump that a conventional atv motorcycle right hand handle uses and the water brake master cylinder that simultaneously can be controlled two water brakes pincers 38 by shunt oil pipe, its mounting interface is mounted on down backward and turns to the bearing seat lower left being connected pedestal 115 to turn on the mounting interface of the root one drag two water brake pump 103 forward of commutation declutch shift shaft, the brake wisp end of one drag two water brake pump 103 is towards the front, right side bottom fuselage column 1, as oil pump lever brake wisp end head be arranged on down turn to the bearing seat lower right being connected pedestal 115 to stretch out spindle nose on the hollow bracing wire adjusting screw(rod) of brake transition bracing wire 104 installed corresponding, the brake wisp end head of oil pump lever be processed with the connection end of a brake transition bracing wire 104 and be connected by the termination that brake transition bracing wire 104 is corresponding with waiting brachium dual control wisp 12 upper end.

Turn to commutation shift fork 117 be one vertically use and be arranged on down the strip shape bipitch connecting rod turned on commutation declutch shift shaft turning to the bearing seat lower left being connected pedestal 115 from the side, turn to commutation middle, shift fork 117 side have turn to commutation declutch shift shaft mounting hole and two ends be processed with towards fore-and-aft direction U-shaped connect pawl, turn to commutation shift fork 117 upper end to be provided with a width near the position of U-shaped connection pawl to be enough to insert the long trough convergence hole of laterally putting down the commutation shifting fork bar termination of stretching out under steering shaft in the middle part of spindle nose 112, this long trough convergence hole is broadened gradually by Inside To Outside and forms certain taper, turn to commutation shift fork 117 on turning to commutation shift fork axis hole and long trough convergence hole perforate direction identical, turn to commutation shift fork 117 by its middle have turn to commutation shift fork axis hole ecto-entad to be arranged on down to turn to the bearing seat lower left being connected pedestal 115 turn on the polished rod axle of commutation declutch shift shaft stage casing while, turn to the long trough convergence hole on commutation shift fork 117 also ecto-entad installation sleeve be connected on down on the commutation shifting fork bar crossed out to the left of spindle nose 112 under the steering shaft turning to and be connected and install above pedestal 115, under turn to the commutation declutch shift shaft end thread termination that turns to of the bearing seat lower left being connected pedestal 115 to turn to that commutation shift fork axis hole is to the left to be stretched out and by turning to the shift fork captive nut 118 that commutates to be fixed from what turn to commutation shift fork 117 middle.

Be arranged on down and turn to the U-shaped of side direction in commutation shift fork 117 two ends that turns to be connected on the left of pedestal 115 to connect the front and back end of U-lag gap towards fuselage of pawl, turn to the upper end U-shaped of commutation shift fork 117 to connect between pawl and front steering wheel shaft 18 stretch out to the left front steering wheel shaft 18 spindle arm and be bolted the front-wheel steering pull bar 119 that self two ends is provided with shaft-like oscillating bearing, the empennage turning to the lower end U-shaped of commutation shift fork 117 to connect to be provided with shaft-like oscillating bearing by being bolted self two ends between caudal wing shaft 20 spindle arm that pawl and caudal wing shaft 20 stretch out to the left turns to pull bar 120.

As shown in figure 12, the handle bar upper end of left control stalk 100 front end raises up on the termination of stretching out, with the form be arranged above and below, the hollow bracing wire adjusting screw(rod) of two terminations towards left control stalk front is housed, the hollow bracing wire adjusting screw(rod) that the handle bar upper end top position being positioned at left control stalk 100 front end is installed is as brake transition bracing wire 104 adjusting bolt, the hollow bracing wire adjusting screw(rod) that the handle bar upper end lower position being positioned at left control stalk front end is installed is as displacement bracing wire 105 adjusting bolt, the wisp mounting groove waiting the U-shaped of brachium dual control wisp 12 for being connected and fixed is stretched out before the handle bar stage casing of left control stalk 100 front end is provided with one, the bolt connecting hole that a correspondence such as to be connected and fixed at the brachium dual control wisp 12 is provided with between U-shaped wisp mounting groove both sides.

On the lever that brachium dual control wisp 12 is the brachiums such as two ends, on conventional handle, wisp controls on the Length discrepancy lever construction basis of bracing wire, the intimate isometric arm of force will be designed to by the wisp part that holds controls with the resistance arm being connected and fixed bracing wire termination as power arm, bolt connecting hole corresponding between the wisp mounting groove both sides of U-shaped is provided with Deng in the middle of brachium dual control wisp 12, erect in the wisp mounting groove of the U-shaped be installed on the handle bar of left control stalk 100 front end Deng in the middle of brachium dual control wisp 12 with the part of bolt connecting hole, between the bolt connecting hole that brachium dual control wisp 12 is corresponding with the wisp mounting groove both sides of the U-shaped on the handle bar of left control stalk 100 front end, penetrated by a bolt as fulcrum shaft and be connected and fixed,

Using the power arm waiting brachium dual control wisp 12 lower end wisp to control as driver with the form of holds, the handle bar upper end of resistance arm upper end towards left control stalk 100 front end of bracing wire termination is fixed Deng brachium dual control wisp 12, owing to will connect brake transition bracing wire 104 and displacement bracing wire 105 as resistance arm upper end simultaneously, transition bracing wire 104 of wherein braking is the connecting stay wire between the brake wisp end head on brachium dual control wisp 12 upper ends such as connection and one drag two water brake pump 103, and displacement bracing wire 105 is that the connection pawl of the displacement bracing wire 105 connecting displacement shifting fork bar 78 front end U-shaped is to the connecting stay wire waited between brachium dual control wisp 12 upper end, because it is different that the wisp that during rotor 22 displacement, displacement shifting fork bar 78 reaches the amplitude range of stirring needed for action effect and controls one drag two water brake pump 103 reaches the amplitude range of moving needed for action effect, brake transition bracing wire 104 termination and displacement bracing wire 105 termination of fixing the resistance arm upper end connection of bracing wire termination Deng brachium dual control wisp 12 are respectively according to the difference of the size of its movable amplitude, be mounted on respectively using the form be arranged above and below and wait the top of termination, brachium dual control wisp 12 upper end and the position of lower end, adjacent top as resistance arm.

When the grip that wisp termination Deng brachium dual control wisp 12 lower end is subject to driver is pulled, the bolt of the both sides of the wisp mounting groove of U-shaped can be penetrated as balance pivot on the handle bar of left control stalk 100 front end at brachium dual control wisp 12 two ends, isometric distance can be streaked in termination up and down Deng brachium dual control wisp 12, displacement bracing wire 105 and brake transition 104 bracing wire are similarly two of the simplifying steering unit transition bracing wire across the brake wisp of distance join displacement shifting fork bar 78 bracing wire connection end and one drag two water brake pump 103, simplify omit traditional span from rigid connection operation link quantity and weight while, the front end of termination meeting towing brake transition bracing wire simultaneously 104 and displacement bracing wire 105 that the upper end Deng brachium dual control wisp 12 is connected and fixed bracing wire moves simultaneously, brake transition bracing wire 104 and displacement bracing wire 105 by the grip of hand by etc. the termination up and down of brachium dual control wisp 12 be close to after isometric lever streaks intimate isometric distance, by the pulling force of grip brachium dual control wisp 12 lower end such as being applied to of driver by wait brachium dual control wisp 12 upper end to convert to displacement bracing wire 105 that reciprocity brachium dual control wisp 12 upper end connects and brake transition 104 bracing wire front end, and equally pulling force transition is delivered to displacement shifting fork bar 78 on U-shaped connection pawl termination displacement bracing wire 105 end of front end and with on brake transition 104 end of pulling to be close to.

When displacement action is carried out in brachium dual control wisp 12 lower ends such as driver holds with a firm grip, displacement bracing wire 105 front end of brachium dual control wisp 12 upper end such as to affect, and it is descending centered by the horizontal pitch change axes of distance-variable rocker arm 76 to drive the displacement bracing wire of the U-shaped of displacement bracing wire 105 end drop-down displacement shifting fork bar 78 to connect pawl termination

Due to two Length discrepancy lever arm of force that the horizontal pitch change axes axle center O being mounted on the pedestal left and right clamping plate that vert 70 with distance-variable rocker arm 76 both sides formed between the axle center B of two spindle nose D of crossed strip resetting shaft and the axle center C near the distance-variable rocker arm pin axle 83 of horizontal pitch change axes axle center O front position on distance-variable rocker arm 76 is a dot center, because the spacing BO of distance-variable rocker arm 76 rear end crossed strip resetting shaft axle center B and horizontal pitch change axes axle center O is equivalent to horizontal pitch change axes axle center O and the several times near spacing OC between the distance-variable rocker arm pin axle 83 axle center C below it, because the arm of force OB of the horizontal pitch change axes O on distance-variable rocker arm 76 to crossed strip resetting shaft B one end is longer, under leverage, OB can centered by the horizontal pitch change axes O on distance-variable rocker arm 76, the lever termination of two less displacement reset tension spring 81 crossed strip resetting shaft axle center B as lever OB two ends be equipped with, can to horizontal pitch change axes axle center O to distance-variable rocker arm pin axle 83C between shorter arm of force OC applies the downward displacement reset pulling force being several times as much as two displacement reset tension spring 81 pulling force, make distance-variable rocker arm 76 rear end crossed strip resetting shaft only need to be arranged on distance-variable rocker arm 76 on crossed strip resetting shaft two less displacement reset tension springs 81 under the effect of autogenous shrinkage pulling force, remain distance-variable rocker arm pin axle 83 thrust upwards to connecting double end spherical plain bearing rod end 46 lower end axis hole in distance-variable rocker arm 76.

When same with the displacement shifting fork bar 78 that termination on the left of the horizontal pitch change axes on distance-variable rocker arm 76 links together as one end fulcrum centered by the horizontal pitch change axes axle center O of distance-variable rocker arm 76, the other end to the U-shaped shift fork end A point of displacement shifting fork bar 78 front end is the lever arm of force OA of brachium, its OA lever length is far longer than the several times of the lever arm of force OC between the horizontal pitch change axes on distance-variable rocker arm 76 to the lever arm of force OB and horizontal pitch change axes to distance-variable rocker arm pin axle 83 of two spindle noses of crossed strip resetting shaft, in the strength that the U-shaped shift fork end A point of displacement shifting fork bar 78 applies, the strength lever arm of force OC termination between the horizontal pitch change axes on distance-variable rocker arm 76 to the lever arm of force OB and horizontal pitch change axes to distance-variable rocker arm pin axle 83 of two spindle noses of crossed strip resetting shaft producing several times can be delivered under leverage.

Relative to the U-shaped connection pawl termination of displacement shifting fork bar 78 towards front end, only need apply very little pulling force to the displacement bracing wire 105 that U-shaped connects pawl termination, just leverage can be passed through, pull the double end spherical plain bearing rod end 46 be arranged near the distance-variable rocker arm pin axle 83 of front end and connection thereof in distance-variable rocker arm 76 descending, and the pitch change axes 44 driving double end spherical plain bearing rod end 46 upper end to connect is slided descending along rotor shaft 40 inwall, and can be in addition spacing to pitch change axes 44 amplitude that glides as the bottom dead point glided by running through the pitch change axes Limit screw 43 that is fixed on rotor shaft 40 main shaft root, the displacement cantilever 47 that descending pitch change axes 44 can affect pitch change axes 44 upper end to install simultaneously is descending, the displacement spherical plain bearing rod end screw rod 51 that displacement cantilever 47 two ends is installed downwards presses down rotary wing changing between the rotor clamping plate 65 that are attached thereto apart from pole socket 62, rotor clamping plate 65 are connected with rotor pitch change axes about 63 and runs through rotor clamping plate 65 and clamping plate type propeller hub for main point of connection, and the rotor 22 installed additional between rotor clamping plate 65 is twisted centered by the outer spherical inner sleeve center-point being arranged on the displacement oscillating bearing 56 on clamping plate type propeller hub by rotor pitch change axes 63, rotor pitch change axes 63 drives in displacement oscillating bearing 56 outer spherical to be enclosed within displacement oscillating bearing 56 and twists in ball-type overcoat in twist process, also therefore there is the change that the angle of attack reduces in the rotor 22 that rotor clamping plate 65 other end is connected, the operating angle of attack of rotor 22 is reduced to 0 degree from 2 degree by the design, thus realize the displacement of rotor 22, such displacement is convenient to rotor 22 and enters required spin range of speed as early as possible under pusher propeller 10 wake flow is brushed effect.

In displacement process when displacement shifting fork bar 78 pulls the distance-variable rocker arm pin axle 83 being arranged on close front end in distance-variable rocker arm 76 and the double end spherical plain bearing rod end 46 connected is descending, the upper end of two displacement reset tension springs 81 that distance-variable rocker arm 76 rear end crossed strip resetting shaft two ends mounts is stretched, after making driver unclamp the assurance control of reciprocity brachium dual control wisp 12 for extended state displacement reset tension spring 81, by the restorative shrinkage tensions effect of displacement reset tension spring 81, rotor 22 angle of attack is returned to the normal angle of attack.

Owing to can make tilt slide by a relatively large margin in self in ball-type overcoat up and down as self outer spherical inner sleeve of displacement oscillating bearing 56, while meeting rotor 22 displacement needs, because displacement buffering gum cover 58 diameter that clamping plate type propeller hub two ends are installed be greater than propeller hub face 53 combines with lower propeller hub face 54 external end head after thickness be still slightly less than between the thicker external end head end face of displacement oscillating bearing inner covering 57 two in the spherical joint inner sleeve of two opposed insertion displacement oscillating bearings 56 and spacing, be less than and be arranged on spacing between axle sleeve two ends, stage casing Flat-end that the contour and rotor that is common support rotor clamping plate 65 of displacement oscillating bearing inner covering 57 two external end head end faces in displacement oscillating bearing 56 waves buffer shaft 60 too, put centered by the outer spherical inner sleeve of the displacement oscillating bearing 56 that the rotor clamping plate 65 of connection rotor 22 can be connected by rotor pitch change axes 63 and wave up and down, and while the leeway making rotor 22 have to wave up and down, rotor 22 can also be made to wave in process up and down, the crimp of the outer face of rotor clamping plate 65 pairs of displacement buffering gum covers 58 is utilized to be able to flexible buffer, even when rotor 22 laterally brandishes work centered by rotor shaft 40, the collision that the stage casing axle sleeve of buffer shaft 60 and two displacements cushions transverse direction between gum cover 58 can be waved the side shake of rotor 22 is cushioned by erectting the rotor be installed between two displacements buffering gum cover 58, thus reach to meet and to wave up and down when rotor 22 works and the needs of yaw.

When left hand such as to hold with a firm grip at the brachium dual control wisp 12 lower end wisp, it is descending towards the U-shaped connection pawl termination of front end that displacement bracing wire 105 Deng brachium dual control wisp 12 upper end can draw displacement shifting fork bar 78 simultaneously, and the pitch change axes 44 pulling distance-variable rocker arm 76 to connect by leverage is descending, the displacement cantilever 47 simultaneously affecting pitch change axes 44 upper end to install is descending, the displacement spherical plain bearing rod end screw rod 51 that displacement cantilever 47 two ends is installed downwards presses down rotary wing changing between the rotor clamping plate 65 that are attached thereto apart from pole socket 62, rotor clamping plate 65 are connected by rotor pitch change axes about 63 and runs through rotor clamping plate 65 and clamping plate type propeller hub and centered by the outer spherical inner sleeve center-point being arranged on the displacement oscillating bearing 56 on clamping plate type propeller hub, rotor pitch change axes 63 drives in displacement oscillating bearing 56 outer spherical to be enclosed within displacement oscillating bearing 56 and twists in ball-type overcoat, also therefore there is the change that the angle of attack reduces in the rotor 22 that rotor clamping plate 65 other end connects, realize the displacement action of rotor 22.

As shown in figure 13, when holding the wisp such as dual control such as brachium such as grade 12 of left control stalk 100 front end left hand handle, realize affecting displacement bracing wire 105 and brake transition bracing wire 104 simultaneously, can complete rotor 22 pitch-changing mechanism and the control controlling left and right support wheel 37 brake system.

Be close to isometric owing to waiting brachium dual control wisp about 12 two ends, when driver's left hand such as to hold with a firm grip at the brachium dual control wisp 12 lower end wisp, the bolt of the both sides of the wisp mounting groove of U-shaped can be penetrated as balance pivot on the handle bar of left control stalk 100 front end at brachium dual control wisp 12 two ends, isometric distance can be streaked in termination up and down Deng brachium dual control wisp 12, displacement bracing wire 105 and brake transition 104 bracing wire are similarly as two of simplifying steering unit are across the transition bracing wire of the brake wisp of distance join displacement shifting fork bar 78 bracing wire connection end and one drag two water brake pump 103, simplify omit traditional span from rigid connection operation link quantity and weight while, upper end Deng brachium dual control wisp 12 is connected and fixed bracing wire termination meeting towing brake transition bracing wire simultaneously 104 and displacement bracing wire 105 is moved simultaneously, brake transition bracing wire 104 and displacement bracing wire 105 by the grip of hand by etc. the termination up and down of brachium dual control wisp 12 be close to after isometric lever streaks intimate isometric distance, grip is close to equivalent transition and is delivered to displacement shifting fork bar 78 towards on the U-shaped connection pawl termination of front end and the brake wisp end head of one drag two water brake pump 103, the brake wisp of brake transition bracing wire 104 one drag two water brake pump 103 that transition bracing wire 104 lower end connects and tension is braked is affected to streak and wait the scope of the radians such as brachium dual control wisp 12 lower end wisp and distance, and make the brake wisp of one drag two water brake pump 103 extruding brake pump be achieved simultaneously and synchronously complete brake.

As shown in figure 14, because control stalk lateral tilting rotating shaft 94 stage casing intersects vertically as the vert axial line of control stalk anteversion and retroversion rotating shaft 95 that the polished rod axle axial line of faying face and control stalk lateral tilting rotating shaft annular side end face, termination central shaft hole install of left and right, the T-shaped being connected to the front of control stalk pedestal 92 trailing arm 96 that verts verts using the control stalk anteversion and retroversion rotating shaft 95 of its stage casing lateral connection as T-shaped the lateral shaft of trailing arm 96, and T-shaped is verted, trailing arm 96 verts using the polished rod axle of control stalk lateral tilting rotating shaft 94 as T-shaped the longitudinal axis of trailing arm 96, be common center of verting using the axial line intersection point as the control stalk lateral tilting rotating shaft 94 of longitudinal axis and the flat end face RC control stalk anteversion and retroversion rotating shaft 95 that penetrates the annular termination of longitudinal axis control stalk lateral tilting rotating shaft 94 as lateral shaft, the T-shaped trailing arm 96 that verts is made to have possessed and realize the function of verting all around for support with control stalk pedestal.

When driver is with when all around different angles pull left control stalk 100 and right control stalk 101, because T-shaped is verted the axial line of two, both sides, U-shaped control stalk mount pad 97 upper end in the transversely arranged engaging lug of concentric that trailing arm 96 bottom connects, contour and parallel with the axial line of the control stalk anteversion and retroversion rotating shaft 95 of installing through side end face, control stalk lateral tilting rotating shaft 94 annular termination central shaft hole, make two, both sides, U-shaped control stalk mount pad 97 upper end engaging lug equally can with have T-shaped vert trailing arm 96 longitudinal axis function control stalk lateral tilting rotating shaft 94 and have T-shaped vert trailing arm lateral shaft function and the axial line intersection point of flat end face RC control stalk anteversion and retroversion rotating shaft 95 that penetrates longitudinal axis control stalk lateral tilting rotating shaft annular termination is common center of verting, verting forwards, backwards, the pull bar 23 and push-and-pull two that the U-shaped connection pawl verting both sides, trailing arm 96 upper end by T-shaped connects is verted, two rotor shaft be connected with rotor shaft 40 lateral shaft driving two pull bar 23 upper ends of verting to connect are verted arm 85, centered by axial line intersection point each other, rotor shaft 40 and clamping plate type propeller hub verting all around is realized by laterally vert rotor shaft 40 that function and self both sides lateral shaft have an anteversion and retroversion rotating function of lateral tilting rotating shaft about 74.

When left control stalk 100 turns in course of action making anteversion and retroversion, can pass in its back-end turn to connector loop 106 in sideways elongated slot ring before and after rotate, but the connector loop 106 that turns to being mounted on central steering shaft 107 upper end can not be made to be subjected to displacement.

And when left control stalk 100 transfers in process making lateral tilting, left control stalk 100 rear end is turning to connector loop 106 to move up and down in sideways elongated slot ring, but the connector loop 106 that turns to being mounted on central steering shaft 107 upper end also can not be made to be subjected to displacement centered by the axle center of central steering shaft 107.

Due on this basis, U-shaped control stalk mount pad 97 can also under the left control stalk 100 of maintenance and the original attitude of verting of right control stalk 101, left and right directions torsion is realized to install with it centered by the control stalk steering shaft axle center that trailing arm 96 is downward and the T-shaped be connected is verted, do in process when left control stalk 100 reverses about making, can promote or pull be attached thereto turn to connector loop 106 towards sideways elongated slot ring, on the steering shaft making to turn to connector loop 106 to be connected with central steering shaft 106 upper end by its other end spindle nose 105 axle center centered by left and right reverse, central authorities' steering shaft 107 be one be mounted on turn to be connected pedestal 108 and under turn to and be connected transition axis between pedestal 115, the left control stalk about 101 penetrated that turns in connector loop 106 that its upper end connects by central authorities' steering shaft 107 reverses strength by being delivered to below fuselage column 1 above fuselage column 1, when be positioned on higher position, column 1 upper end turn to the long trough connector loop on the free end of connector loop 106 to be promoted by left control stalk about 100 time, turn to connector loop 106 when lower end connects and on the steering shaft being fixed on spindle nose bearing 110 on steering shaft, centered by spindle nose 109, horizontal radial rotates, drive central steering shaft 107 radial rotary that on steering shaft, spindle nose 109 lower end connects, and spindle nose 112 synchronous axial system under the steering shaft driving central steering shaft 107 lower end to connect, under steering shaft spindle nose 112 by its cross out and be inserted into turn to the commutation shifting fork bar of long trough convergence hole on commutation shift fork 117 to stir to turn to commutation shift fork less than 117 to turn to be connected that pedestal 115 stretches out to the left turn to swing centered by commutation declutch shift shaft, promoting or pull turn to the upper end U-shaped of commutation shift fork 117 to connect front-wheel steering pull bar 119 that pawl and front steering wheel shaft 18 connect and turning to the lower end U-shaped of the shift fork 117 that commutates to connect pawl turns to pull bar 120 synchronously to complete corresponding handling maneuver with the empennage that caudal wing shaft 20 is connected.

Claims (5)

1. single manual cyclogyro of the present invention, single complete manual cyclogyro is by fuselage sections, rotor shaft cantilever verts structure, full manual mechanism and possess inner variable-distance rotor head mechanism composition, adopt positive 3 the alighting gear fuselages of high center of gravity, main machine body is by column, front-axle beam, the back rest, engine bed, front support beam forms, adopt wheel flutter in dead ahead, empennage is rearmounted, operator's saddle and driving engine are placed in column front and back respectively, using pusher propeller as power, 3 framework type independence shock-absorbing support mechanisms with propeller reaction thrust balancing device carry out the antagonistic force that when symmetric screw propeller works, air produces fuselage, strengthen the smoothness that rises and falls of complete machine self, the full manual mechanism of converged functionality is turned to enable driver as controlling the rotary wing changing distance completed motor bike cyclogyro by possessing, rotor shaft is verted, dogled, the full manual mode operation of brake.

2. single manual cyclogyro according to claim 1, is characterized in that described fuselage sections is made up of fuselage main support and 3 framework type independence shock-absorbing support mechanism two parts with propeller reaction force balance auxiliary device;

1) the fuselage main support described in is by column, front-axle beam, pedal, gauge panel column, gauge panel, the back rest, engine bed beam, front support beam, driving engine, pusher propeller, motor support column, Deng brachium dual control wisp, turn to connector loop, turn to commutation shift fork, can constant speed throttle, left and right support wheel, steering front wheel, front steering wheel shaft, empennage, caudal wing shaft, tail wheel, rotor, vert pull bar, radiator-water box, operator's saddle, column lower end connecting strap, balance wing axle bed, balance wing axle, front support beam lower end connecting cleat, engine beam lower end connecting cleat, double-threaded screw bar, the spherical plain bearing rod end nut composition of horizontal support bar, the column of fuselage main support occupies fuselage central authorities and erects and omit hypsokinesis, its upper end is for installing rotor head mechanism, the both hands control stalk mechanism of rotor shaft cantilever inclining rotary mechanism and full manual mechanism, column lower end head turns to the column lower end connecting strap being connected foundation bolt connecting bore to be connected on back rest front end position more rearward with clamping plate form under being had by two pieces of front ends, column stage casing upper position, be connected and fixed forward the front-axle beam of a test forward, be fixedly connected with the engine bed beam of a level backward, connected by a motor support column erect between the fuselage back rest stage casing of engine bed beam rear end and below thereof and support, termination, back rest front end connects the front support beam that stretches out of oblique upper forward, front support beam upper end by clamping plate connecting strap with to be fixedly connected with in the middle part of front-axle beam and supplemental support front-axle beam, be connected to front support beam lower end and the front support beam lower end connecting cleat lower end between back rest front end and motor support column lower end connecting cleat lower end be connected with back rest two side backward under stretch out back rest lower surface, form two for installing the clamping plate shape space of balance wing axle bed, the square bulk of balance wing axle bed outside support, balance wing axle bed left and right width is identical with rear beam width and front/rear end is processed with a balance wing axle installs through hole, two balance wing axle beds are close to bottom the back rest with the square upper end face of outside, between the clamping plate space that two sides embedding front support beam lower end connecting cleats of balance wing axle bed and motor support column lower end connecting cleat lower end are formed, the circular mounting through hole run through between two balance wing axle bed front/rear ends is the arrangement of front and back concentric below the back rest, balance wing axle two terminations of a tubulose penetrate the mounting hole at two balance axle bed centers respectively, be arranged on after between two balance wing axle beds below the back rest, the balance wing axle bed both sides of installing below front support beam lower end connecting cleat and motor support column lower end connecting cleat are run through respectively from the side by two double-threaded screw bars, balance wing axle and balance wing axle bed are fastened on below the back rest, after the threaded portion of two double-threaded screw rod end heads is protruding through the both sides of two balance wing axle beds, two threaded ends are respectively stretched out to both sides, two threaded end parts that every side is stretched out are connected with the spherical plain bearing rod end nut of two horizontal support bars of the same side is respectively fixed, nut top, the rod end joint ball-and-socket joint centre hole of two horizontal support bars becomes two horizontal connecting hole of 3 framework type independence shock-absorbing support mechanism bottoms of every side, operator's saddle and be placed in column front and back respectively using pusher propeller backward as the driving engine of power, operator's saddle and engine bottom are in equal height, wherein operator's saddle is a backrest is the seat of fuel tank, operator's saddle bottom be arranged on adopt clamping plate connecting strap to be connected with column front-axle beam rear end on, the top of the fuel tank backrest of operator's saddle be bolted be fixed on above column stage casing on turn to and be connected on pedestal front end face, radiator-water box is fastened on column rear and is positioned at the position turning to and be connected above pedestal rear end, a gauge panel column is upwards installed by clamping plate connecting strap in the stage casing, front-axle beam front end of front end test, gauge panel is installed in gauge panel column upper end, gauge panel column bottom front is horizontally installed with a pedal, front-axle beam front end installs the front steering wheel shaft that a bottom adopts trailing arm type shock-absorbing support downwards, steering front wheel is arranged on the towing arm lower end of front steering wheel shaft bottom, in the middle part of steering front wheel wheel shaft, side is provided with the spindle arm of the cantilevered steering front wheel that is stretched out on the left of fuselage, driving engine is placed on the engine bed beam that stretches out at column rear, a small-sized support tail wheel is installed with by connecting strap below back rest follower head, and upwards install one by clamping plate connecting strap and have and stretch out cantilevered spindle arm and self vertically rotating caudal wing shaft to the left, the full dynamic formula empennage of connection one above caudal wing shaft, the tailplane on empennage top and the center of thrust line of pusher propeller contour,

2) the presylvian fissure strut that 3 the framework type independence shock-absorbing support mechanism section with propeller reaction force balance auxiliary device described in are all had by the every side of fuselage, rear horizontal support bar, lateral support bar, left and right supports wheel shaft, water brake clamps, left and right support wheel captive nut and left and right support wheel composition, and on the basis of this mechanism, with the addition of the propeller reaction thrust balancing device be made up of a balance wing, left and right support wheel shaft toward the outer side the spindle nose of a section through after the left and right support wheel possessing brake disc wheel hub, fixed by left and right support wheel captive nut, left and right supports the stage casing of wheel shaft to be possessed and is respectively used to be connected presylvian fissure strut and lateral support bar engaging lug toward the outer side with the U-shaped engaging lug of two upward forward, left and right supports the water brake pincers that wheel shaft connection pawl is towards the rear used for fixing left and right support wheel, lateral support bar towards the upper end decoupling rod top of inner side engaging lug connect be supported on fuselage column is connected with operator's saddle fuel tank backrest upper end on turn to the U-shaped being connected pedestal both sides to connect on pawl, presylvian fissure strut and rear horizontal support bar are connected pawl towards the U-shaped of inner side and are connected as bikini framework lower horizontal connecting bore with nut top, two the rod end joints ball-and-socket joint centre hole below fuselage back rest both sides front end and stage casing respectively by bolt, presylvian fissure strut, rear horizontal support bar and lateral support bar termination toward the outer side are all fastened on left and right and support on wheel shaft, balance wing as propeller reaction thrust balancing device is one piece of triangular fibre aerofoil, according to the difference of pusher propeller hand of rotation, balance wing is arranged on and pusher propeller hand of rotation opposite side, balance wing principal plane and balance wing axle, presylvian fissure strut, the level triangle frame area that rear horizontal support bar is formed is identical, three limits of triangle aerofoil are processed to hollow sleeve tubular, correspondence can be enclosed within any side of fuselage by balance wing axle, presylvian fissure strut, on the triangle horizontal frame that rear horizontal support bar is formed, its principal plane covers balance wing axle, presylvian fissure strut, on the triangle horizontal frame that rear horizontal support bar is formed, form a leg-of-mutton horizontal aerofoil.

3. single manual cyclogyro according to claim 1, it is characterized in that described rotor head mechanism by possessing the clamping plate type propeller hub mechanism of inner variable-distance and rotor shaft agent structure, rotor connection part three part forms;

1) buffer shaft, up and down propeller hub face tie bolt composition are waved primarily of upper propeller hub face, lower propeller hub face, double-range ball bearing, displacement oscillating bearing, displacement oscillating bearing inner covering, rotor pitch change axes, displacement buffering gum cover, displacement cushion compound sleeve, rotor by the clamping plate type propeller hub mechanism described in;

Upper propeller hub face and lower propeller hub face are the identical and strip shape clamping plate of symmetry of two outward appearances, upper propeller hub face is provided with bolt connecting hole corresponding to each other with lower propeller hub face periphery, upper propeller hub face and center, lower propeller hub face are processed with a vertical double-range ball bearing mounting hole run through, the double-range ball bearing mounting hole of the center in upper propeller hub face and lower propeller hub face is processed with the limited step of double-range ball bearing overcoat upper and lower end face towards the faying face end face outside direction in upper propeller hub face and lower propeller hub face, upper propeller hub face and lower propeller hub face can be combined in the face of detaining by inner side binding end, propeller hub face and lower propeller hub face end face outside are distinguished upward and below, from upper propeller hub face and center, lower propeller hub face double-range ball bearing mounting hole on the end face of two ends, centered by double-range ball bearing mounting hole, along upper propeller hub face and lower propeller hub facing on the line of centers of each termination each corresponding be processed with one vertical run through end face outside in upper propeller hub face and lower propeller hub face displacement oscillating bearing mounting hole and one near external end head, the rectangle elongated hole that displacement cushions gum cover is installed, each displacement oscillating bearing mounting hole is processed with the limited step of displacement oscillating bearing overcoat towards upper propeller hub face and end face outside direction, lower propeller hub face, each displacement oscillating bearing mounting hole is used for installing an oscillating bearing with spherical joint inner sleeve as displacement oscillating bearing using radial direction as Impact direction, the part outer face upper propeller hub face and lower propeller hub face being cushioned the rectangle elongated hole of gum cover for installing displacement is processed to inclined-plane to end portion, the rectangle elongated hole of each correspondence in inner side in conjunction with end face being respectively processed with in two rectangular edges in double-row bearing mounting hole and external end head direction two recessed mounting grooves, when the inner side binding end of upper propeller hub face and lower propeller hub is connected to become a complete propeller hub shell in the face of detaining installation, the groove of these correspondences just defines one by one independently axle head location and installation hole, this rectangle elongated hole is used for being installed into two displacement cushion compound sleeves having penetrated polished rod shape towards the form level arranged side by side in upper propeller hub face and lower propeller hub two ends direction and the displacement retaining certain interval to each other cushions gum cover, and one is erect the displacement that vertical folder is contained between two displacement cushion compounds cover gaps of installing side by side and waves buffer shaft,

The two-port up and down of trepanning each opposed installation displacement oscillating bearing inner covering in each displacement oscillating bearing spherical joint, displacement oscillating bearing inner covering is the round sleeve of the annular stop step being provided with projection for lining between trepanning and rotor pitch change axes and outside in displacement oscillating bearing spherical joint, one end that two displacement oscillating bearing inner coverings are slightly thin and displacement oscillating bearing inner sleeve endoporus equal diameter, two displacement oscillating bearing inner coverings are respectively from the two ends opposed insertion displacement oscillating bearing spherical joint inner sleeve of displacement oscillating bearing spherical inner sleeve endoporus, the limited step of displacement oscillating bearing inner covering outer face is stuck on two ports of displacement oscillating bearing spherical joint inner sleeve endoporus, each displacement oscillating bearing inner covering endoporus penetrates a rotor pitch change axes for the mode erect, the thicker external end head end face of displacement oscillating bearing inner covering two is for supporting rotor clamping plate,

Rotor pitch change axes and rotary wing changing apart from spindle nut be one in an upright manner through the nut of the bolt shank while the displacement oscillating bearing inner covering in rotor clamping plate and displacement oscillating bearing endoporus, the two linked together and coupling thereof;

Displacement buffering gum cover is limited and makes and cushion the circular tube shaped rubber coating that rotor waves shimmy amplitude, displacement buffering gum cover diameter be greater than propeller hub face be combined with lower propeller hub face external end head after thickness, but displacement buffering gum cover diameter is slightly less than spacing between the thicker external end head end face of displacement oscillating bearing inner covering two in the spherical joint inner sleeve of two opposed insertion displacement oscillating bearings, the displacement cushion compound sleeve being slightly longer than the polished rod shape axial plane of displacement buffering gum cover by one in two end face center holes of its tubular penetrates and outside two ends, stretches out two spindle noses

The displacement that after upper propeller hub face is combined with lower propeller hub face, two penetrate displacement cushion compound sleeve on each side head cushion gum cover and is arranged in the rectangle elongated hole that upper propeller hub face is combined with lower propeller hub face on each side head afterwards side by side, two spindle noses of the displacement cushion compound sleeve stretched out outside each displacement buffering gum cover two ends, upper propeller hub face and lower propeller hub face in conjunction with time embed recessed mounting groove corresponding to two ends rectangle elongated hole two rectangular edges in conjunction with time the axle head location and installation hole that formed in;

The round sleeve of to be thick and face, termination, curved recessed two ends, a stage casing be plane that rotor waves buffer shaft and one penetrate the double-threaded screw bar composition of axle sleeve, and rotor is waved between the Flat-end of axle sleeve two ends, buffer shaft stage casing and is arranged between displacement oscillating bearing inner covering two the external end head end faces in displacement oscillating bearing contour;

Rotor is waved in the gap that the curved recessed part in buffer shaft round sleeve stage casing is installed between two displacement buffering gum covers arranged side by side, rotor waves double-threaded screw bar two ends that buffer shaft center the penetrates axle sleeve end face outside towards upper propeller hub face and lower propeller hub face, the upper and lower end face that rotor waves round sleeve two terminations in buffer shaft stage casing is plane, use for supporting rotor clamping plate, the double-threaded screw bar that the round sleeve center that rotor waves buffer shaft stage casing penetrates is supported and fixed between rotor clamping plate for the round sleeve connection of rotor being waved buffer shaft;

Upper propeller hub face and lower propeller hub face are installed in the face of detaining by the inner side binding end in upper propeller hub face and lower propeller hub face, and installed by the face of the propeller hub up and down tie bolt bolt hole that upper propeller hub face is corresponding with lower propeller hub face periphery and penetrate upper and lower propeller hub face tie bolt and fixed, double-range ball bearing, displacement oscillating bearing, displacement buffering gum cover, displacement cushion compound sleeve, rotor are waved buffer shaft and be arranged on wherein;

2) the rotor shaft body structure portion described in is made up of rotor shaft, the horizontal axle sleeve of rotor shaft, rotor shaft upper end locking nut, pitch change axes Limit screw, pitch change axes, pitch change axes lower end connecting pins axle, double end spherical plain bearing rod end, displacement cantilever, pitch change axes bearing, pitch change axes bearing flange, pitch change axes bearing flange tie bolt, displacement spherical plain bearing rod end screw rod, pitch change axes upper end captive nut;

Rotor shaft is a rotor shaft in inversion T-shaped outward appearance, rotor shaft main body forms by by the vertical shaft of a hollow and the vertical shaft root lateral shaft that both sides are stretched out to the left and right, the vertical shaft upper end of rotor shaft is the cylindrical vertical shaft erectting extension upward, rotor shaft lower end main shaft root is thicker bulk four prismatic, between former and later two roots of main shaft root, inclined-plane is processed in lower surface, aft end face is slightly long and to downward-extension, main shaft root front/rear end upper end is processed with a pre-and post perforative caging bolt hole near circular vertical shaft root place, face, main side, two sides, left and right is plane, center, face, main side, left and right respectively to left and right separately level stretch out a lateral shaft, two lateral shafts are segmented from inside to outside and are processed in step-like tapered three parts, light over glaze body is divided near a lateral shaft root part and center section part, lateral shaft stage casing light over glaze body divides the spline being processed with tiltedly below rotor shaft lateral shaft spline forward, the outwardly directed end section of lateral shaft is processed with screw thread,

Four parts are from bottom to top processed in the outside of the vertical shaft part for rotor shaft that rotor shaft four prismatic main shaft root upwards extends, close main shaft root one section is polished rod axial plane, middle part is processed with the limited step of the double-range ball bearing of an evagination, the limited step of double-range ball bearing is upwards processed with the bearing installation position of the double-range ball bearing in one section of light face, and the bearing installation position vertical shaft top end part upwards of double-range ball bearing omits thin and is processed with outside thread;

The installation axle hole processing pitch change axes circular in hollow light face is run through up and down from vertical shaft operative tip to main shaft root bottom, the circular shaft bore being wherein positioned at main shaft root portion is slightly thick, and with upwards in the junction of the circular shaft bore portion U-shaped that is processed into an interior pitch change axes lower end be connected the mounting limit step of the upper surface of pawl;

Pitch change axes is a middle part main shaft is polished rod axle, the U-shaped that bottom is processed with down connects pawl, top is be threaded the pitch change axes bearing installation position of rod end head and the axle of setting use, bottom it, be divided into U-shaped to top connect pawl, main shaft polished rod axial plane, three, the installation position part of pitch change axes bearing, U-shaped connects pawl, main shaft polished rod axial plane, two steps processed between pitch change axes bearing installation position are divided in tapered three parts, it is excessively step-like between boundary bottom polished rod axle that U-shaped connects in the middle part of upper end, radix unguis portion and slightly thin pitch change axes, the lower end of its main shaft polished rod shaft portion connects the axle root place of pawl transition shoulder near its U-shaped, with U-shaped connect two connecting bores corresponding on pawl towards in the position of 90 degree of angles, be processed with an elongate in shape along a pitch change axes above-below direction pre-and post perforative spacing hole corresponding near the caging bolt hole at circular vertical shaft root place with rotor shaft main shaft root front/rear end upper end, main shaft polished rod axle both sides axial plane is processed with an oil resevoir from top to down separately, step between pitch change axes bearing installation position, top and main shaft polished rod axial plane is the mounting limit step of pitch change axes bearing inner sleeve lower port, polished rod shaft portion above pitch change axes bearing mounting limit step is the installation site of pitch change axes bearing inner sleeve, top is slightly thin thread rod,

Two connection pawls that U-shaped connection pawl in pitch change axes takes the shape of the letter U down, bottom pitch change axes, U-shaped down connects between two connecting bores corresponding on pawl, be installed into a spherical plain bearing rod end nut and dock with a spherical plain bearing rod end bolt upper end forming displacement double end spherical plain bearing rod end, by penetrate one to be connected the isometric pitch change axes lower end connecting pins axle of connecting bore olo on pawl with pitch change axes U-shaped while, also through the upper end bearing hole connecting the double end spherical plain bearing rod end upper end of the displacement two connecting bores corresponding on pawl at U-shaped, displacement is connected with double end spherical plain bearing rod end upper end and is suspended on pitch change axes lower end U-shaped and connects two that pawl takes the shape of the letter U and connect between pawls,

Pitch change axes upper end penetrates in the pitch change axes mounting hole in the rotor shaft in inverted T-shaped from bottom to top, pitch change axes bottom U-shaped connect radix unguis portion bottom upper surface and pitch change axes main shaft between transition shoulder spacing by the limited step of the pitch change axes U-shaped pawl in rotor shaft main shaft root, the connecting pins axle two ends, pitch change axes lower end that pitch change axes lower end U-shaped connects between pawl are spacing by rotor shaft main shaft root circular shaft bore inwall, load pitch change axes main shaft polished rod axial plane part in the middle of rotor shaft and U-shaped connect the lower port of pre-and post perforative strip shape spacing hole between the step-like root of pawl and rotor shaft main shaft root front/rear end upper end corresponding near pre-and post perforative caging bolt hole, circular vertical shaft root place, and the strip spacing hole lower port penetrated by pitch change axes Limit screw in the pitch change axes in face, rotor shaft rear and front end and rotor shaft adds in case turn round and move up and down the spacing of amplitude to pitch change axes, loading the transverse axis center that on the pitch change axes lower end U-shaped connection pawl in the middle of rotor shaft, two corresponding connecting bore centers and rotor shaft main shaft root extend towards the left and right sides is that concentric arranges, connect the U-shaped being suspended on pitch change axes and to connect between pawl that the other end of double end spherical plain bearing rod end is sagging stretches out rotor shaft bottom,

The pitch change axes bearing installation position part axis body penetrating the pitch change axes top of rotor shaft from bottom to top stretches out from rotor shaft upper end for connection displacement cantilever;

The horizontal axle sleeve of rotor shaft is the round sleeve that two termination external process have raised annular limited step, the horizontal endoporus of axle sleeve of rotor shaft is identical near the light over glaze diameter of main shaft root portion with the lateral shaft of the rotor shaft both sides of inverted T-shaped, is socketed on the lateral shaft of inverted T-shaped rotor shaft both sides with the horizontal axle sleeve bottom protrusion annular stop step one end of rotor shaft towards the mode inside rotor shaft main shaft root;

The connection of rotor shaft main body and clamping plate type propeller hub is protruded upward from trepanning in the double-range ball bearing at clamping plate type propeller hub center by the screwed upper end of its vertical shaft part by rotor shaft, double-range ball bearing limited step in rotor shaft is by spacing towards lower port for the double-range ball bearing inner sleeve at clamping plate type propeller hub center, rotor shaft vertical shaft stretches out the double-range ball bearing inner sleeve threaded end upwards at clamping plate type propeller hub center, fix double-range ball bearing inner sleeve upper port by rotor shaft upper end locking nut, rotor shaft is connected with the clamping plate type propeller hub of fixing double-range ball bearing;

In rotor shaft, protrude upward the termination, pitch change axes bearing installation position, pitch change axes upper end at rotor shaft top, be used for being connected with displacement cantilever;

Displacement cantilever is one and has the symmetrical bearing seat stretching out two cantilevers below two skew backs, the cantilever termination of stretching out to both sides is processed with downward tapped bore, the bolt hole of two cantilever terminations at right angle setting displacement spherical plain bearing rod end screw rod from bottom to top separately, bearing seat between its two cantilevers is provided with a pitch change axes bearing mounting hole, pitch change axes bearing mounting hole periphery has the bolt connecting hole of pitch change axes bearing flange, pitch change axes bearing mounting hole lower port has the limited step of pitch change axes bearing outside lower port, after pitch change axes bearing is fit into the pitch change axes bearing mounting hole in displacement cantilever centre, by the top of displacement cantilever center pitch change axes bearing mounting hole, a pitch change axes bearing flange be installed and be connected and fixed by pitch change axes bearing flange tie bolt, the pitch change axes bearing inner sleeve being arranged on displacement cantilever centre is socketed in pitch change axes from the top down and stretches out on the pitch change axes bearing installation position of the upper end of rotor shaft, pitch change axes bearing inner sleeve lower port is spacing by the step between the pitch change axes bearing installation position on pitch change axes top and the main shaft polished rod axle of pitch change axes, after the slightly thin thread rod in pitch change axes top stretches out pitch change axes bearing inner sleeve upper port, be locked by pitch change axes upper end captive nut, the oblique front side that the displacement spherical plain bearing rod end screw rod that two cantilever terminations of displacement cantilever are installed overhangs displacement oscillating bearing position on clamping plate type propeller hub respectively to,

3) the rotor connection part described in is waved buffer shaft nut by rotary wing changing form apart from pole socket, rotor, rotor clamping plate, rotor check screw, rotor;

Rotor clamping plate are one group of horizontal use with two pieces and the L-shaped strip shape connecting cleat of main body outward appearance, for being connected vertical between the upper and lower end face of each termination of clamping plate type propeller hub and the upper and lower end face of rotor, every group leader's bar shaped clamping plate are made up of clamping plate type propeller hub connection end and rotor connection end two parts, correspondingly on the vertical bar shaped end face of wherein rotor connection end part be processed with the bolt mounting holes connecting rotor, clamping plate type propeller hub connection end waves the installation axle hole of buffer shaft two-thread screw except possessing the rotor pitch change axes corresponding with clamping plate type propeller hub and rotor, and have the correspondence of face toward the outer side extend one less of installing the strip connecting arm of a rotary wing changing apart from pole socket,

Rotary wing changing is main body apart from pole socket is strip and block, the strip connecting arm area that main body upper and lower end face area and rotor clamping plate extend laterally is suitable, its height and rotor waves buffer shaft stage casing axle sleeve two ends Flat-end and the spacing that is arranged between displacement oscillating bearing inner covering two the external end head end faces in displacement oscillating bearing is contour, and upper and lower end face is processed with the corresponding bolt connecting hole of the strip connecting arm of organizing rotor clamping plate with each and is bolted to be supported on often to be organized between strip connecting arm corresponding on rotor clamping plate, at rotary wing changing apart from pole socket end face centre toward the outer side, there is the displacement spherical plain bearing rod end screw flight pipe link for being mounted on displacement cantilever termination stretched out outside Xiang Yigen,

The upper and lower end face correspondence of each termination of clamping plate type propeller hub installs one group of rotor clamping plate, often organize the upper and lower being arranged on the upper and lower end face of clamping plate type propeller hub termination between two pieces of clamping plate type propeller hub connection ends in the rotor clamping plate be arranged above and below respectively, often organizing the mounting hole of the rotor pitch change axes on rotor clamping plate front end and rotor, to wave the mounting hole of buffer shaft corresponding with the axis hole that the mounting hole of the rotor pitch change axes on the every one end of clamping plate type propeller hub and rotor wave round sleeve two ends, buffer shaft stage casing, the spindle nose that each rotor waves the double-threaded screw bar axle of buffer shaft waves axle sleeve two ends, buffer shaft stage casing through the rotor that the every one end of clamping plate type propeller hub rotor clamping plate is installed and the threaded shank portion of double-threaded screw bar spindle nose two ends is stretched out from often organizing rotor clamping plate end face and down upward, then wave buffer shaft nut by rotor to be connected and fixed,

Often organize the rotor being all subject to every one end of clamping plate type propeller hub of rotary wing changing distance pole socket and correspondence thereof is installed between rotor clamping plate to wave buffer shaft stage casing axle sleeve two ends Flat-end and be arranged on the common support of displacement oscillating bearing inner covering two the external end head end faces in displacement oscillating bearing;

The rotary wing changing of bolt shank from the upper surface rotor clamping plate being positioned at clamping plate type propeller hub as rotor pitch change axes penetrates apart from axis hole, through two displacement oscillating bearing inner coverings opposed in trepanning in displacement oscillating bearing in clamping plate type propeller hub, the rotary wing changing of bolt shank lower end from the lower surface rotor clamping plate being positioned at clamping plate type propeller hub as rotor pitch change axes passes apart from axis hole, and fixed apart from spindle nut by rotary wing changing

Displacement buffering gum cover diameter be greater than propeller hub face combines with lower propeller hub face external end head after thickness be still slightly less than between the thicker external end head end face of displacement oscillating bearing inner covering two in the spherical joint inner sleeve of two opposed insertion displacement oscillating bearings and spacing, be less than too and be arranged on that displacement oscillating bearing inner covering two external end head end faces in displacement oscillating bearing are contour and rotor that is common support rotor clamping plate waves spacing between the Flat-end of axle sleeve two ends, buffer shaft stage casing, point centered by the outer spherical inner sleeve of the displacement oscillating bearing that the rotor clamping plate of connection rotor can be connected by rotor pitch change axes, thus leeway rotor being had wave up and down,

Apart from pole socket, end-face helical pipe link termination is corresponding toward the outer side with being fixed on the rotary wing changing often organizing between strip connecting arm corresponding to rotor clamping plate for the ball-and-socket joint endoporus being arranged on two the displacement spherical plain bearing rod end screw rod lower ends sagging to front, clamping plate type propeller hub oblique side, displacement cantilever two ends, rotary wing changing apart from pole socket toward the outer side end-face helical pipe link termination through be arranged on two the displacement spherical plain bearing rod end screw rod lower ends sagging to its front upper place, displacement cantilever two ends ball-and-socket joint endoporus and after stretching out, and fixed apart from the pole socket threaded shank portion of nut to the ball-and-socket joint bore section stretching out displacement spherical plain bearing rod end screw rod lower end that whorl brace rod termination is mated toward the outer side by rotary wing changing,

The rotor connection end of rotor clamping plate is arranged on the two sides up and down of rotor with the end face correspondence of rotor tie bolt mounting hole, and after being connected and fixed by rotor check screw, is connected respectively by two groups of rotors with clamping plate type propeller hub two terminations.

4. single manual cyclogyro according to claim 1, is characterized in that described rotor shaft cantilever structure of verting is made up of vert base holder portion, anteversion and retroversion rotation mechanism, displacement return mechanism part of left and right;

1) base holder portion that verts of the left and right described in is made up of lateral tilting rotating shaft, lateral tilting rotating shaft axle sleeve, the pedestal front frame that verts, the pedestal after poppet that verts, the pedestal left and right clamping plate that vert, the clamping plate studdle that verts, the clamping plate studdle captive nut that verts, vert pedestal clamping plate and the tie bolt of base seat support of verting, displacement reset tension spring spacing limit shaft sleeve, displacement reset tension spring, the pedestal left and right clamping plate tie bolt that verts that has bracing wire adjusting base concurrently;

Lateral tilting rotating shaft main body is square bulk and the polished rod spindle nose of two concentrics is stretched out at center, face, rear and front end to two ends, the width of the gap ratio fuselage column front/rear end between lateral tilting rotating shaft left and right sides end face is slightly wide, the side end face, two, left and right of lateral tilting rotating shaft is all processed with one up and down between two row bolts hole and the two row bolts hole sunk coak laterally processed be connected with the cantilever that verts about clamping plate type, the outside face of the polished rod spindle nose of lateral tilting rotating shaft is socketed with termination, one end external process separately and becomes raised annular limited step and center is processed with the lateral tilting rotating shaft axle sleeve with the polished rod spindle nose equal diameter centre hole of lateral tilting rotating shaft, lateral tilting rotating shaft axle sleeve is socketed on the polished rod spindle nose of the lateral tilting rotating shaft that center, face, lateral tilting rotating shaft rear and front end is stretched out with one end of protruding limited step towards the form in face, lateral tilting rotating shaft rear and front end, be socketed in left and right vert the protruding limited step of lateral tilting rotating shaft axle sleeve on polished rod spindle nose towards front and back outer face between spacing between spacing with fuselage column front/rear end identical,

Vert pedestal front frame and the pedestal after poppet that verts is that two pieces of upper ends are semicircular end and centered by the center of circle of semicircular end-face, are processed with the mounting hole of lateral tilting rotating shaft axle sleeve and the lower end width strip shape plate identical with the left and right spacing width of fuselage column front/rear end, vert pedestal front frame forward strip shape plate end face the latter half and pedestal after poppet strip shape plate end face the latter half backwards of verting on be processed to long recess, vert pedestal front frame end face forward and vert in the recess sidewall of pedestal after poppet end face backwards, correspondence is processed with the tie bolt mounting hole of the pedestal left and right clamping plate that vert,

The pedestal front frame that verts one in front and one in back is placed on the front/rear end on fuselage column top with the form that pedestal after poppet stretches out upper surface, fuselage column top with its upper end semicircular end part respectively of verting, vert pedestal front frame and the mounting hole at upper end semicircular end center between pedestal after poppet that verts is that concentric arranges, two spindle noses that two ends is socketed with the lateral tilting rotating shaft of lateral tilting rotating shaft axle sleeve are installed into the mounting hole at vert pedestal front frame and semicircular end center, pedestal after poppet upper end of verting respectively, lateral tilting rotating shaft is connected and is supported on above vert pedestal front frame and the fuselage column that verts between pedestal after poppet,

The pedestal left and right clamping plate that vert are two pieces of connecting cleats with the symmetry towards back boom, on the right opposed left and right end face being arranged on fuselage column top of one the first from left, vert clamping plate front end, pedestal left and right and middle part surface is processed with the tie bolt mounting hole corresponding with the pedestal front frame that verts on the front/rear end being placed in fuselage column top, pedestal after poppet side of verting, and every block to vert in the middle of pedestal left and right clamping plate cantilever backward with the mounting hole of a distance-variable rocker arm lateral shaft lining and is processed with the mounting hole of the clamping plate studdle that verts in cantilever follower head position;

The clamping plate studdle that verts is the double-threaded screw bars of two two ends with limited support step, the clamping plate studdle two ends limited support step that verts is identical with the width of the distance between left and right of fuselage column front/rear end, vert the two ends thread rod of clamping plate studdle for penetrating the mounting hole of the clamping plate studdle that verts verted on pedestal left and right clamping plate two cantilever follower heads, clamping plate studdle two ends of verting are supported verting between pedestal left and right clamping plate two cantilever terminations backward with limited support step, pedestal left and right clamping plate end face outside of verting is stretched out in the vert thread rod termination of clamping plate studdle, and fixed by the captive nut of the clamping plate studdle that verts,

Vert pedestal front frame, vert pedestal after poppet, verting between the clamping plate of pedestal left and right can be connected to each other with the tie bolt of the base seat support that verts by the pedestal left and right clamping plate that vert is fixed on the end face of four, fuselage column top, vert after the front end that has the pedestal left and right clamping plate tie bolt that verts of bracing wire adjusting base concurrently by one between the bolt hole corresponding with bottommost on the pedestal left and right clamping plate that vert of both sides, pedestal front frame front end face recess sidewall bottom inserts to the right on the left of fuselage column and be connected and fixed, the follower head having the pedestal left and right clamping plate tie bolt that verts of bracing wire adjusting base concurrently is thicker, thereafter termination by under a hollow bracing wire adjusting screw(rod) is installed upward,

To vert between the bolt hole corresponding with bottommost on the pedestal left and right clamping plate that vert of both sides, pedestal after poppet aft end face recess sidewall bottom when penetrating the pedestal left and right clamping plate that vert and being connected with the tie bolt of the base seat support that verts, it is the displacement reset tension spring spacing limit shaft sleeve of hollow thin-wall pipe spreader by a main body, be placed in and vert between the bolt hole of pedestal after poppet groove bottom on two sidewalls, displacement reset tension spring spacing limit shaft sleeve two ends and vert between pedestal after poppet groove two sidewalls and keep certain interval, this gap is for installing the lower end of two two ends with the displacement reset tension spring of loop-hook, and fixed spacing to the loop-hook of displacement reset tension spring lower end,

The pedestal left and right clamping plate that vert are installed by its cantilever termination and are connected displacement return mechanism;

2) the displacement return mechanism described in is made up of distance-variable rocker arm, distance-variable rocker arm lateral shaft lining, displacement shifting fork bar, displacement shifting fork bar spline, horizontal pitch change axes captive nut, distance-variable rocker arm pin axle;

Distance-variable rocker arm is the double end rocking arm of a horizontal use, a rectangular through holes is processed with between rocking arm main body upper and lower end face, rocking arm main body is made to form a strip shape square frame, distance-variable rocker arm using strip shape square frame both sides strip plate face as rocking arm end face, the follower head in distance-variable rocker arm strip plate face and midway location respectively have two to stretch out circular lateral shaft to both sides correspondence level, the slightly thin lateral shaft in distance-variable rocker arm follower head position is crossed strip resetting shaft, two spindle noses of crossed strip resetting shaft run through the strip plate surface rear end head left and right sides of strip shape square frame both sides, spindle nose end is respectively processed with a ring annular groove, and to be used for mounting two two ends spacing to it with the upper end of the displacement reset tension spring of loop-hook,

What outside two strip plate faces of the strip shape square frame distance-variable rocker arm, middle part was stretched out to both sides is horizontal pitch change axes, horizontal pitch change axes root is slightly thick, main body is polished rod axle, shaft end is comparatively thin and be processed with screw thread, thinner shaft end and thicker root are processed with transition shoulder, wherein the polished rod shaft portion of the horizontal pitch change axes in left side compares the horizontal pitch change axes slightly length of opposite side, it compares the slightly longer part polished rod axle of the horizontal pitch change axes of opposite side towards on the surface of front end, be processed with one for being connected and fixed the installation groove of the horizontal pitch change axes spline of displacement shifting fork bar, near the position in horizontal pitch change axes front, correspondence is processed with the mounting hole of the distance-variable rocker arm pin axle that is connected for the double end spherical plain bearing rod end lower end ball-and-socket joint axis hole of same pitch change axes lower end connecting pins axle connection,

The lower end of the double end spherical plain bearing rod end lower end ball-and-socket joint that pitch change axes lower end connects injects in the strip shape square frame of distance-variable rocker arm hollow, by the distance-variable rocker arm pin axle of the two ends length polished rod axial plane identical with the spacing of the strip shape square frame lateral surface of distance-variable rocker arm hollow while the strip plate face, strip shape square frame both sides through distance-variable rocker arm hollow, also simultaneously through double end spherical plain bearing rod end lower end axis hole and connect and be fixed in the strip shape square frame of distance-variable rocker arm hollow;

Distance-variable rocker arm lateral shaft lining is that two bottoms are with protruding outer ring step and the isodiametric round sleeve of horizontal pitch change axes polished rod axle of interior axis hole and distance-variable rocker arm both sides, the distance-variable rocker arm lateral shaft liner sleeve length horizontal pitch change axes polished rod partial-length shorter with distance-variable rocker arm is identical, distance-variable rocker arm lateral shaft lining is socketed in the horizontal pitch change axes of distance-variable rocker arm both sides in its protruding outer ring step mode to the inside, bottom it, ring-shaped step termination is to the inside close on distance-variable rocker arm strip shape square frame outer wall, distance-variable rocker arm pin axle two ends are limited in distance-variable rocker arm strip shape square frame, distance-variable rocker arm lateral shaft lining towards both sides ring-shaped step outer face between spacing and the both sides of fuselage column front/rear end width identical, distance-variable rocker arm lateral shaft lining towards the external end head of both sides end face between spacing be arranged on the fuselage column end face left and right sides vert pedestal left and right clamping plate towards outside end face between width spaces identical,

When being arranged on the pedestal left and right clamping plate that vert on fuselage column top, vert pedestal front frame, when the pedestal after poppet that verts connects, distance-variable rocker arm with its one end with crossed strip resetting shaft backwards and overall horizontal form is installed between two cantilevers that two pieces of pedestal left and right clamping plate that vert extend to fuselage column rear, in the middle of distance-variable rocker arm, two are socketed with the horizontal pitch change axes spindle nose end of distance-variable rocker arm lateral shaft lining, protruding from the mounting hole of two pieces of distance-variable rocker arm lateral shaft linings pedestal left and right clamping plate cantilever backwards that vert respectively, the distance-variable rocker arm lateral shaft lining outer face that distance-variable rocker arm both sides are socketed in horizontal pitch change axes flushes with the pedestal left and right clamping plate outer face that verts after penetrating the distance-variable rocker arm lateral shaft bush hole of verting on the clamping plate cantilever of pedestal left and right, longer this one end polished rod shaft portion of horizontal pitch change axes on the left of distance-variable rocker arm is after stretching out the pedestal left and right clamping plate outer face that verts, to be arranged in the displacement shifting fork bar termination of installing from the left-external side of the pedestal left and right clamping plate that vert in axis hole in the way to insert,

Displacement shifting fork bar is the cantilever that a left-external side from the pedestal left and right clamping plate that vert is installed, its front end free end headband has the displacement bracing wire of U-shaped to connect pawl, termination side straps is fixed in rear end has the axis hole identical with the polished rod axle external diameter of horizontal pitch change axes longer on the left of distance-variable rocker arm and the installation groove accordingly with horizontal pitch change axes spline forward, displacement shifting fork bar connects the termination of pawl towards fuselage column front with the displacement bracing wire of U-shaped, connecting spacing horizontal pitch change axes spline insertion displacement shifting fork bar rear end as radial direction fixes in spline groove corresponding between axis hole with pitch change axes horizontal on the left of distance-variable rocker arm in termination,

The horizontal pitch change axes two ends threaded portion of distance-variable rocker arm is stretching out on vert pedestal left and right clamping plate outer face and displacement shifting fork bar after axis hole respectively, fixed respectively by two horizontal pitch change axes captive nuts, displacement shifting fork bar distance-variable rocker arm and outside thereof connected is arranged on the cantilever that two pieces of pedestal left and right clamping plate that vert extend to fuselage column rear in horizontal mode;

Distance-variable rocker arm defines between the spindle nose of crossed strip resetting shaft and the distance-variable rocker arm pin axle near horizontal pitch change axes front position and is mounted on distance-variable rocker arm both sides two Length discrepancy lever arm of force that the horizontal pitch change axes of verting on the clamping plate of pedestal left and right is a dot center, wherein the spacing of distance-variable rocker arm rear end crossed strip resetting shaft and horizontal pitch change axes is equivalent to horizontal pitch change axes and the several times near spacing between the distance-variable rocker arm pin axle below it, lever arm of force as by the horizontal pitch change axes of distance-variable rocker arm a centered by fulcrum same with the displacement shifting fork bar that termination on the left of the horizontal pitch change axes on distance-variable rocker arm links together, its lever length is the several times of the lever arm of force between the horizontal pitch change axes on distance-variable rocker arm to the lever arm of force and horizontal pitch change axes to distance-variable rocker arm pin axle of crossed strip resetting shaft spindle nose,

The loop-hook of two displacement reset tension spring lower ends is connected to pedestal after poppet aft end face groove bottom of verting, two displacement reset tension spring upper end loop-hooks are connected on the crossed strip resetting shaft of distance-variable rocker arm rear end, two displacement reset tension springs, under the effect of autogenous shrinkage pulling force, remain the distance-variable rocker arm pin thrust axially to connecting double end spherical plain bearing rod end lower end axis hole in distance-variable rocker arm;

The same side being arranged on displacement shifting fork bar vert pedestal front frame front lower end on have bracing wire adjusting base concurrently the hollow bracing wire adjusting screw(rod) centre hole installed of the pedestal left and right clamping plate tie bolt root that verts and the displacement bracing wire of the U-shaped on displacement shifting fork bar to connect pawl corresponding, the end of displacement bracing wire is through this hollow bracing wire adjusting screw(rod) centre hole, and the displacement bracing wire being connected to the U-shaped on displacement shifting fork bar connects on pawl;

3) the anteversion and retroversion rotation mechanism part described in is made up of the cantilever that verts about clamping plate type, left and right cantilever rear end bracing frame, left and right cantilever rear end bracing frame tie bolt, rotor shaft arm, rotor shaft lateral shaft stage casing spline, rotor shaft vert cantilever bolt of rear end plate, the pull bar that verts of arm captive nut, left and right that vert that vert that vert that vert;

Vert pedestal front frame with vert pedestal after poppet by the connection with the pedestal left and right clamping plate that vert lateral tilting rotating shaft connected be supported on above fuselage column time, lateral tilting rotating shaft is all connected with the cantilever that verts about clamping plate type with the sunk coak of the bolt hole connected corresponding to the cantilever that verts about clamping plate type with transverse direction by two side end faces about it;

The cantilever that verts about clamping plate type is two pieces of edge-on uses of transverse direction and the oblong strip board of symmetry, the side surface of side surface and lateral tilting rotating shaft main body is between the upper and lower apart from wide, two pieces of strip board front ends are the connection end of lateral tilting rotating shaft, except being processed with the bolt connecting hole corresponding with side, lateral tilting rotating shaft main body both sides at side surface on connection end, and on the inner surface corresponded to each other, be processed with the horizontal tenon step that sunk coak horizontal with lateral tilting rotating shaft main body both sides is corresponding and isometric, the side surface middle position center of strip board rear end cantilever is provided with the mounting hole of the horizontal axle sleeve of rotor shaft, and near this termination along mounting hole cross cut end (of a beam) upper-lower position being processed with about two the cantilever rear end bracing frame tie bolts that vert,

The cantilever that verts about clamping plate type is inwardly connected and fixed the two with the form of clamping plate from lateral tilting rotating shaft and rotor shaft both sides, the cantilever that verts about clamping plate type utilizes the horizontal tenon step of its front end connection end inner surface to embed in the horizontal sunk coak in lateral tilting rotating shaft main body both sides, and bolt connecting hole corresponding with side, lateral tilting rotating shaft main body both sides for cantilever front end of verting about clamping plate type is connected and fixed by the cantilever bolt of rear end plate that verts about utilizing, cantilever front end of verting about clamping plate type is mounted on lateral tilting rotating shaft both sides, the left and right sides end distance ratio of the square block-shaped main body of lateral tilting rotating shaft verts pedestal front frame, the pedestal after poppet end face that verts is slightly wide, the end face part that the cantilever that verts about making the two clamping plates formula be connected with lateral tilting rotating shaft oblong block-shaped main body both sides is downward and vert and keep certain between the end face of pedestal after poppet side left and right and vert gap,

The cantilever that verts about two clamping plates formula utilizes the horizontal axle sleeve mounting hole of the rotor shaft of its rear end central authorities to be socketed in rotor shaft from rotor shaft both sides to stretch out to both sides and be set with the lateral shaft of the horizontal axle sleeve of rotor shaft, annular stop step also identical with the width of lateral tilting rotating shaft front/rear end towards width between end face outside of the horizontal axle sleeve projection of rotor shaft on the lateral shaft being arranged on rotor shaft both sides, vert about the outer face of rotor shaft horizontal axle sleeve raised annular limited step supports two clamping plates formula cantilever inner side end, vert after cantilever about rotor shaft lateral shaft cover penetrates two clamping plates formula, the end face of the horizontal axle sleeve of two rotor shaft side outwardly flushes with the cantilever outer face that verts about two clamping plates formula,

Two lateral shaft stage casings of rotor shaft are protruding from the horizontal axle sleeve mounting hole of rotor shaft of cantilever rear end central authorities of verting about clamping plate type with the polished rod shaft portion of spline and end thread bar part, vert about clamping plate type the left and right of termination, cantilever rear end vert cantilever rear end bracing frame tie bolt mounting hole between, clamp one piece of vertically-arranged and use and vert in the left and right of the square plate bulk identical with lateral tilting rotating shaft front/rear end length and width cantilever rear end bracing frame, left and right bracing frame both sides, the cantilever rear end end face that verts is processed with the bolt connecting hole corresponding with the cantilever follower head that verts about clamping plate type, utilize left and right vert cantilever rear end bracing frame tie bolt is verted in left and right cantilever rear end bracing frame clamp be fixed on clamping plate type about vert between termination, cantilever rear end,

The left and right cantilever rear end bracing frame that verts verts the rear of rotor shaft main shaft root aft end face between cantilever about being installed in two clamping plates formula equally, and maintains the spacing gap of verting before and after rotor shaft between rotor shaft root aft end face;

Vert about clamping plate type cantilever by with lateral tilting rotating shaft, rotor shaft, vert the connection of cantilever rear end bracing frame in left and right, vert on cantilever cantilever termination backwards about the clamping plate type propeller hub connect rotor shaft and rotor shaft upper end and rotor are fastened on clamping plate type, having of verting about clamping plate type that cantilever front end connects left and right laterally verts that the spindle nose axial line at lateral tilting rotating shaft front/rear end center of function is connected with cantilever rear end of verting about clamping plate type have before and after the central axis of longitudinal lateral shaft in the rotor shaft of function that verts contour and on intermediate point between the lateral shaft of giving rotor shaft root to stretch out to both sides mutually,

From the external end head part of two lateral shafts of the outwardly directed rotor shaft of the horizontal axle sleeve mounting hole of rotor shaft of cantilever rear end central authorities of verting about clamping plate type for and two symmetries be arranged on clamping plate type about the rotor shaft of verting outside cantilever rear end vert between arm and connected;

The rotor shaft arm that verts is two horizontal uses and two the oblique cantilevers of termination not in same plane, the rotor shaft arm rear end fixed end headband that verts has the mounting hole of rotor shaft lateral shaft, and rotor shaft mounting hole is processed with the groove installing rotor shaft lateral shaft stage casing spline towards direction, free termination, rotor shaft vert arm front end free end headband have U-shaped connect pawl, the rotor shaft of the every side of cantilever of verting about clamping plate type is verted between free termination that arm straps has the fixing termination of rotor shaft lateral shaft mounting hole to be connected pawl with U-shaped and is connected each via the connecting arm stretched out sideling to front lateral direction after,

The vert rotor shaft lateral shaft mounting hole of arm rear end of rotor shaft is socketed in polished rod axle outside the cantilever that to vert about rotor shaft lateral shaft stretches out clamping plate type and rotor shaft lateral shaft end thread bar part, and by rotor shaft lateral shaft stage casing spline insert from outside to inside rotor shaft lateral shaft and rotor shaft vert spline corresponding to arm spacing after, stretch out the vert rotor shaft lateral shaft end thread bar part of arm rear end mounting hole of rotor shaft to be fixed by the rotor shaft arm captive nut that verts, vert between cantilever about two of rotor shaft root lateral shaft outer ends are fastened on two clamping plates formula,

The vert U-shaped of arm front end of two rotor shaft connects pawl respectively from two side direction fuselage stud sides fronts of the cantilever that verts about two clamping plates formula to stretching out, the vert U-shaped of arm of two rotor shaft is connected pawl and is fastened on by bolt on the upper end spherical plain bearing rod end of two pull bars that vert of fuselage column both sides respectively, the pull bar that verts to be two main bodys be tubulose two ends with spherical plain bearing rod end, for the connecting rod of the clamping plate type hub tilting work of push-and-pull rotor shaft and connection thereof.

5. single manual cyclogyro according to claim 1, is characterized in that described full manual mechanism is by both hands control stalk mechanism and turn to combining mechanism to form;

1) the both hands control stalk mechanism described in by composition control rod base, U-shaped draw-in groove bolt of rear end plate, the rotating shaft of control stalk lateral tilting, the rotating shaft of control stalk anteversion and retroversion, T-shaped vert trailing arm, U-shaped control stalk mount pad, control stalk steering bearing, turn to connector loop, control stalk steering bearing captive nut, left control stalk, right control stalk, left and right control stalk bolt of rear end plate, brake transition bracing wire, displacement bracing wire to form;

The rotating shaft of control stalk lateral tilting is by the annular termination be connected, faying face and anticreep termination three part composition are reversed in left and right, annular termination, control stalk lateral tilting rotating shaft front end is the button-head that flat horizontal surface is processed in larger two side end faces, the flat end face center of control stalk lateral tilting rotating shaft annular termination is processed with one for installing the axis hole of control stalk anteversion and retroversion rotating shaft, the rotating shaft of control stalk anteversion and retroversion is a horizontal use and is used as bolt shank and the nut thereof of the flat end face center shaft of the annular termination of control stalk lateral tilting rotating shaft, control stalk lateral tilting rotating shaft stage casing is that to reverse the part of faying face as left and right be one section of polished rod axle, the axial line of polished rod axle axial line and side end face, annular termination central shaft hole intersects vertically, transition shoulder is processed with between annular termination and stage casing polished rod axle, anticreep termination be two from stage casing polished rod shaft end at right angles to the anticreep limiting stopper that bilateral symmetry lateral projection is stretched out, anticreep limiting stopper stretches out direction and becomes 90 degree with the axis hole direction at center, annular termination to both sides, the stage casing of control stalk lateral tilting rotating shaft and rear end are used for being arranged in control stalk pedestal with the form inserted,

Control stalk pedestal is a pedestal being connected and fixed the rotating shaft of control stalk lateral tilting, its main body is two inner side ends long strip-board shape column connecting arm composition in opposite directions that a block control stalk Connection Block of front end and the rear end level backward that is connected with it are stretched out, formed between the aft end face plane of control stalk Connection Block part and control stalk Connection Block part two long strip-board shape column connecting arms that level is stretched out backward and can block fuselage column front end face and left and right end face U-shaped draw-in groove, two long strip-board shape column connecting arm ends omit the corresponding connecting bore being processed with two U-shaped draw-in groove bolt of rear end plates between long and longer end section than fuselage column left and right sides end face width, control stalk pedestal is stuck in from fuselage column front end face the top turning to linking pedestal that column stage casing is connected and fixed lateral support bar upper end backward, control stalk pedestal rear end stretch out two long strip-board shape column connecting arm ends between be connected and fixed by two U-shaped draw-in groove bolt of rear end plates, the control stalk lateral tilting rotating shaft axis hole longitudinally running through block control stalk Connection Block is processed with between the front/rear end of the control stalk Connection Block part of control stalk pedestal front end, before and after this axis hole, the end face of two sections is processed to different shapes, the axis hole end surface shape of control stalk lateral tilting rotating shaft axis hole front section is identical with the rear end end face that the control stalk lateral tilting shaft end left and right sides has two anticreep limiting stoppers, and the left and right sides of the leading portion axis hole of control stalk lateral tilting rotating shaft is processed with the corresponding long recess in the anticreep limiting stopper cross section protruding with two, control stalk lateral tilting rotating shaft rear end, the front segment length of control stalk pedestal front-end control bar lateral tilting rotating shaft axis hole and the polished rod axle in control stalk lateral tilting rotating shaft stage casing isometric, and the hindfoot portion of axis hole, in the position isometric with the polished rod shaft portion in control stalk lateral tilting rotating shaft stage casing, axis hole back segment by with spacing between the protruding anticreep limiting stopper end face outside of control stalk lateral tilting shaft end end face two for diameter, and with the anticreep limiting stopper of control stalk anteversion and retroversion shaft end anticreep termination towards the end face of control stalk anteversion and retroversion rotating shaft front end for plane, be processed into a larger circular shaft bore, a recessed step cutting pattern face is formed between this part circular shaft bore and axis hole leading portion, this recessed step cutting pattern face is used for after the rotating shaft of control stalk lateral tilting is inserted and reversed in addition spacing to the end face towards its annular termination of the protruding anticreep limiting stopper of control stalk lateral tilting shaft end two,

The annular end of control stalk lateral tilting rotating shaft is headfirst inserted in the control stalk lateral tilting rotating shaft axis hole of control stalk pedestal front end face backwards in anticreep termination, because the polished rod axle in control stalk lateral tilting rotating shaft axis hole leading portion and control stalk lateral tilting rotating shaft stage casing is isometric, transition shoulder end face between the annular termination of control stalk lateral tilting rotating shaft and its polished rod axle is close to control stalk pedestal front end face, control stalk lateral tilting rotating shaft stage casing polished rod axle axial plane combines with the control stalk lateral tilting rotating shaft axis hole leading portion inner hole wall of control stalk pedestal, the recessed step cutting pattern face that control stalk lateral tilting shaft end anticreep limiting stopper end face forward can be close to control stalk lateral tilting rotating shaft axis hole back segment is rotated, after in the control stalk lateral tilting rotating shaft axis hole that the rotating shaft of control stalk lateral tilting is inserted into control stalk pedestal front end face, the normal use angle turning 90 degrees and reach its design need be turned round in the annular termination of control stalk lateral tilting rotating shaft front end, and the protruding anticreep limiting stopper of control stalk lateral tilting shaft end two turn round turn 90 degrees after be positioned at the upper and lower of former insertion position, the protruding anticreep limiting stopper of control stalk lateral tilting shaft end two is in by the spacing state in the recessed step cutting pattern face of control stalk lateral tilting rotating shaft axis hole back segment, meet the work torsional amplitude of about the rotating shaft of normality lower control arm lateral tilting 8 degree, and make the rotating shaft of control stalk lateral tilting be unlikely to deviate from the control stalk lateral tilting rotating shaft axis hole of control stalk pedestal front end face, the control stalk anteversion and retroversion rotating shaft axis hole reversing the flat end face central authorities of annular termination, later control stalk lateral tilting rotating shaft front end towards control stalk pedestal both sides and for connecting T-shaped to vert trailing arm by being laterally fit into a bolt as the rotating shaft of control stalk anteversion and retroversion,

The T-shaped trailing arm that verts to be connected with U backward by a two ends and to stretch out downward vertically in the middle of the horizontal trailing arm of pawl and horizontal trailing arm and the control stalk steering shaft be connected forms, the vert control stalk axle of trailing arm of T-shaped becomes T-shaped profile with horizontal trailing arm, vert horizontal trailing arm two ends two U backward of trailing arm of T-shaped connect pawls respectively towards the both sides of fuselage column, T-shaped is verted and is provided with the lateral connection bolt hole of the pull bar lower end spherical plain bearing rod end that verts between the horizontal trailing arm two ends of trailing arm each U connection pawl backward, vert horizontal trailing arm two ends two U backward of trailing arm of T-shaped connect the spacing of pawl and two side direction fuselage columns, two rotor shaft, two U-shapeds verted on arm that lateral direction is stretched out forward of the cantilever that verts from about two clamping plates formula to connect spacing between pawl identical and corresponding up and down, what T-shaped verted that trailing arm two U backward connect respectively by the bolt rotor shaft be connected to above its same side correspondence, pawls vert that U-shaped on arm connects that pawl connects verts on pull bar lower end spherical plain bearing rod end, the vert termination, control stalk steering shaft upper end of trailing arm and horizontal trailing arm mesophase spherule of T-shaped links into an integrated entity, control stalk steering shaft stage casing is processed with one for being installed into the long trough through hole of flat, annular termination in the control stalk lateral tilting rotating shaft being torqued into normal use angle with the form of socket towards fore-and-aft direction, on the wall middle position of the long trough through hole left and right sides, correspondence is processed with one for penetrating by horizontal the axis hole that the rotating shaft of control stalk anteversion and retroversion comes end face center, annular termination in the rotating shaft of connection control bar lateral tilting, the vert control stalk steering shaft hypomere of trailing arm of T-shaped is grouped into by the polished rod shaft portion for inserting control stalk steering bearing and the hypomere tip thread rod part for connection control bar steering bearing captive nut,

The long trough through hole that T-shaped is verted on trailing arm is socketed on the annular termination of control stalk lateral tilting rotating shaft front end, T-shaped vert the control stalk anteversion and retroversion rotating shaft corresponding with on the flat end face in annular termination in the rotating shaft of control stalk lateral tilting of the two side of control stalk steering shaft stage casing long trough through hole of trailing arm axis hole between, after being passed by the bolt shank being used as the rotating shaft of control stalk anteversion and retroversion as, be connected and fixed with the same nut as a control stalk anteversion and retroversion rotating shaft part, T-shaped is verted trailing arm with the downward stateful connection of the threaded end of its control stalk steering shaft hypomere tip in the front of control stalk pedestal,

The T-shaped being connected to the front of control stalk pedestal vert trailing arm can vert using the control stalk anteversion and retroversion rotating shaft of its stage casing lateral connection as T-shaped trailing arm realize before and after the lateral shaft that verts, and T-shaped is verted, the trailing arm trailing arm that can vert using the polished rod axle of control stalk lateral tilting rotating shaft as T-shaped realizes the longitudinal axis that verts of left and right, is common center of verting using the axial line intersection point as the control stalk lateral tilting rotating shaft of longitudinal axis and the flat end face RC control stalk anteversion and retroversion rotating shaft that penetrates longitudinal axis control stalk lateral tilting rotating shaft annular termination as lateral shaft;

Be connected for the U-shaped control stalk mount pad installed by two control stalk steering bearings and its underpart as the vert control stalk steering shaft part of trailing arm hypomere of T-shaped;

U-shaped control stalk mount pad front appearance is U-shaped, above the bearing seat of the control stalk steering bearing used by vertically-arranged and the bearing seat left and right sides, two protruding corresponding engaging lugs form, the center, bearing seat upper and lower end face of control stalk steering bearing is processed with the mounting hole of the control stalk steering bearing running through upper and lower, control stalk steering bearing mounting hole inwall stage casing is processed with the limited step of the control stalk steering bearing of inside annular protrusion, above the bearing seat both sides of control stalk steering bearing, on two corresponding engaging lugs, correspondence is processed with the axis hole that is installed left control stalk and right control stalk separately, axis hole between two engaging lugs is that concentric is transversely arranged, the all corresponding mounting hole being processed with about two control stalk bolt of rear end plates in both sides before and after the axis hole wall of every side engaging lug, U-shaped control stalk mount pad two engaging lugs are used for the corresponding end installing fixing left control stalk and right control stalk, and use left and right control stalk bolt of rear end plate to be fixed through the end of U-shaped control stalk mount pad two engaging lugs to left control stalk and right control stalk,

Two control stalk steering bearings are installed into the mounting hole of control stalk steering bearing from the two ends up and down of U-shaped control stalk mount pad respectively, between the bearing outside of two control stalk steering bearings, end face is in opposite directions stuck in the both ends of the surface up and down of the limited step of the control stalk steering bearing of the mounting hole stage casing annular protrusion of control stalk steering bearing, after the bearing inner sleeve hole of two control stalk steering bearings is socketed in the control stalk steering shaft hypomere termination that T-shaped verts on trailing arm from bottom to top, the vert threaded end of the control stalk steering shaft hypomere tip on trailing arm of T-shaped stretches out downwards from the bearing inner sleeve hole of two control stalk steering bearings and is fixed by control stalk steering bearing captive nut, U-shaped control stalk mount pad is connected to T-shaped to vert the bottom of trailing arm, axial line between the engaging lug that two, both sides, U-shaped control stalk mount pad upper end are transversely arranged in concentric, contour with the vert axial line of control stalk anteversion and retroversion rotating shaft that trailing arm installs through control stalk lateral tilting rotating shaft annular side end face, termination central shaft hole of T-shaped, two, both sides, U-shaped control stalk mount pad upper end engaging lug and the T-shaped trailing arm that verts is made to have the common center-point that verts all around, and U-shaped control stalk mount pad can vert the downward control stalk steering shaft axle center of trailing arm for left and right center of twist with the T-shaped be attached thereto,

Left control stalk and right control stalk are the control stalk of two the body shape symmetries be arranged in engaging lug corresponding above U-shaped control stalk mount pad both sides, left control stalk and right control stalk rear end curve inwardly with arc level, left control stalk and right control stalk rear end tip all have and corresponding left and right control stalk bolt of rear end plate mounting hole on U-shaped control stalk mount pad engaging lug, left control stalk and right control stalk front end extend forward and lean out, left control stalk and right control stalk front end are respectively connected a handle bar bent respectively to front lower place, side, wherein the handle bar of right control stalk front end be provided with control engine speed can constant speed throttle, the handle bar upper end of left control stalk front end raises up on the termination of stretching out, with the form be arranged above and below, the hollow bracing wire adjusting screw(rod) of two terminations towards left control stalk front is housed, the hollow bracing wire adjusting screw(rod) that the handle bar upper end top position being positioned at left control stalk front end is installed is as brake transition bracing wire adjusting bolt, the hollow bracing wire adjusting screw(rod) that the handle bar upper end lower position being positioned at left control stalk front end is installed is as displacement bracing wire adjusting bolt, the wisp mounting groove waiting the U-shaped of brachium dual control wisp for being connected and fixed is stretched out before the handle bar stage casing of left control stalk front end is provided with one, the bolt connecting hole that a correspondence such as to be connected and fixed at the brachium dual control wisp is provided with between U-shaped wisp mounting groove both sides,

On the lever that brachium dual control wisp is the brachiums such as two ends, on conventional handle, wisp controls on the Length discrepancy lever construction basis of bracing wire, the intimate isometric arm of force will be designed to by the wisp part that holds controls with the resistance arm being connected and fixed bracing wire termination as power arm, bolt connecting hole corresponding between the wisp mounting groove both sides of U-shaped is provided with Deng in the middle of brachium dual control wisp, erect in the wisp mounting groove of the U-shaped be installed on the handle bar of left control stalk front end Deng in the middle of brachium dual control wisp with the part of bolt connecting hole, between the bolt connecting hole that brachium dual control wisp is corresponding with the wisp mounting groove both sides of the U-shaped on the handle bar of left control stalk front end, penetrated by a bolt as fulcrum shaft and be connected and fixed,

Using the power arm waiting brachium dual control wisp lower end wisp to control as driver with the form of holds, the handle bar upper end of resistance arm upper end towards left control stalk front end of bracing wire termination is fixed Deng brachium dual control wisp, owing to will connect brake transition bracing wire and displacement bracing wire as resistance arm upper end simultaneously, the transition bracing wire of wherein braking is the connecting stay wire between the brake wisp end head on the brachium dual control wisp upper ends such as connection and one drag two water brake pump, and displacement bracing wire is connect the displacement bracing wire connection pawl of displacement shifting fork bar front end U-shaped to the connecting stay wire waited between brachium dual control wisp upper end, because it is different that the wisp that during rotary wing changing distance, displacement shifting fork bar reaches the amplitude range of stirring needed for action effect and controls one drag two water brake pump reaches the amplitude range of moving needed for action effect, brake transition bracing wire termination and the displacement bracing wire termination of fixing the resistance arm upper end connection of bracing wire termination Deng brachium dual control wisp are respectively according to the difference of the size of its movable amplitude, be mounted on respectively using the form be arranged above and below and wait the top of termination, brachium dual control wisp upper end and the position of lower end, adjacent top as resistance arm,

Left control stalk and right control stalk are with arc level aduncate rear end tip, corresponding insertion respectively engaging lug axis hole above U-shaped control stalk mount pad both sides, and the mounting hole being each passed through the left and right control stalk bolt of rear end plate of the axis hole wall of U-shaped control stalk mount pad every side engaging lug by left and right control stalk bolt of rear end plate is fixed, left control stalk and right control stalk are separately fixed at above the U-shaped control stalk mount pad left and right sides, be arranged on the tiller grip that left control stalk above the U-shaped control stalk mount pad left and right sides and right control stalk stretch out forward, lay respectively at the front, the left and right sides of operator's saddle, lateral connection auxiliary control rod between the handle, at its lower end head that left control stalk and right control stalk stretch out forward,

Wherein left control stalk rear end tip be installed on the left of U-shaped control stalk mount pad engaging lug in before, need first to be inserted by left control stalk rear end tip after of being positioned at below U-shaped control stalk mount pad turn to the long trough connector loop upwards erect on the cantilever termination of connector loop, left control stalk rear end tip loads and installed again in the lateral of engaging lug on the left of U-shaped control stalk mount pad to be fixed;

Connector loop is turned to be that a fixed end headband has spindle nose mounting hole on the steering shaft that runs through up and down, the horizontal cantilever of the long trough connector loop that free end headband has upwards to erect, its overall side is L-shaped, the annular through-hole of the long trough connector loop turning to the free termination of connector loop upwards to erect is towards side, turn to the annular through-hole insied width of connector loop and left control stalk, right control stalk diameter is identical, lower-upper length in the annular through-hole of the long trough connector loop of connector loop is turned to be left control stalk, the several times of right control stalk diameter, turn to the elongated slot vias direction of the long trough connector loop on the free termination of connector loop towards side and vertical with the hole axis direction of spindle nose mounting hole on the steering shaft run through up and down on fixing termination, connector loop fixed end headband is turned to have the fixing termination of spindle nose mounting hole on steering shaft towards the below of the control stalk steering bearing mounting hole of U-shaped control stalk mount pad, the free termination of connector loop connector loop elongated slot through hole is upwards turned to be placed in the outside of U-shaped control stalk mount pad upper left side engaging lug and to be connected with left control stalk after penetrating via left control stalk end, turn to connector loop with the fixing termination of spindle nose mounting hole on steering shaft, by with the fixing of spindle nose upper end on steering shaft and be connected to turn to and be connected above pedestal,

2) described in turn to combining mechanism to turn to be above connected pedestal, spindle nose under spindle nose bearing spring card, central steering shaft, steering shaft on spindle nose bearing, steering shaft on spindle nose, steering shaft on steering shaft, steering shaft lower shaft head bearing, steering shaft lower shaft head bearing Spring Card, under turn to and be connected pedestal, one drag two water brake pump, column lower end connecting strap, turn to commutation shift fork, turn to commutation shift fork captive nut, front-wheel steering pull bar, empennage to turn to pull bar to form;

On turn to that to be connected Base body by a front end be that the bearing seat of spindle nose bearing on block steering shaft and the level backward that is connected with it are stretched out two inner side ends long strip-board shape column connecting arm in opposite directions and formed, on turn to and be connected pedestal and formed between two long strip-board shape column connecting arms stretching out of level backward and can block fuselage column front end face and left and right end face U-shaped draw-in groove, on turn to two long strip-board shape column connecting arm ends being connected pedestal slightly long and longer than fuselage column left and right sides end face end section between the corresponding connecting bore being processed with two U-shaped draw-in groove bolt of rear end plates, on turn to be connected pedestal be stuck in fuselage column front end face and left and right end face backward, on turn to and be connected between pedestal two long strip-board shape column connecting arm ends, after being connected by U-shaped draw-in groove bolt of rear end plate by turn to and be connected pedestal and be fixed on the below of control stalk pedestal on fuselage column, on turn to the back being connected the front end face of pedestal and being close to operator's saddle oil tank type backrest top, on turn to be connected pedestal front end steering shaft on the front end surface of spindle nose bearing seat be provided with the bolt connecting hole corresponding with operator's saddle oil tank type backrest top and linked together by bolt and operator's saddle,

On turn to be connected pedestal front end steering shaft on the front end of bearing seat of spindle nose bearing run through the mounting hole being processed with spindle nose bearing on a steering shaft up and down, on steering shaft, the mounting hole upper port of spindle nose bearing is processed with the draw-in groove of spindle nose bearing spring card on steering shaft and lower port is provided with the limited step of spindle nose bearing outer shaft lower surface on steering shaft, above turns to be connected pedestal front end and to be each side provided with the U-shaped engaging lug that is used for being connected and fixed by penetrating bolt the lateral support bar upper end of the fuselage column left and right sides;

On the steering shaft that on steering shaft, spindle nose bearing is arranged on the bearing seat of spindle nose bearing on the steering shaft that turns to and be connected pedestal front end from top to bottom spindle nose bearing mounting hole in, on the steering shaft that on steering shaft, the outer face upper surface of the outer bearing sleeve of spindle nose bearing is installed in the mounting hole upper port draw-in groove of spindle nose bearing on steering shaft by, spindle nose bearing spring card is in addition spacing;

On steering shaft, spindle nose is one and erects the hollow tubular that uses and centre is processed with the double end polished rod axle of annular protrusion limited step, its upper end tubular shafts is upwards inserted into and turns to connector loop with being fixed by bolt lateral connection in the termination of spindle nose mounting hole on steering shaft, on steering shaft, the lower end of spindle nose is inserted downwards and stretches out spindle nose bearing internal axle sleeve on steering shaft, in addition spacing to spindle nose bearing internal axle sleeve upper surface on steering shaft by the annular stop step on steering shaft in the middle of spindle nose, be horizontally through the two by bolt and be fixedly connected with in the central steering shaft upper port that the end portion that on steering shaft, spindle nose stretches out spindle nose bearing internal axle sleeve on steering shaft is downwards inserted into the hollow tubular that one, below is erect, central authorities steering shaft as one its upper end is connected turn to the left control stalk penetrated in connector loop about reverse strength by the transition axis be delivered to above fuselage column below fuselage column, central authorities' steering shaft lower port is fixed on down to turn to by being connected with spindle nose under a steering shaft and is connected above pedestal,

The T-shaped of spindle nose entirety in horizontal side under steering shaft, the double end polished rod vertical shaft of raised annular limited step is processed in the stage casing used by a setting and the annular stop step midway location of projection forms to the flat commutation shifting fork bar stretching out a polished rod of side transverse direction, laterally be fixed together by bolt after the upper spindle nose end that under steering shaft, spindle nose is erect upwards inserts central steering shaft lower port, the lower shaft head end that under steering shaft, spindle nose is erect is for installing in the steering shaft lower shaft head bearing inner sleeve being inserted in down and turning to and be connected and pedestal is installed downwards;

Under turn to be connected pedestal by a bearing seat being processed with vertical steering shaft lower shaft head bearing mounting hole and one through two engaging lugs corresponding to left and right below bearing seat and the transverse axis stretched out to both sides form, under turn to and be connected the left and right sides, pedestal rear and be provided with and fix with two panels fuselage column lower end connecting strap and be connected the bolt hole of use, and be bolted and be fixed between fuselage column lower end connecting strap;

Under turn to the lower port of the mounting hole of the steering shaft lower shaft head bearing be connected on pedestal to be provided with steering shaft lower shaft head bearing outer shaft lower surface limited step and upper port is processed with the draw-in groove of steering shaft lower shaft head bearing Spring Card, when the mounting hole of steering shaft lower shaft head bearing is after being fit into steering shaft lower shaft head bearing, the draw-in groove in the mounting hole of steering shaft lower shaft head bearing is installed into by a steering shaft lower shaft head bearing Spring Card, in addition spacing to the outer shaft upper surface of steering shaft lower shaft head bearing, be connected to the commutation shifting fork bar that spindle nose under the steering shaft of central steering shaft lower port crosses out with it to put towards left side, and the termination, bottom of spindle nose under steering shaft is arranged in the internal axle sleeve hole of steering shaft lower shaft head bearing downwards,

Under turn to and be connected the transverse axis that both sides, direction are stretched out under pedestal and be used for respectively brake transition bracing wire is installed, one drag two water brake pump and turn to commutation shift fork, under turn to be connected spindle nose end that pedestal lower right stretches out be equipped with one settle forward for installing the hollow bracing wire adjusting screw(rod) regulating brake transition bracing wire, under turn to be connected stretch out to the left below pedestal be one and turn to commutation declutch shift shaft, the root of commutation declutch shift shaft is turned to be provided with the mounting interface of one drag two water brake pump forward, commutation declutch shift shaft stage casing is turned to be polished rod axial plane, commutation declutch shift shaft end is outwardly turned to be processed into thread rod,

Turn to commutation shift fork and one drag two water brake pump to be all arranged on down and turn to turning to of the bearing seat lower left being connected pedestal to commutate on declutch shift shaft, one drag two water brake pump is the brake wisp oil pump that a conventional atv motorcycle right hand handle uses and the water brake master cylinder that simultaneously can be controlled two water brakes pincers by shunt oil pipe, its mounting interface is mounted on down backward and turns to the bearing seat lower left being connected pedestal to turn on the mounting interface of the root one drag two water brake pump forward of commutation declutch shift shaft, the brake wisp end of one drag two water brake pump is towards the front, right side of fuselage column bottom, as oil pump lever brake wisp end head be arranged on down turn to the bearing seat lower right being connected pedestal to stretch out spindle nose on the hollow bracing wire adjusting screw(rod) of brake transition bracing wire installed corresponding, brake wisp end head be processed with the connection end of a brake transition bracing wire and be connected by the termination that brake transition bracing wire is corresponding with waiting brachium dual control wisp upper end,

Turn to commutation shift fork to be that a setting uses and be arranged on down the strip shape bipitch connecting rod turned on commutation declutch shift shaft turning to and be connected pedestal lower left from the side, turn to commutation middle, shift fork side have turn to commutation declutch shift shaft mounting hole and two ends be processed with towards fore-and-aft direction U-shaped connect pawl, turn to commutation shift fork upper end to be provided with a width near the position of U-shaped connection pawl to be enough to insert the long trough convergence hole that steering shaft lower shaft centriciput laterally puts down the commutation shifting fork bar termination of stretching out, this long trough convergence hole is broadened gradually by Inside To Outside and forms certain taper, turn to commutation shift fork on turning to commutation shift fork axis hole and long trough convergence hole perforate direction identical, turn to commutation shift fork by its middle have turn to commutation shift fork axis hole ecto-entad to be arranged on down to turn to the bearing seat lower left being connected pedestal turn on the polished rod axle of commutation declutch shift shaft stage casing while, turn to the long trough convergence hole on commutation shift fork also ecto-entad installation sleeve be connected on down on the commutation shifting fork bar crossed out to the left of spindle nose under the steering shaft turning to and be connected and install above pedestal, under turn to the commutation declutch shift shaft end thread termination that turns to being connected pedestal lower left turning to that commutation shift fork axis hole is to the left to be stretched out and by turning to the shift fork captive nut that commutates to be fixed from turning in the middle of commutation shift fork, the U-shaped of side direction in commutation shift fork two ends is turned to connect the front and back end of U-lag gap towards fuselage of pawl,

Turn to the upper end U-shaped of commutation shift fork connect pawl and steering front wheel axially left side stretch out steering front wheel axle steer arm between be bolted the front-wheel steering pull bar that self two ends is provided with shaft-like oscillating bearing, the empennage turning to the lower end U-shaped of commutation shift fork to connect to be provided with shaft-like oscillating bearing by being bolted self two ends between caudal wing shaft spindle arm that pawl and caudal wing shaft stretch out to the left turns to pull bar.