CN208774442U - A kind of amphibious helicopter of No Tail Rotor high speed single rotor - Google Patents

Abstract

The utility model discloses a kind of amphibious helicopters of No Tail Rotor high speed single rotor, including single rotor dynamical system, vectored thrust system, casing, hull, rack, solar battery, radar, laser detector, camera and power supply；It is mainly characterized by that two axle thrust vector dynamical systems are installed in fuselage two sides designated position, it not only can produce biggish forward thrust, it can also be yawed by the thrust vectoring of two systems differential, yaw control moment is generated while balancing main paddle torque, the pitching of two axle thrust vector systems linkage and the differential pitching formed to fuselage and rolling control moment can also be passed through simultaneously, influence caused by row speed difference causes lift uneven before and after overcoming single-rotor helicopter during high-speed flight because of blade, hull cooperates single rotor dynamical system and vectored thrust system, can also have excellent mobility in water surface man the helo, tail is equipped with sonar unit, detect operation can be carried out to underwater, and different positions can be exchanged in due course.

Description

A kind of amphibious helicopter of No Tail Rotor high speed single rotor

Technical field

The utility model relates to single-rotor helicopter technical field, specially a kind of No Tail Rotor high speed single rotor has the sun It can helicopter of the battery with detecting function.

Background technique

Currently, most helicopters mostly use greatly single rotor magnetic tape trailer oar system.Its disadvantage is mainly shown as: transmission mechanism It is complicated, power loss is big, tail boom is too long that flexibility decline, tail-rotor is caused to be easy to be damaged and maintenance cost height etc..For small For type helicopter or small-sized depopulated helicopter, there is its flexibility of tail-rotor worse, and complicated mechanism is easier machinery occur Failure causes to ruin machine.Meanwhile the single-rotor helicopter with tail-rotor its flying speed is a significant feature slowly；Continuation of the journey energy Power is general, and power supply electric energy, which exhausts rear helicopter, can not once be walked operation or need to make a return voyage in time.

Utility model content

The purpose of this utility model is to provide a kind of amphibious helicopters of No Tail Rotor high speed single rotor, to solve above-mentioned ask Topic, including single rotor dynamical system, vectored thrust system, casing, hull, rack, solar battery, radar, laser detector, Camera and power supply；The structure of the amphibious helicopter of No Tail Rotor high speed single rotor is symmetrical about mechanical longitudinal axis；The hull Buoyancy be much larger than body gravity；The hull of symmetrical structure is set, good balance is able to maintain on the water surface, on the one hand, On the other hand the weight for mitigating helicopter as far as possible is designed by structure, hull is allowed to have biggish buoyancy, is reduced helicopter and is existed The resistance of hull when aerial.

The rack includes frame main body and both wings and layout triangular in shape, and the single rotor dynamical system is fixed on rack In main body, the vectored thrust system is fixed on rack both wings, and the frame main body is mounted on casing internal, the casing piecemeal Integrally casting is installed integral.The rack both wings pass through casing from frame main body and are suspended from outside fuselage；The hull is mounted on machine Shell lower end；When helicopter needs to drop on the water surface, the buoyancy support helicopter of hull is suspended on the water surface, and afterbody is logical Cross linkage structure, sonar unit be discharged into water, by control module control sonar unit work, detect the underwater hydrology, The shoal of fish or other effect activities.The solar battery is mounted on the casing of the unmanned plane upper half, can preferably be received in this way Sunlight.Especially when helicopter hovers on the water surface, solar battery charges to power supply, when greatly improving operation Between.The radar and camera are mounted on ventral, when helicopter is skyborne, open radar installations, following to fuselage Aerial and ground carry out observing and controlling, especially there is effect well to landform exploration, forest fire protection, urban transportation monitoring etc., The radar is millimetre-wave radar or other more fine radars, and the radar mouth is provided with shield, and when use opens anti- Shield stops working and closes shield, protects to radar.The camera can shoot operating area；And it will Captured image or video are transmitted to the 4G module on signalling means by control module, realize real-time data transmission.It therefore, can be with By interaction 4G module manipulation and control module, helicopter is manipulated, can be more convenient more timely to make adjustment.The laser Detector is mounted on chain-drive section, detects the flight condition in front of helicopter, timely avoiding barrier, when hovering on the water surface, It gushes to come if any big wave, laser acquisition, which detects, communicates information to control module, and control module releases news dynamic to single rotor Force system and vectored thrust system, i.e., helicopter, which takes off, avoids stormy waves.When on the water surface, it can be provided with single rotor dynamical system Certain lift, vectored thrust system provide forward thrust, and helicopter is quickly slided on the water surface, greatly promotes and go straight up to The mobility of machine.

The power supply is single rotor dynamical system, laser detector, signalling means, sonar unit, radar, camera and vector Push system provides electric energy, and the solar battery is connected to power supply by conducting wire, and the solar battery connects to power supply line Rectification circuit, filter circuit, inversion regulating circuit are provided in road, such solar battery can charge to power supply, go straight up to For machine when the task of execution, solar battery can give power source charges, improve the cruising ability of helicopter, especially helicopter Emergency situations are met, when electric power deficiency has supported helicopter to make a return voyage, possessing solar battery can improve to power source charges The operating limit of helicopter.

The power supply provides electric energy for locating module, and the locating module is GPS positioning system, BEI-DOU position system or base The one or more for positioning system of standing.

As a further improvement of the above technical scheme:

The rack includes U-shaped part, fixed frame, big square tube, the first small square tube, the second small square tube, round tube and Fixing clamp-seat； The U-shaped part is opening down, and two sides are horizontally installed with big square tube by screw, and the big square tube tail end is fixed by Fixing clamp-seat There is round tube, the round tube is vertical with big square tube；The round tube end is mounted with fixed frame, and described first small square tube one end is solid It is scheduled on big square tube front end, the other end is fixed on fixed frame；In the secure u-shaped member of described second small square tube one end, the other end is fixed On fixed frame；The first small square tube, the second small square tube be not in same level, therefore the first small square tube, the second small side Pipe constitutes pyrometric cone with round tube, and fixed frame is in endpoint, and the fixing pipe in three different directions can preferably fix fixed frame, Being unlikely to deform causes fixed frame to be displaced.

The single rotor dynamical system is mounted on U-shaped part bottom plate, and bottom plate front end is equipped with main motor, on the main motor First rotating shaft is installed；Base plate rear end is equipped with the second shaft, and the first rotating shaft is connect by belt with the second shaft, described Second shaft is fixed with pinion gear, and the pinion gear is engaged with gear wheel, is welded with third on the gear wheel central axes Shaft, first steering engine are uniformly distributed along third shaft and are fixedly mounted on casing, and is equipped on first steering engine One rudder arm, first rudder arm are connect by first connecting rod with cross plate, and the cross plate passes through the second connecting rod and rotor Folder connection, the rotor press from both sides and are equipped with main rotor；The main motor and the first steering engine are connected to power supply by conducting wire.

The fixed frame level is fixedly installed with support frame, and the second steering engine, institute are fixedly installed on support frame as described above pedestal State the second steering engine and the second rudder arm be installed, holder is installed on support frame as described above, second rudder arm by third connecting rod with Holder connection；The holder is provided with support rod, and fixed disk is movably installed on the support rod, and the fixed disk is fixedly mounted Have from motor, described be equipped with from motor is fixedly installed with from rotor, and third steering engine, institute are fixedly installed on the holder It states third steering engine and third rudder arm is installed, the third rudder arm is connect by the 4th connecting rod with fixed disk；Second rudder arm With third rudder arm at being vertically arranged；Support frame as described above and support rod are at being vertically arranged；Second steering engine and third steering engine pass through Conducting wire connects to power supply.

The amphibious helicopter of No Tail Rotor high speed single rotor is in canard configuration.Improve the skyborne mobility of helicopter Can, also improve the function performance of helicopter in water.

Control module, the control module and main motor, the first steering engine, the second steering engine, third are provided in the casing Steering engine, laser detector, signalling means, sonar unit and radar pass through electric data connection, and the control module is with power supply by leading Line connection, the control module have the function of to receive, storage, processing, release news.

The solar battery is thin-film solar cells or flexible solar battery.

The casing includes entablature, fixing layer and carbon fiber layer, and the solar battery is mounted on the carbon on the outside of casing Fibrous layer.

The signalling means has the function of sending and receiving information.

The technical solution of each embodiment can be combined in the utility model, and the technical characteristic in embodiment can also carry out group Conjunction forms new technical solution.

The beneficial effects of the utility model, conventional single-rotor helicopter propose a kind of based on thrust vectoring on the basis of being laid out The No Tail Rotor high-speed helicopter design layout of structure.It is mainly characterized by installing two axle thrust vectors in fuselage two sides designated position Dynamical system not only can produce biggish forward thrust, can also be differential by the yaw of the thrust vectoring of two systems, lead in balance Yaw control moment is generated while paddle torque, while can also be linked and differential formation by the pitching of two axle thrust vector systems Pitching and rolling control moment to fuselage, row speed difference before and after overcoming single-rotor helicopter during high-speed flight because of blade Influence caused by causing lift uneven.The type is not only able to achieve the high-speed flight of remote unconventional helicopter, and structure is simple, Conventional tail-rotor transmission parts are eliminated, while two sets of thrust vectoring systems can be mutually backups, and ensure that whole aircraft reliability and safety Property.External form feature is in canard configuration, and fairshaped fuselage greatly reduces air drag, meanwhile, because of its appearance structure feature, During doing exceedingly difficult movements or Fast marching, relative to other types, stationarity is had more.It increases detecting function and swashs Optical detection avoids obstacle function, while can also add other function equipment, and expand the utility model meets the tendency of range, increases its function It can effect.Solar battery is arranged in casing, increases cruising ability, and improve the working limit of helicopter.Due to hull Cooperate single rotor dynamical system and vectored thrust system, can also have excellent mobility, tail peace in water surface man the helo Equipped with sonar unit, detect operation can be carried out to underwater, and different positions can be exchanged in due course.When hovering on the water surface, Single rotor dynamical system and vectored thrust system are closed, and the biggish device that consumes energy is shut down, and solar battery charges to power supply, Greatly improve cruising ability and operation time.

Detailed description of the invention

Fig. 1 is the utility model appearance assumption diagram.

Fig. 2 is appearance front view on the utility model.

Fig. 3 is appearance top view on the utility model.

Fig. 4 is the utility model schematic diagram of internal structure.

Fig. 5 is that the utility model single rotor dynamical system changes big structure schematic diagram.

Fig. 6 is the utility model single rotor dynamical system front view.

Fig. 7 is the utility model vectored thrust system schematic.

Fig. 8 is a kind of example structure schematic diagram of the utility model casing.

Fig. 9 is a kind of example structure schematic diagram of the utility model casing.

In appended drawing reference: 1, single rotor dynamical system；101, main motor；102, belt；103, pinion gear；104, canine tooth Wheel；105, the first steering engine；106, the first rudder arm；107, first connecting rod；108, cross plate；109, third shaft；110, second Connecting rod；111, rotor presss from both sides；112, main rotor；2, vectored thrust system；201, support frame；202, the second steering engine；203, second Rudder arm；204, third connecting rod；205, holder；206, third steering engine；207, third rudder arm；208, the 4th connecting rod；209, from Motor；210, from rotor；211, support rod；212, fixed disk；3, casing；301, entablature；302, fixing layer；303, carbon fiber Tie up layer；4, hull；5, rack；501, U-shaped part；502, big square tube；503, the first small square tube；504, the second small square tube；505, circle Pipe；506, fixed frame；507, Fixing clamp-seat；6, mechanical longitudinal axis；7, solar battery；8, laser detector；9, radar；10, Signalling means；11, sonar unit；12, camera.

Specific embodiment

The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.

The term " first " of the specification and claims of the utility model, " second ", " third ", " the 4th " etc. are (such as Fruit presence) or "left", "right", "front", "rear", "top", "bottom" be used to distinguish similar objects or convenient for the utility model Structure description, the structure technology feature without being used to describe a particular order or precedence order and limiting the utility model. It should be understood that the information used in this way is interchangeable under appropriate circumstances, so as to the embodiments of the present invention described herein, Such as it can be performed in other sequences than those illustrated or described herein.In addition, term " includes " and " having " with And their any deformation, it is intended that cover it is non-exclusive include, for example, contain the process of a series of steps or units, Method, system, product or equipment those of are not necessarily limited to be clearly listed step or unit, but may include not arranging clearly Other step or units out or intrinsic for these process, methods, product or equipment.

As shown in figs 1-9, the amphibious helicopter of No Tail Rotor high speed single rotor of the present embodiment, including single rotor dynamical system 1, Vectored thrust system 2, casing 3, hull 4, rack 5, solar battery 7, radar 9, signalling means 10, sonar unit 11, camera 12, laser detector 8 and power supply；The structure of the amphibious helicopter of No Tail Rotor high speed single rotor is symmetrical about mechanical longitudinal axis 6；It is mechanical Structure it is symmetrical, helicopter can be made more steady, in high-speed motion and the complicated motion of automobile, ensuring the substantially steady of mechanism of qi Single rotor dynamical system 1 and vectored thrust system 2 are adjusted under state in time, makes accurate operation.The solar battery 7 is installed On the casing 3 of the unmanned plane upper half, sunlight can be preferably received in this way, when helicopter hovers on the water surface, solar energy Battery 7 charges to power supply, greatly improves the activity duration.Solar battery 7 is mounted on the casing 3 of the unmanned plane upper half On, radar 9 is mounted on ventral, and laser detector 8 is mounted on chain-drive section.Helicopter can also be measured apart from ground level, and Determination data is transmitted to control module, control module transmits information to signalling means 10, and signalling means 10 sends data to other Interaction end, interaction end respond, and signalling means 10 receives information, are transmitted to control module, and to helicopter single rotor dynamical system System 1 and vectored thrust system 2 make regulation, control the next step operation of helicopter；When execute landing order or control module from When I issues landing order, control module regulates and controls single rotor dynamical system 1 and vectored thrust system 2, laser detector 8 the real time measure data are transmitted to control module and control helicopter stable landing；The radar 9 is mounted on ventral, when straight When the machine of liter is skyborne, radar installations is opened, the aerial and ground following to fuselage carries out observing and controlling, especially surveys to landform Spy, forest fire protection, urban transportation monitoring etc. have good effect；Radar can also measure the height of helicopter, and radar is millimeter Wave radar or other more fine radars, the radar mouth are provided with shield, and when use opens shield, and stop working pass Shield is closed, radar is protected.Shield can carry out altitude location to helicopter with auxiliary laser detector 8 when opening. The camera 12 can shoot operating area；And captured image or video are transmitted to signal by control module 4G module on device 10 realizes real-time data transmission.It therefore, can be by interaction 4G module manipulation and control module, to helicopter It is manipulated, can be more convenient more timely to make adjustment.Laser detector 8 is mounted on chain-drive section, detects and flies in front of helicopter Row situation, timely avoiding barrier.Power supply is single rotor dynamical system 1, laser detector 8, radar 9, signalling means 10, sonar dress It sets 11, camera 12 and vectored thrust system 2 provides electric energy, solar battery 7 is connected to power supply by conducting wire, solar battery 7 connect to power supply and are provided with rectification circuit, filter circuit, inversion regulating circuit in route.Helicopter when the task of execution, Solar battery 7 can give power source charges, improve the cruising ability of helicopter, especially go straight up to opportunity emergency situations, power supply electricity When power deficiency has supported helicopter to make a return voyage, possessing solar battery 7 can be to power source charges, and improve helicopter uses pole Limit.

The power supply provides electric energy for locating module, and the locating module is GPS positioning system, BEI-DOU position system or base The one or more for positioning system of standing.

Sonar unit 11 is one kind of towed sonar or hand sonar.Sonar unit 11 (is often by transducer array Receive and dispatch dual-purpose), transmitter (including waveform generator, transmitting beamformer), timing center, receiver, display, controller It is formed etc. several parts.Sonar unit emits sound wave " irradiation " target, then receives the echo time of target reflection in water, and Echo parameter is to measure the parameter of target.The movement such as it can be used to detecting underwater object, and measure its distance, orientation, the speed of a ship or plane, course Element.Since target information is stored among echo, so the presence of target can be judged according to the echo-signal received, and Measure or estimate the parameters such as the distance, orientation, speed of target.Specifically, can by echo-signal and transmitting signal ask when Prolong the distance for deducing target, can deduce the direction of target by echo wavefront normal direction, and by echo-signal and transmitting signal it Between frequency displacement can deduce the radial velocity of target.Furthermore by the amplitude of echo, phase and changing rule, target can be identified Shape, size, property and motion state.For providing a great convenience property of underwater monitoring.

Rack 5 includes frame main body and both wings and layout triangular in shape, and single rotor dynamical system 1 is fixed on 5 main body of rack On, vectored thrust system 2 is fixed on 5 both wings of rack, and 5 main body of rack is mounted on inside casing 3, and 5 both wings of rack are from frame main body It is suspended from outside fuselage across casing 3；Hull 4 is mounted on 3 lower end of casing；The buoyancy of hull 4 is much larger than the gravity of helicopter, works as the water surface When tranquil, ventral not dampening.When helicopter needs to drop on the water surface, the buoyancy support helicopter of hull 4 is suspended in water On face, sonar unit 11 is discharged into water by afterbody by linkage structure, controls 11 work of sonar unit by control module Make, detects the underwater hydrology, the shoal of fish or other effect activities.The power supply is single rotor dynamical system 1 and vectored thrust system 2 provide electric energy.After rack 5 installs upper casing 3, both wings layout triangular in shape same as body, in conventional single-rotor helicopter cloth A kind of No Tail Rotor high-speed helicopter design layout based on thrust vectoring structure is proposed on the basis of office.Mainly in fuselage two sides Two axial vector push system 2 are installed in designated position, not only can produce biggish forward thrust, can also pass through the thrust of two systems Vector yaw is differential, yaw control moment is generated while balancing 112 torque of main rotor, while can also swear by two axle thrusts Pitching and rolling control moment of the pitching linkage and differential formation of amount system to fuselage, overcome single-rotor helicopter to fly in high speed Influence caused by causing lift uneven because of rotor front and back row speed difference during row.When hovering on the water surface, if any big wave Surge comes, and to control module is communicated information to, control module releases news to single rotor dynamical system 1 for laser acquisition detection 8 With vectored thrust system 2, i.e., helicopter, which takes off, avoids stormy waves.When on the water surface, it can be provided with single rotor dynamical system 1 centainly Lift, vectored thrust system 2 provides forward thrust, and helicopter is quickly slided on the water surface, greatly promotes helicopter In the mobility of the water surface.

Self-desttruction equipment is bound in control module, when helicopter faces a danger or is out of control or other smart machines and electricity When magnetic signal is invaded, self-desttruction equipment starting destroys control module.

Rack 5 includes U-shaped part 501, fixed frame 506, big square tube 502, the first small square tube 503, the second small square tube 504, circle Pipe 505 and Fixing clamp-seat 507；U-shaped part 501 is opening down, and 501 bottom of U-shaped part just above, facilitates installation single rotor dynamical system Device, it is also possible to power supply is mounted in the slot of U-shaped part 501, the weight of such fuselage can balance vertical in machinery well On axis 6, two sides are horizontally installed with big square tube 502 by screw, and big 502 tail end of square tube is fixed with circle by Fixing clamp-seat 507 Pipe 505, round tube 505 are vertical with big square tube 502；505 end of round tube is mounted with fixed frame 506, first small 503 one end of square tube It is fixed on big 502 front end of square tube, the other end is fixed on fixed frame 506；In second small 504 one end secure u-shaped member 501 of square tube, The other end is fixed on fixed frame 506, and the first small square tube 503, the second small square tube 504 be not in same level.Therefore first Small square tube, the second small square tube and round tube constitute pyrometric cone, and fixed frame is in endpoint, and the fixing pipe in three different directions will fix Frame can be fixed preferably, and being unlikely to deform causes fixed frame to be displaced.Pass through round tube 505, the first small square tube 503 and the second small square tube 504 tripartites fix fixed frame 506, and the first small square tube 503, the second small square tube 504 be in same level, therefore round tube 505, the first small square tube 503 and the second small square tube 504 constitute cone structure, so fixed frame 506 is highly stable, 5 structure of rack It simplifies, rack 5 can be made using the strong material of aluminum alloy materials or carbon fibre material or other light structures, mitigate rack 5 Own wt, while reinforcing the structural strength of rack 5.The profile pieces such as its U-shaped part 501, square tube and round tube can also use right angle Profile or other profiles substitution, mainly play fixed fixed frame 506, have no specific requirement.

Single rotor dynamical system 1 is mounted on 501 bottom plate of U-shaped part, and bottom plate front end is equipped with main motor 101, main motor 101 On first rotating shaft 113 is installed；Base plate rear end is equipped with the second shaft 114, and first rotating shaft 113 passes through belt 102 and second turn Axis 114 connects, and main motor 101 drives the rotation of the second shaft 114 by belt 102, and the second shaft 114 is fixed with pinion gear 103, Pinion gear 103 is engaged with gear wheel 104, the rotation of 114 rotation driving pinion 103 of the second shaft, is driven greatly into face by engagement Gear 104 rotates, and gear wheel is welded with third shaft 109 on 104 central axes, and therefore, third shaft 109 follows gear wheel 104 rotations, the first steering engine 105 are uniformly distributed along third shaft 109 and are fixedly mounted on casing 3, and the first steering engine 105 is arranged extremely It is 2 few, it is uniformly distributed along third shaft 109；First steering engine 105 and cross plate 108 are rotated with third shaft 109, the first steering engine First rudder arm 106 is installed, the first rudder arm 106 is connect by first connecting rod 107 with cross plate 108, the first steering engine on 105 105 stretch first connecting rod 107 by the rotation of the first rudder arm 106 and act on cross plate 108, and cross plate 108 is caused to incline Tiltedly, cross plate 108 is connect by the second connecting rod 110 with rotor folder 111, is equipped with main rotor 112 on rotor folder 111；Therefore The inclination of cross plate 108 drives the direction inclination of main rotor 112, and main motor 101 and the first steering engine 105 are connected by conducting wire and power supply It connects.Since the connection structure of cross plate 108 and main rotor 112 belongs to the prior art, therefore it is not described in further details.

506 level of fixed frame is fixedly installed with support frame 201, is fixedly installed with the second steering engine on 201 pedestal of support frame 202, the second steering engine 202 is equipped with the second rudder arm 203, and holder 205 is equipped on support frame 201, and the second rudder arm 203 passes through third Connecting rod 204 is connect with holder 205.Second steering engine 202 drives the rotation of the second rudder arm 203, is acted on by third connecting rod 204 In holder 205, rotate holder 205 around fixed link.Holder 205 is provided with support rod 211, is movably installed on support rod 211 Fixed disk 212, fixed disk 212 are fixedly installed with from motor 209, are equipped with and are fixedly installed with from rotor from motor 209 210, third steering engine 206 is fixedly installed on holder 205, and third steering engine 206 is equipped with third rudder arm 207, third rudder arm 207 It is connect by the 4th connecting rod 208 with fixed disk 212.Third steering engine 206 rotates related 4th company by controlling third rudder arm 207 Extension bar 208 acts on fixed disk 212, and control fixed disk 212 is fixed on the motion bar rotation of support rod 211 around it.Second rudder arm 203 with third rudder arm 207 at being vertically arranged；Support frame 201 and support rod 211 are at being vertically arranged；So the second rudder can be passed through Machine 202 and third steering engine 206 turning to from horizontal and vertical regulation fixed disk 212, to be carried out finely to vectored thrust system 2 Angle regulation.Second steering engine 202 and third steering engine 206 are connected to power supply by conducting wire.

The amphibious helicopter of No Tail Rotor high speed single rotor is in canard configuration.Helicopter uses canard configuration, in normal flight shape Not how many superiority under state, but when aircraft need to do big intensity it is motor-driven such as face upward, tight spiral movement when, or it is fast When fast forward motion, which is not only able to achieve the high-speed flight of remote unconventional helicopter, and structure is simple, eliminates conventional tail Paddle transmission parts, while two sets of thrust vectoring systems can be mutually backups, and ensure that whole aircraft reliability and safety.On the water surface When, it is downward that 2 angle of vectored thrust system can be regulated and controled, it can upward lift is provided, forward thrust can also be provided, Cooperate single rotor dynamical system 1, it can be with high-speed maneuver operation on the water surface.

Control module is installed on U-shaped part 501, control module and main motor 101, the first steering engine 105, the second steering engine 202, Third steering engine 206, laser detector 8, radar 9, sonar unit 11, camera 12 and signalling means 10 pass through electric data connection, control Molding block is connect with power supply by conducting wire.Regulate and control main motor 101, the first steering engine 105, the second steering engine 202 by control module Vector promotion is carried out with third steering engine 206, makes many fine highly difficult flare maneuvers.The control module, which has, to be connect It receives, storage, processing, release information function.The signalling means has the function of receiving and release news, since carbon fiber layer has Screen effect, control module are mounted on fuselage interior, in order to avoid helicopter is obstructed sending and receiving information, therefore letter are arranged Number device is for interact at letter with other smart machines or control module.

Solar battery 7 is thin-film solar cells or flexible solar battery.Curved surface can be carried out according to the surface of casing 3 Installation, and the pneumatic property of helicopter is not influenced；And thin-film solar cells or flexible solar battery are very thin, and weight is very Gently, little to the weight of fuselage.

Casing 3 includes entablature 301, fixing layer 302 and carbon fiber layer 303, and solar battery 7 is mounted on 3 outside of casing Carbon fiber layer 303.Carbon fibre material has excellent electric conductivity, has shielding action to electromagnetic wave；Alleviate helicopter Own wt, while strengthening the intensity of helicopter casing 3.Carbon fibre materials are 5 times of intensity of steel, 1/the 6 of quality, because This, casing structure intensity greatly promotes, and weight saving.

While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.

Claims (7)

1. a kind of amphibious helicopter of No Tail Rotor high speed single rotor, it is characterised in that: pushed away including single rotor dynamical system (1), vector Force system (2), casing (3), hull (4), rack (5), solar battery (7), radar (9), laser detector (8), signalling means (10), sonar unit (11), camera (12) and power supply；The structure of the amphibious helicopter of No Tail Rotor high speed single rotor is about machine Tool longitudinal axis (6) is symmetrical；

The rack (5) includes frame main body and both wings and layout triangular in shape, and the single rotor dynamical system (1) is fixed on machine In frame (5) main body, the vectored thrust system (2) is fixed on rack (5) both wings, and rack (5) main body is mounted on casing (3) Inside, rack (5) both wings pass through casing (3) from frame main body and are suspended from outside fuselage；The hull (4) is mounted on casing (3) Lower end；The solar battery (7) is mounted on the casing (3) of the unmanned plane upper half, and the radar (9) is mounted on ventral, The laser detector (8) is mounted on chain-drive section；The signalling means (10) is mounted on tail；Sonar unit (11) installation In drive end unit；The camera (12) is mounted on ventral；

Control module, the control module and main motor (101), the first steering engine (105), second are installed in the casing (3) Steering engine (202), third steering engine (206), laser detector (8), signalling means (10), sonar unit (11), camera (12) and thunder Pass through electric data connection up to (9), the control module connect with power supply by conducting wire, the control module with reception, store, Processing, release information function；Locating module is installed in the control module；4G module is installed on the signalling means (10)；

The power supply is single rotor dynamical system (1), laser detector (8), signalling means (10), sonar unit (11), camera (12), radar (9) and vectored thrust system (2) provide electric energy, and the solar battery (7) is connected to power supply by conducting wire, institute It states solar battery (7) and connects to power supply and be provided with rectification circuit, filter circuit, inversion regulating circuit in route；

The amphibious helicopter of No Tail Rotor high speed single rotor is in canard configuration；

The solar battery (7) is thin-film solar cells or flexible solar battery.

2. the amphibious helicopter of No Tail Rotor high speed single rotor according to claim 1, it is characterised in that: rack (5) packet Include U-shaped part (501), fixed frame (506), big square tube (502), the first small square tube (503), the second small square tube (504), round tube (505) and Fixing clamp-seat (507)；The U-shaped part (501) is opening down, and two sides are horizontally installed with big square tube by screw (502), big square tube (502) tail end is fixed with round tube (505) by Fixing clamp-seat (507), the round tube (505) with it is generous It is vertical to manage (502)；Round tube (505) end is mounted with fixed frame (506), and described first small square tube (503) one end is solid It is scheduled on big square tube (502) front end, the other end is fixed on fixed frame (506)；The fixed U-shaped in second small square tube (504) one end On part (501), the other end is fixed on fixed frame (506), and the first small square tube (503), the second small square tube (504) be not same On one horizontal plane.

3. the amphibious helicopter of No Tail Rotor high speed single rotor according to claim 2, it is characterised in that: the single rotor power System (1) is mounted on U-shaped part (501) bottom plate, and bottom plate front end is equipped with main motor (101), is installed on the main motor (101) There are first rotating shaft (113)；Base plate rear end is equipped with the second shaft (114), the first rotating shaft (113) by belt (102) with Second shaft (114) connection, second shaft (114) are fixed with pinion gear (103), the pinion gear (103) and gear wheel (104) it engages, is welded with third shaft (109) on gear wheel (104) central axes, the first steering engine (105) edge Third shaft (109) is uniformly distributed and is fixedly mounted on casing (3), is equipped with the first rudder arm on first steering engine (105) (106), first rudder arm (106) is connect by first connecting rod (107) with cross plate (108), and the cross plate (108) is logical It crosses the second connecting rod (110) to connect with rotor folder (111), main rotor (112) is installed on the rotor folder (111)；The master Motor (101) and the first steering engine (105) are connected to power supply by conducting wire.

4. the amphibious helicopter of No Tail Rotor high speed single rotor according to claim 2, it is characterised in that: the fixed frame (506) level is fixedly installed with support frame (201), is fixedly installed with the second steering engine (202) on support frame as described above (201) pedestal, Second steering engine (202) is equipped with the second rudder arm (203), is equipped on support frame as described above (201) holder (205), and described Two rudder arms (203) are connect by third connecting rod (204) with holder (205)；The holder (205) is provided with support rod (211), It being movably installed with fixed disk (212) on the support rod (211), the fixed disk (212) is fixedly installed with from motor (209), It is described be equipped with to be fixedly installed with from motor (209) be fixedly installed with third from rotor (210), the holder (205) Steering engine (206), the third steering engine (206) are equipped with third rudder arm (207), and the third rudder arm (207) passes through the 4th connection Bar (208) is connect with fixed disk (212)；Second rudder arm (203) and third rudder arm (207) are at being vertically arranged；The support Frame (201) and support rod (211) are at being vertically arranged；Second steering engine (202) and third steering engine (206) pass through conducting wire and power supply Connection.

5. the amphibious helicopter of No Tail Rotor high speed single rotor according to claim 1, it is characterised in that: casing (3) packet Entablature (301), fixing layer (302) and carbon fiber layer (303) are included, the solar battery (7) is mounted on the outside of casing (3) Carbon fiber layer (303).

6. the amphibious helicopter of No Tail Rotor high speed single rotor according to claim 1, it is characterised in that: the signalling means (10) With reception, send informational function.

7. the amphibious helicopter of No Tail Rotor high speed single rotor according to claim 1, it is characterised in that: the sonar unit It (11) is one kind of towed sonar or hand sonar.