CN208036602U - Manned vehicle - Google Patents
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- CN208036602U CN208036602U CN201820338081.XU CN201820338081U CN208036602U CN 208036602 U CN208036602 U CN 208036602U CN 201820338081 U CN201820338081 U CN 201820338081U CN 208036602 U CN208036602 U CN 208036602U
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Abstract
The utility model provides a kind of manned vehicle, including aircraft body, and manned portion is provided on aircraft body, and the both sides of front end are provided with preceding duct, and the both sides of rear end are provided with rear duct, symmetric screw propeller is equipped in preceding duct and rear duct；The centre position of front end is equipped with the first auxiliary duct, and the first auxiliary propeller is equipped in the first auxiliary duct, and the internal diameter of the first duct is more than the internal diameter of preceding duct, and the peak power output of the first auxiliary propeller is more than the peak power output of symmetric screw propeller；The centre position for flying rear end is equipped with the second auxiliary duct, the second auxiliary propeller is installed in second auxiliary duct, the internal diameter of second duct is more than the internal diameter of rear duct, and the peak power output of the second auxiliary propeller is equal to the peak power output of the first auxiliary propeller.The aircraft, when meeting manned operation, power take-off demand simultaneously, in the case where there is lateral wind flight, is also not easy to increase the power needed when the influence for overcoming lateral wind to aircraft.
Description
Technical field
The utility model is related to field of aerospace technology, more particularly, to a kind of manned vehicle.
Background technology
With development in science and technology, no matter aircraft is widely used on military or civilian, is especially rescuing
The fields such as calamity is speedily carried out rescue work, crops spray, take photo by plane greatly facilitate people's lives, and therefore, development prospect can not despise；
Utility model patent " a kind of culvert type unmanned plane and its control method " (201610204096.2) discloses one kind
Culvert type unmanned plane with polymorphic stabilized flight and hovering ability, power is smaller when the unmanned plane of this structure takes off, no
Can meet the needs of manned operation, if the propeller of duct and its inside, which is done, can meet greatly manned job requirements, still
The area of aircraft both sides can greatly increase, in the case where there is lateral wind flight, when overcoming influence of the lateral wind to aircraft
The power needed greatly increases, and then considerably increases aircraft energy consumption, to greatly increase flight cost.
Utility model content
Therefore, the utility model provides a kind of manned vehicle, to solve the above problems.
The technical solution of the utility model is：A kind of manned vehicle, including aircraft body, on the aircraft body
It is provided with manned portion, the both sides of the front end of the aircraft body are provided with preceding duct, and the two of the rear end of the aircraft body
Side is provided with rear duct, and symmetric screw propeller is equipped in the preceding duct and the rear duct；The front end of the aircraft body
Centre position the first auxiliary duct is installed, the first auxiliary propeller is installed in the first auxiliary duct, described first
The internal diameter of duct is more than the internal diameter of the preceding duct, and the peak power output of first auxiliary propeller is more than the balance spiral shell
Revolve the peak power output of paddle；The centre position of the rear end of the aircraft body is equipped with the second auxiliary duct, and described second
Second auxiliary propeller 19 is installed, the internal diameter of second duct is more than the internal diameter of the rear duct, described in auxiliary duct
The peak power output of second auxiliary propeller is equal to the peak power output of first auxiliary propeller.
Optionally, it is provided with driver's cabin in the manned portion.
Optionally, the centre position of the front end of the aircraft body is vertically fixed the first fixed body, and described first is solid
Determine to be horizontally fixed with the second fixed body and third fixed body on body, second fixed body is parallel with the third fixed body to be set
It sets；The front end of the aircraft body is provided with the first driving body and the second driving body, and first driving body includes：First base
Bar, the first bending part, first connecting portion and second connecting portion, first base shaft, the first bending part, first connecting portion and second
What interconnecting piece was integrated, first bending part in first base shaft close to one end of first fixed body, described
One interconnecting piece and second connecting portion are located at the one end of first base shaft far from first fixed body, and first base shaft is hinged
In being provided with first hydraulic cylinder, the power of the first hydraulic cylinder on the front end of the aircraft body, second fixed body
Output end is connected with the first telescopic rod, and first telescopic rod connect with first bending part, cut with scissors in the second connecting portion
It is connected to the first crimp type terminal, train line is fixed on first crimp type terminal, first is fixed on first fixed body
Support；Second driving body includes：Second base shaft, the second bending part, third interconnecting piece and the 4th interconnecting piece, second base
What bar, the second bending part, third interconnecting piece and the 4th interconnecting piece were integrated, second bending part is leaned in second base shaft
One end of nearly first fixed body, the third interconnecting piece and the 4th connecting portion are in second base shaft far from described first
One end of fixed body, second base shaft are articulated with the front end of the aircraft body, and is provided on the third fixed body
The power output end of two hydraulic cylinders, the second hydraulic cylinder is connected with the second telescopic rod, second telescopic rod and described second
Bending part connects, and is hinged with the second crimp type terminal on the 4th interconnecting piece, the second support is fixed on the third fixed body
Frame；The front end of the aircraft body is additionally provided with penetration pipe, and the penetration pipe is supported by first supporting rack and second
Frame is fixed on the front end of the aircraft body, and the train line is fixed on across the penetration pipe on the second crimp type terminal；Institute
It states and is provided with the first connector and the second connector on the first auxiliary duct, first connector is located at first auxiliary and contains
The top in road, second connector are located at the bottom of first duct, first connector and the first connecting portion
Hinged, second connector is hinged with the third interconnecting piece.
Optionally, the one or both sides of the aircraft body are provided with automatically-controlled door, and appearance is provided on the inside of the automatically-controlled door
Between emptying, transmitting holder is installed in the accommodating space, the front end of the transmitting holder is provided with drive roll, the transmitting branch
The rear end of frame is provided with the first driven voller, and the second driven voller is provided between the drive roll and first driven voller, described
It is wound with multiple rubber nets on first driven voller, is connected by plastic ties between multiple rubber nets；The front end of the rubber net and
Rear end is both provided with Weight plate, and the edge of the rubber net is provided with plastic cloth bound edge, and the plastic cloth bound edge surrounds institute completely
State the grid of rubber net；
Position on the transmitting holder positioned at second driven voller both ends is equipped with Auxiliary support roller and limit roller, institute
It is hollow to state Auxiliary support roller, and surface is provided with multiple spray orifices, is internally provided with ignition, is set on the transmitting holder
It is equipped with oil pipe, piston engine is provided in the aircraft body, the piston engine is connect with the oil pipe；The hair
It penetrates the front end on holder positioned at the drive roll and is provided with guide plate, the guide plate is smooth.
Optionally, the bottom of the aircraft body is equipped with searchlight, human body temperature survey meter and locator.
Optionally, the one or both sides of the aircraft body are provided with two door-plates worked in coordination, and the door-plate is logical
It crosses first rotating shaft to be fixed on the aircraft body, warehouse is provided on the inside of the door-plate, is provided with and puts in the warehouse
Set plate, it is described to shelve tiling on plate and have rubber net；There are two driving device, two driving device positions for installation in the warehouse
In the both sides for shelving plate, the both sides of the front end of the rubber net are provided with drawstring, per side the drawstring with apart from the side
Closer driving device connection, the driving device include：Hollow pipe is fixed on the inside of the warehouse；Energy-storaging spring, it is fixed
In in hollow pipe, and positioned at the front end of hollow pipe；First sliding block is connect with the energy-storaging spring；Second sliding block is slided with first
Block contacts；Electric telescopic rod coordinates with second sliding block, so that energy-storaging spring is stored for driving the second sliding block to compress the first sliding block
Can, the electric telescopic rod of two driving devices moves synchronously；Power output rod, power output rod one end setting
There are the first bending section, one end that first bending section is not connect with the power output end to be stuck on second sliding block, institute
The one end for being provided with the first bending section for stating power output rod is fixed on by the second shaft in the warehouse, on the hollow pipe
It is provided with first through hole, is passed through for first bending section, the diameter of the first through hole is more than first bending section
Diameter；Turntable, the other end of the power output rod is fixed on by central shaft, and the turntable is protruded at the top of the central shaft
Top surface；Blade, is fixed on the top of the central shaft, and the blade includes horizontal part and vertical portion, the horizontal part and institute
Vertical portion connection is stated, the horizontal part is fixed on the central shaft；Column is fixed on the turntable, is located at the one of blade
Side, and the distance of the column to the central shaft is less than the vertical portion to the distance of central shaft, the height of the column
Higher than the vertical portion bottom and be less than the horizontal part, the drawstring is fixed on the column；Second bending section, it is described
Second bending section is fixed on the outside of the hollow pipe, the hollow pipe by being set to the third shaft on the outside of the hollow pipe
On be provided with the second through-hole, passed through for second bending section, the diameter of second through-hole is more than second bending section
Diameter, in the initial state, second bending section one end offsets with first sliding block, and the other end is provided with pulling force bullet
One end for being provided with tension spring of spring, second bending section is provided with magnetic tip；Electromagnet is matched with the magnetic tip
It closes, the electromagnet of two driving devices moves synchronously；Fixed shell, is fixed on the outside of the hollow pipe, covers
The electromagnet, third shaft, the second bending section and tension spring, the electromagnet, third shaft and tension spring are fixed on
On the fixed shell.
Optionally, the hollow pipe is inclined, and the power output rod is inclined, the hollow pipe and the power
The inclined direction of output rod is on the contrary, two power output rods are located at the inside of two hollow pipes, in the initial state,
Turntable on each power output rod is just being adjusted the distance its closer door-plate.
Optionally, the rubber net is rectangular, is provided with drawstring 81 on the angle of rubber net front end both sides, on each angle
Drawstring connect with the driving device closer apart from the angle.
Optionally, second sliding block and the first sliding block are integrated.
Manned vehicle provided by the utility model, by the first auxiliary duct of setting and the second auxiliary duct, and respectively
Positioned at the centre position of the front end of aircraft body and the centre position of rear end, to the power take-off need when meeting manned operation
While asking, in the case where there is lateral wind flight, also it is not easy to increase and is needed when the influence for overcoming lateral wind to aircraft
Power.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of manned vehicle of embodiment 1；
Fig. 2 is the structural schematic diagram of embodiment 2；
Fig. 3 is enlarged drawings of the Fig. 2 at A；
Fig. 4 is the structural schematic diagram of the transmitting holder of embodiment 3；
Fig. 5 is enlarged drawings of the Fig. 4 at B；
Fig. 6 is the structural schematic diagram of the rubber net of embodiment 3；
Fig. 7 is the attachment structure schematic diagram of the rubber net of embodiment 3；
Fig. 8 is the structural schematic diagram of the warehouse of embodiment 4；
Fig. 9 is enlarged drawings of the Fig. 8 at C；
Figure 10 is enlarged drawings of the Fig. 8 at D；
Figure 11 is the three-dimensional structure diagram of the third shaft in embodiment 4.
Specific implementation mode
The technical solution of the utility model is described in detail below in conjunction with the accompanying drawings.
Embodiment 1, the utility model provide a kind of manned vehicle, described referring to Fig. 1, including aircraft body 11
Manned portion 12 is provided on aircraft body 11, manned portion can use existing structure, such as seat assembly, seat ASSY
Deng even bar shaped babinet is not specifically limited, the aircraft body as long as the structure for carrying people can be realized herein
Front end both sides be provided with before duct 13, the both sides of the rear end of the aircraft body are provided with rear duct 14, contain before described
Symmetric screw propeller 15 is installed in road and the rear duct；It is auxiliary that the centre position of the front end of the aircraft body is equipped with first
Duct 16 is helped, the first auxiliary propeller 17 is installed, the internal diameter of first duct is more than described in the first auxiliary duct
The internal diameter of preceding duct, the peak power output of first auxiliary propeller are more than the maximum work output of the symmetric screw propeller
Rate；The centre position of the rear end of the aircraft body is equipped with the second auxiliary duct 18, is installed in the second auxiliary duct
There are the second auxiliary propeller 19, the internal diameter of second duct to be more than the internal diameter of the rear duct, second auxiliary propeller
Peak power output be equal to first auxiliary propeller peak power output.For the sake of security, in the manned portion
Or outside is provided with driver's cabin, the setting of driver's cabin is well known to those skilled in the art, and details are not described herein again.
Manned vehicle provided by the utility model, by the first auxiliary duct of setting and the second auxiliary duct, and respectively
Positioned at the centre position of the front end of aircraft body and the centre position of rear end, to the power take-off need when meeting manned operation
While asking, in the case where there is lateral wind flight, also it is not easy to increase and is needed when the influence for overcoming lateral wind to aircraft
Power.
Embodiment 2, on the basis of embodiment 1, referring to Fig. 2 and Fig. 3, the centre position of the front end of the aircraft body
It is vertically fixed the first fixed body 20, the second fixed body 21 and third fixed body 22 are horizontally fixed on first fixed body,
Second fixed body 21 and the third fixed body 22 are arranged in parallel；The front end of the aircraft body is provided with the first driving
Body 23 and the second driving body 24, first driving body include：First base shaft 25, the first bending part 26,27 and of first connecting portion
Second connecting portion 28, what first base shaft 25, the first bending part 26, first connecting portion 27 and second connecting portion 28 were integrated,
First bending part is in first base shaft close to one end of first fixed body, the first connecting portion 27 and second
Interconnecting piece 28 is located at the one end of first base shaft far from first fixed body, and first base shaft is articulated with the aircraft
The front end of ontology is provided with first hydraulic cylinder 29, the power output end connection of the first hydraulic cylinder on second fixed body
There are the first telescopic rod 30, first telescopic rod to be connect with first bending part, first is hinged in the second connecting portion
Crimp type terminal 31, pressure line terminal are referred to as line nose, are fixed with train line 32 on first crimp type terminal, and described
The first supporting rack 33 is fixed on one fixed body；Second driving body includes：Second base shaft, the second bending part, third connection
Portion and the 4th interconnecting piece, what second base shaft, the second bending part, third interconnecting piece and the 4th interconnecting piece were integrated, described
Two bending parts are located at second base shaft close to one end of first fixed body, the third interconnecting piece and the 4th connecting portion
In the one end of second base shaft far from first fixed body, before second base shaft is articulated with the aircraft body
It holds, is provided with second hydraulic cylinder 34 on the third fixed body, the power output end of the second hydraulic cylinder is connected with second and stretches
Contracting bar 35, second telescopic rod are connect with second bending part, and the second crimp type terminal is hinged on the 4th interconnecting piece
36, the second supporting rack 37 is fixed on the third fixed body；The front end of the aircraft body is additionally provided with penetration pipe 38, institute
The front end that penetration pipe is fixed on the aircraft body by first supporting rack and the second supporting rack is stated, the train line is worn
The penetration pipe is crossed to be fixed on the second crimp type terminal；It is provided with the first connector 39 and second company on the first auxiliary duct
Junctor 40, first connector are located at the described first top for assisting duct, and second connector is located at described first and contains
The bottom in road, first connector is hinged with the first connecting portion, and second connector is cut with scissors with the third interconnecting piece
It connects.
By above structure, in flight course, the rotation of the first auxiliary duct can be controlled, when needing to fast forward through,
Such as when rescuing in a hurry, the first auxiliary duct can be rotated to being rearward vented, accelerate forward speed.Control process is such as
Under：As shown in Fig. 2, the first stage：First hydraulic cylinder 29 pushes the first telescopic rod 30 of the first driving body to move to the right, drives
First bending part 26 of the first driving body to rotating backward counterclockwise, to make the first connecting portion 27 of the first driving body push the
One connector 39 moves to the left, drives the first of left side to assist duct top side to overturn to the left；Meanwhile second stage：First
The second connecting portion 28 of driving body moves to the left, pulls train line 32, makes the second connecting portion of the second driving body 24 to the right
Movement drives the second connector 40 to move to the right, drives the first of left side to assist duct bottom side to overturn to the right, reaches control
The purpose that first auxiliary duct rotates counterclockwise drives second when the second connecting portion of the second driving body 24 moves to the right
First bending part of driving body moves to the left, and the second telescopic rod is shunk；
When needing to restore original state, the phase III：First hydraulic cylinder 29 pulls the first telescopic rod of the first driving body
Stretching, extension, while second hydraulic cylinder 34 pushes the second telescopic rod to move to the right, drives the first bending part of the second driving body to inverse
Hour hands rotate backward, and to make the first connecting portion of the second driving body that the second connector 40 be pushed to move to the left, drive left side
The first auxiliary duct bottom side to overturn to the left；Meanwhile fourth stage：The second connecting portion of second driving body moves to the left,
Train line 32 is pulled, the second connecting portion of the first driving body 23 is made to move to the right, the first connector 39 is driven to move to the right,
It drives the first of left side to assist duct top side to overturn to the right, achievees the purpose that control the first auxiliary duct rotates clockwise,
When the second connecting portion of first driving body 23 moves to the right, the first bending part of the first driving body is driven to move to the left, the
One telescopic rod is shunk；
If one of hydraulic cylinder or driving body damage in entire journey, such as first hydraulic cylinder or the first driving body
Damage can also move the first bending for driving the second driving body to the left by the second telescopic rod of second hydraulic cylinder direct pull
Portion, to drive the first of left side to assist duct bottom side to overturn to the right, can also reach control first to rotating backward clockwise
The purpose that auxiliary duct rotates counterclockwise pushes only when needing to restore original state when the second telescopic rod being pushed to shrink
Apart from relatively long, the effect of the first auxiliary duct rotation is slightly worse, for example rotation angle becomes 60 degree from 90 degree, still, still
Be conducive to fast forward through, will not can not be fast forwarded through, certain second hydraulic pressure because of first hydraulic cylinder or the damage of the first driving body
Cylinder or the second driving body can also be by first hydraulic cylinders and the first driving body control the first auxiliary duct rotation when damaging.It needs
Illustrate, as a kind of deformation, the first above-mentioned driving body and the second driving body structure can also be applied to the second auxiliary
Duct, the installation and control of hydraulic cylinder can be generally controlled by flight control known to this example and technical staff,
Details are not described herein again.
Embodiment 3, when being rescued for mountain, such as when being rescued when the lost stranded steep cliff of tour pal, by external environment (such as
Massif, trees etc.) it influences, manned vehicle tends not to directly sue and labour immediately below the rescued, for this purpose, applicant is in embodiment
1 or embodiment 2 on the basis of devise following scheme：Referring to Fig. 4-Fig. 7, the one or both sides of the aircraft body are provided with
The installation settings of automatically-controlled door, automatically-controlled door is well known to those skilled in the art, therefore is not drawn into figure, can also be incited somebody to action with reference to Fig. 8
Door-plate replaces with the door automatically controlled, is provided with accommodating space on the inside of the automatically-controlled door, transmitting is equipped in the accommodating space
The front end of holder 41, the transmitting holder is provided with drive roll 42, and the rear end of the transmitting holder is provided with the first driven voller 43,
It is provided with the second driven voller 44 between the drive roll and first driven voller, multiple rubbers are wound on first driven voller
Glue net 45 is connected by plastic ties 46 between multiple rubber nets；The front-end and back-end of the rubber net are both provided with Weight plate 53,
The edge of the rubber net is provided with plastic cloth bound edge 47, and when rubber net is connected to by deliverer, plastic cloth bound edge is without elasticity
And rubber net is flexible, is pounded in people and pocketed is more readily formed when on rubber net, makes to not readily disengage from rubber net by deliverer, institute
State the grid 48 that plastic cloth bound edge surrounds the rubber net completely；It is attached to be located at second driven voller both ends on the transmitting holder
Close position is equipped with Auxiliary support roller and limit roller 50, and the Auxiliary support roller is hollow, and surface is provided with multiple spray orifices
54, it is internally provided with ignition, naturally it is also possible to which only installation electronic ignition head, other parts draw Auxiliary support with lead
Outside roller, it is provided with oil pipe 51 on the transmitting holder, piston engine, the piston engine are provided in the aircraft body
Machine is connect with the oil pipe；Front end on the transmitting holder positioned at the drive roll is provided with guide plate 52, the guide plate
To be smooth, in order to which rubber net slips over.
For the structure in rescue, drive roll movement drives the movement of the first driven voller, be laid in rubber net on drive roll by
In having frictional force with drive roll, the first driven voller and the second driven voller, travel forward, when plastic ties move at aiding support roller
When, engine moment rail fuel feeding, certain engine can also be replaced with fuel gas supply equipment, ignition moment point
Fire, flare are sprayed from spray orifice, plastic ties are blown, above-mentioned engine and igniter can use flight control control
System, the rubber net of front continue to move along guide plate, fly out to be caught and change by under deliverer by deliverer outward
Direction is fallen, is conducive to avoid danger (such as pylon) by deliverer, and buffering is formed in landing, is conducive to protection and is succoured
Person, when plastic ties are blown, subsequent rubber net front end is continued to move to the second driven voller by inertia, in the first driven voller and
Continue to move under the action of second driven voller, until moving to drive roll, repeats the movement of the rubber net of front, the structure is opposite
Simply, easy to use.
It should be noted that in the present embodiment, front end is the tandem that is moved in transmitting using rubber net as reference,
A rubber net can also be arranged in the device, and multiple rubber nets are only arranged and can continuously emit in rescue, more insure, rubber
Net is the net made of rubber material, when catching by deliverer, due to having certain horizontal velocity that can change after its transmitting
By the falling direction of deliverer, be conducive to avoid danger (such as pylon) by deliverer, and buffering is formed in landing, favorably
In protection by deliverer, rubber net can also be made using silica gel material, and thickness can be arranged according to actual conditions, use silica gel
When material, the inside of net can be arranged to hollow, self-filler and silica gel mesh can also be set in accommodating space
Connection, controls it by the control system of aircraft and quickly fills the gas smaller than atmospheric density, to subtract when catching by deliverer
Slow fall time, and increase elasticity when landing, protection is more advantageous to by deliverer.In order to facilitate the rescue aircraft sheet
The bottom of body is equipped with searchlight, human body temperature survey meter and locator.
Embodiment 4, as another scheme for solving the problems, such as embodiment 3, referring to Fig. 8-Figure 11, the aircraft body
One or both sides be provided with two door-plates 55 worked in coordination, the door-plate is fixed on the aircraft by first rotating shaft 56
On ontology, it is provided with warehouse 59 on the inside of the door-plate, is provided in the warehouse and shelves plate 57, it is described to shelve on plate tiling and have
Rubber net 45；There are two driving devices, two driving devices to be located at the both sides for shelving plate, institute for installation in the warehouse
The both sides for stating the front end of rubber net are provided with drawstring 81, and the drawstring per side is connect with the driving device closer apart from the side,
In general, it is rectangular that networking, which can be arranged, in the rubber, drawstring 81, each angle are provided on the angle of rubber net front end both sides
On drawstring connect with the driving device closer apart from the angle, in the application, the driving device includes：Hollow pipe 58, it is fixed
On the inside of the warehouse；Energy-storaging spring 60, is fixed in hollow pipe, and positioned at the front end of hollow pipe；First sliding block 61, with
The energy-storaging spring connection；Second sliding block 62, with the first shoe contact, the second bad block can also be made as one with the first sliding block
Body, position can also exchange, be not specifically limited herein；Electric telescopic rod 63 coordinates with second sliding block, for driving the
Two sliding blocks, which compress the first sliding block, makes energy-storaging spring accumulation of energy, the electric telescopic rod of two driving devices move synchronously,
It links, can generally be controlled by flight control；Power output rod 64, power output rod one end setting
There are the first bending section 65, one end that first bending section is not connect with the power output end to be stuck on second sliding block,
One end for being provided with the first bending section of the power output rod is fixed on by the second shaft 66 in the warehouse, described hollow
It is provided with first through hole 74 on pipe, is passed through for first bending section, the diameter of the first through hole is curved more than described first
The diameter of pars convoluta can set the diameter of first through hole to the 2-5 of the diameter of bending section for the ease of the activity of the first bending section
Times, the radian of bending section is 60-120 degree；Turntable 67 is fixed on the other end of the power output rod by central shaft 68, in
Bearing can also be installed, turntable is fixed on by bearing on central shaft, and the turntable is protruded at the top of the central shaft in mandrel
Top surface；Blade 69, is fixed on the top of the central shaft, and the blade includes horizontal part 70 and vertical portion 71, the level
Portion is connected with the vertical portion, is generally integrated, and the horizontal part is fixed on the central shaft；Column 72 is fixed on institute
It states on turntable, is located at the side of blade, and the distance of the column to the central shaft is less than the vertical portion to central shaft
Distance, the height of the column higher than the vertical portion bottom and be less than the horizontal part, the drawstring is fixed on described
On column, it is typically secured to the top of column；Second bending section 73, second bending section is by being set to outside the hollow pipe
The third shaft 78 of side is fixed on the outside of the hollow pipe, and the second through-hole 75 is provided on the hollow pipe, for described the
Two bending sections pass through, and the diameter of second through-hole is more than the diameter of second bending section, lives for the ease of the second bending section
It is dynamic, the diameter of the second through-hole can be set to 2-5 times of the diameter of bending section, the radian of bending section is 60-120 degree, initial
Under state, second bending section one end offsets with first sliding block, and the other end is provided with tension spring 76, and described second is curved
One end for being provided with tension spring of pars convoluta is provided with magnetic tip 77, can generally iron, copper etc. be used to be fabricated to column structure；
Electromagnet 79 coordinates with the magnetic tip, and the electromagnet of two driving devices moves synchronously, that is, links
, it can generally be controlled by flight control；Fixed shell 80, is fixed on the outside of the hollow pipe, covers described
Electromagnet, third shaft, the second bending section and tension spring, the electromagnet, third shaft and tension spring are fixed on described
On fixed shell.As a preferred solution, the hollow pipe be it is inclined, the power output rod be it is inclined, it is described
The inclined direction of hollow pipe and the power output rod is on the contrary, two power output rods are located at the interior of two hollow pipes
Side, in the initial state, the turntable on each power output rod are just being adjusted the distance the closer door-plate of the turntable, in general, two
A hollow pipe is arranged in toed-out shape, and two power output rods are in energy toed-in shape setting.It should be noted that in the present embodiment,
Original state refers to the state that driving device does not drive rubber net to move, and front end is suitable before and after being moved in transmitting with rubber net
Sequence is reference.
In rescue, two electromagnet move synchronously the structure, that is, simultaneously it is electric, be attracted magnetic tip, pull the
Two bending sections are rotated along third shaft, and part of second crooked position on the inside of hollow pipe is made to be moved out along the second through-hole rapidly
Go out, the first sliding block breaks away from the constraint of the second bending section, is moved backward rapidly by the active force of energy-storaging spring, and the second sliding block band is pushed
Dynamic first bending section movement, makes power output rod be rotated along the second shaft, and when dial movement on power output rod pulls drawstring,
Rubber net is set to travel forward, and the drawstring of both sides is flared out, when turntable is contacted with door-plate, promotion door-plate is opened, meanwhile, by
Contact point is rotated by the effect of the power of tangential direction when turntable and door contact, and drives drawstring rotation, when drawstring passes through blade
It is cut off, rubber net is still flown out and opened outward by inertia at this time, to be caught and change by deliverer's by deliverer
Falling direction is conducive to avoid danger (such as pylon) by deliverer, and forms buffering in landing, is conducive to protection and is rescued
The person of helping, the structure is relatively easy, easy to use.
Above-described embodiment is the illustration of utility model, should not be described to limit with the exemplary embodiments of specification and attached drawing
The protection domain of patent right processed.
The utility model preferred embodiment and embodiment are explained in detail above in conjunction with attached drawing, but this
Utility model is not limited to the above-described embodiment and examples, within the knowledge of those skilled in the art, may be used also
With various changes can be made without departing from the concept of the premise utility.It in the claims, should not will be between bracket
Any reference mark as limitations on claims.Word "comprising" does not exclude the presence of element not listed in the claims
Or step.The use of word first, second and third etc. does not indicate that any sequence, can these words be construed to title.
Claims (9)
1. a kind of manned vehicle, which is characterized in that including aircraft body (11), be provided on the aircraft body (11)
The both sides of manned portion (12), the front end of the aircraft body are provided with preceding duct (13), the rear end of the aircraft body
Both sides are provided with rear duct (14), and symmetric screw propeller (15) is equipped in the preceding duct and the rear duct；
The centre position of the front end of the aircraft body is equipped with the first auxiliary duct (16), pacifies in the first auxiliary duct
Equipped with the first auxiliary propeller (17), the internal diameter of the first auxiliary duct is more than the internal diameter of the preceding duct, and described first is auxiliary
The peak power output of propeller is helped to be more than the peak power output of the symmetric screw propeller；
The centre position of the rear end of the aircraft body is equipped with the second auxiliary duct (18), pacifies in the second auxiliary duct
Equipped with the second auxiliary propeller (19), the internal diameter of the second auxiliary duct is more than the internal diameter of the rear duct, and described second is auxiliary
The peak power output of propeller is helped to be equal to the peak power output of first auxiliary propeller.
2. manned vehicle according to claim 1, which is characterized in that be provided with driver's cabin in the manned portion.
3. manned vehicle according to claim 1, which is characterized in that the centre position of the front end of the aircraft body
It is vertically fixed the first fixed body (20), the second fixed body (21) and third fixed body are horizontally fixed on first fixed body
(22), second fixed body (21) and the third fixed body (22) are arranged in parallel；
The front end of the aircraft body is provided with the first driving body (23) and the second driving body (24), the first driving body packet
It includes：First base shaft (25), the first bending part (26), first connecting portion (27) and second connecting portion (28), first base shaft
(25), the first bending part (26), first connecting portion (27) and second connecting portion (28) are integrated, first bending part in
First base shaft is located at institute close to one end of first fixed body, the first connecting portion (27) and second connecting portion (28)
The one end of the first base shaft far from first fixed body is stated, first base shaft is articulated with the front end of the aircraft body, institute
It states and is provided with first hydraulic cylinder (29) on the second fixed body, the power output end of the first hydraulic cylinder is connected with the first telescopic rod
(30), first telescopic rod is connect with first bending part, and the first crimp type terminal is hinged in the second connecting portion
(31), it is fixed with train line (32) on first crimp type terminal, the first supporting rack (33) is fixed on first fixed body；
Second driving body includes：Second base shaft, the second bending part, third interconnecting piece and the 4th interconnecting piece, second base
What bar, the second bending part, third interconnecting piece and the 4th interconnecting piece were integrated, second bending part is leaned in second base shaft
One end of nearly first fixed body, the third interconnecting piece and the 4th connecting portion are in second base shaft far from described first
One end of fixed body, second base shaft are articulated with the front end of the aircraft body, and is provided on the third fixed body
Two hydraulic cylinders (34), the power output end of the second hydraulic cylinder are connected with the second telescopic rod (35), second telescopic rod with
Second bending part connects, and the second crimp type terminal (36) is hinged on the 4th interconnecting piece, is consolidated on the third fixed body
Surely there is the second supporting rack (37)；
The front end of the aircraft body is additionally provided with penetration pipe (38), and the penetration pipe passes through first supporting rack and second
Supporting rack is fixed on the front end of the aircraft body, and the train line is fixed on the second crimp type terminal across the penetration pipe
On；
It is provided with the first connector (39) and the second connector (40) on the first auxiliary duct, first connector is located at
The top of the first auxiliary duct, second connector are located at the described first bottom for assisting duct, first connection
Body is hinged with the first connecting portion, and second connector is hinged with the third interconnecting piece.
4. according to claim 1-3 any one of them manned vehicles, which is characterized in that the side of the aircraft body or
Both sides are provided with automatically-controlled door, are provided with accommodating space on the inside of the automatically-controlled door, transmitting holder is equipped in the accommodating space
(41), the front end of the transmitting holder is provided with drive roll (42), and the rear end of the transmitting holder is provided with the first driven voller
(43), it is provided with the second driven voller (44) between the drive roll and first driven voller, is wound on first driven voller
There are multiple rubber nets (45), is connected by plastic ties (46) between multiple rubber nets；
The front-end and back-end of the rubber net are both provided with Weight plate (53), and the edge of the rubber net is provided with plastic cloth bound edge
(47), the plastic cloth bound edge surrounds the grid (48) of the rubber net completely；
Position on the transmitting holder positioned at second driven voller both ends is equipped with Auxiliary support roller and limit roller (50), institute
It is hollow to state Auxiliary support roller, and surface is provided with multiple spray orifices (54), is internally provided with ignition, the transmitting holder
On be provided with oil pipe (51), be provided with piston engine in the aircraft body, the piston engine connects with the oil pipe
It connects；
The front end of the drive roll is provided with guide plate (52) on the transmitting holder, the guide plate is smooth.
5. manned vehicle according to claim 4, which is characterized in that the bottom of the aircraft body is equipped with searchlighting
Lamp, human body temperature survey meter and locator.
6. according to claim 1-3 any one of them manned vehicles, which is characterized in that the side of the aircraft body or
Both sides are provided with two door-plates (55) worked in coordination, and the door-plate is fixed on the aircraft body by first rotating shaft (56)
On, it is provided with warehouse (59) on the inside of the door-plate, is provided in the warehouse and shelves plate (57), it is described to shelve on plate tiling and have
Rubber net (45)；
There are two driving devices, two driving devices to be located at the both sides for shelving plate, the rubber for installation in the warehouse
The both sides of the front end of glue net are provided with drawstring (81), and the drawstring per side is connect with the driving device closer apart from the side, institute
Stating driving device includes：
Hollow pipe (58), is fixed on the inside of the warehouse；
Energy-storaging spring (60), is fixed in hollow pipe, and positioned at the front end of hollow pipe；
First sliding block (61), connect with the energy-storaging spring；
Second sliding block (62), with the first shoe contact；
Electric telescopic rod (63) coordinates with second sliding block, makes energy-storaging spring for driving the second sliding block to compress the first sliding block
The electric telescopic rod of accumulation of energy, two driving devices moves synchronously；
Power output rod (64), described power output rod one end are provided with the first bending section (65), first bending section not with
One end of power output end connection is stuck on second sliding block, and the power output rod is provided with the first bending section
One end is fixed on by the second shaft (66) in the warehouse, and first through hole (74) is provided on the hollow pipe, for described
First bending section passes through, and the diameter of the first through hole is more than the diameter of first bending section；
Turntable (67) is fixed on the other end of the power output rod, the top protrusion of the central shaft by central shaft (68)
The top surface of the turntable；
Blade (69), is fixed on the top of the central shaft, and the blade includes horizontal part (70) and vertical portion (71), the water
Flat portion is connected with the vertical portion, and the horizontal part is fixed on the central shaft；
Column (72), is fixed on the turntable, is located at the side of blade, and the distance of the column to the central shaft is small
The height of distance in the vertical portion to central shaft, the column is higher than the bottom of the vertical portion and is less than the level
Portion, the drawstring are fixed on the column；
Second bending section (73), second bending section are fixed on by being set to the third shaft (78) on the outside of the hollow pipe
The outside of the hollow pipe is provided with the second through-hole (75) on the hollow pipe, is passed through for second bending section, described
The diameter of two through-holes is more than the diameter of second bending section, in the initial state, second bending section one end and described the
One sliding block offsets, and the other end is provided with tension spring (76), one end setting for being provided with tension spring of second bending section
Be magnetic suction nozzle (77)；
Electromagnet (79), coordinates with the magnetic tip, and the electromagnet of two driving devices moves synchronously；
Fixed shell (80), is fixed on the outside of the hollow pipe, cover the electromagnet, third shaft, the second bending section and
Tension spring, the electromagnet, third shaft and tension spring are fixed on the fixed shell.
7. manned vehicle according to claim 6, which is characterized in that the hollow pipe is inclined, and the power is defeated
Rod is inclined, and the inclined direction of the hollow pipe and the power output rod is on the contrary, two power output rods are located at
The inside of two hollow pipes, in the initial state, the turntable on each power output rod is just being adjusted the distance, and it is closer
Door-plate.
8. manned vehicle according to claim 6, which is characterized in that the rubber net is rectangular, before the rubber net
It holds and is provided with drawstring (81) on the angle of both sides, the drawstring on each angle is connect with the driving device closer apart from the angle.
9. manned vehicle according to claim 6, which is characterized in that second sliding block and the first sliding block are integrated
's.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820338081.XU CN208036602U (en) | 2018-03-12 | 2018-03-12 | Manned vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820338081.XU CN208036602U (en) | 2018-03-12 | 2018-03-12 | Manned vehicle |
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| Publication Number | Publication Date |
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| CN208036602U true CN208036602U (en) | 2018-11-02 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108248853A (en) * | 2018-03-12 | 2018-07-06 | 北京零创众成科技有限公司 | Manned vehicle |
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2018
- 2018-03-12 CN CN201820338081.XU patent/CN208036602U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108248853A (en) * | 2018-03-12 | 2018-07-06 | 北京零创众成科技有限公司 | Manned vehicle |
| CN108248853B (en) * | 2018-03-12 | 2024-02-02 | 北京零创众成科技有限公司 | Manned aircraft |
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Effective date of registration: 20200519 Address after: Room 4-1-402, No. 55, Fuye street, Luotuo street, Zhenhai District, Ningbo City, Zhejiang Province Patentee after: Ningbo Tiancheng Intelligent Technology Co.,Ltd. Address before: 100000 Xueyuan Road, Haidian District, Haidian District, Beijing, 14 (1405-003) Patentee before: BEIJING LINGCHUANG ZHONGCHENG TECHNOLOGY Co.,Ltd. |
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Effective date of registration: 20230119 Address after: 241000 Room 21, Floor 7, Building 5, Beihang Wuhu Navigation Innovation Park, Anhui Xinwu Economic Development Zone, Wanzhou District, Wuhu City, Anhui Province Patentee after: Anhui Feixiong Zhongcheng Intelligent Technology Co.,Ltd. Address before: Room 4-1-402, No. 55, Fuye Street, Luotuo Street, Zhenhai District, Ningbo City, Zhejiang Province, 315200 Patentee before: Ningbo Tiancheng Intelligent Technology Co.,Ltd. |