CN206288236U - A kind of multiaxis rescues unmanned plane - Google Patents

A kind of multiaxis rescues unmanned plane Download PDF

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Publication number
CN206288236U
CN206288236U CN201620898594.7U CN201620898594U CN206288236U CN 206288236 U CN206288236 U CN 206288236U CN 201620898594 U CN201620898594 U CN 201620898594U CN 206288236 U CN206288236 U CN 206288236U
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China
Prior art keywords
unmanned plane
multiaxis
engine
rescues
fixed
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Expired - Fee Related
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CN201620898594.7U
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Chinese (zh)
Inventor
王典
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Individual
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Individual
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Priority to CN201620898594.7U priority Critical patent/CN206288236U/en
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Publication of CN206288236U publication Critical patent/CN206288236U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of multiaxis rescues unmanned plane, belongs to unmanned air vehicle technique field, including fixed-wing unmanned plane and engine;It is characterized in that:Also include camera head, laser locating apparatus, wireless communication apparatus, loudspeaker, power supply and parachute;Parachute is arranged at fixed-wing unmanned plane tail;Engine is flexibly connected by connecting rod with fixed-wing unmanned plane;Connecting rod is made up of vertical rod and rotating bar;Vertical rod is fixedly connected by its upper end with body, and vertical rod lower end is fixedly connected with engine.By the connected mode for improving fixed-wing unmanned plane its engine and fuselage so that multiaxis rescue unmanned plane has been provided simultaneously with the speed of fixed-wing unmanned plane and the function of the landing of multiaxis aircraft vertical and hovering.Cause that unmanned plane described in the utility model possesses the advantage that quick positioning rescue target and defence air crash occur simultaneously, and it is simple to operate, it is suitable to popularization and application.

Description

A kind of multiaxis rescues unmanned plane
Technical field
The utility model belongs to unmanned air vehicle technique field, more particularly to a kind of multiaxis rescue unmanned plane.
Background technology
Unmanned plane is developed rapidly and produced by recently as radiotechnics, remote control technology and computer technology A new things, its advantage can be VTOL, and operation is flexible, but also can be connected with computer, and then Automatic flight and Intelligent flight are realized, and its use scope widely, is divided into dual-use two kinds.Current market On unmanned plane be that, mostly with lithium battery as power, but lithium battery can not meet its power demand.Often appear as continuous ETS estimated time of sailing is short, and battery is heavier, civilian unmanned plane mostly based on entertaining or take photo by plane, using scope than narrow, not The application potential that unmanned plane had originally can be played, fails to give full play to its effect in rescue field.
The content of the invention
The utility model aims to solve the problem that above mentioned problem, there is provided a kind of multiaxis rescue unmanned plane that can be applied to rescue field.
A kind of multiaxis rescue unmanned plane described in the utility model, including fixed-wing unmanned plane and engine;Also include Camera head, laser locating apparatus, wireless communication apparatus, loudspeaker, power supply and parachute;The camera head, laser positioning Device, wireless communication apparatus, loudspeaker and power supply may be contained within fixed-wing unmanned plane;The parachute be arranged at fixed-wing without At man-machine tail;The engine is flexibly connected by connecting rod with fixed-wing unmanned plane;The connecting rod is by vertical rod and turns Lever is constituted;The vertical rod is fixedly connected by its upper end with body, and its lower end is connected with rotating bar upper end by transmission device Connect, rotating bar can be rotated around transmission device;The vertical rod lower end is fixedly connected with engine.When rescue is implemented, power supply is Unmanned plane provides electric energy, for engine thereon and various device normal works;Video camera is used to shoot region figure described in unmanned plane Piece looks for rescue target;Laser locating apparatus look for positioning rescue target for auxiliary;Wireless communication apparatus be used for receive for The control signal of unmanned plane, while can be used for the temporary communications with the rescue target looked for;Loudspeaker is used for unmanned plane and quilt Oppressive member's proximity communication;Parachute is used for guarding against the urgent aviation accident for occurring in the air.Connecting rod is in extended configuration, not When rotating, unmanned plane normal flight;After connecting rod is rotated, according to the direction that engine is rotated with vertical rod, unmanned plane can Change of flight direction, to adapt to the rescue environment of complexity.
Multiaxis described in the utility model rescues unmanned plane, and the transmission device is steering wheel, is realized in connecting rod by it The rotation of rotating bar.
Multiaxis described in the utility model rescues unmanned plane, the rotating bar of the connecting rod through foregoing steering wheel rotational angle It is 90 °;The longitudinal section for rotating rear connecting rod is L-shape;When connecting rod is in extended configuration, vertical rod is located at same with rotating bar On straight line, engine is the level of state;After the completion of rotating bar rotation, one 90 ° of angles, hair are formed between rotating bar and vertical rod Motivation in vertical state, makes unmanned plane to realize the function of VTOL and hovering.
Multiaxis described in the utility model rescues unmanned plane, and the engine is turbogenerator;The turbogenerator Three are included, is respectively arranged at immediately below the wing of both sides and immediately below tail.Three turbogenerators can independently work, By any combination of three turbogenerators realize multiaxis rescue unmanned plane highly difficult flight control so that its can compared with Implement rescue under complex environment.
Multiaxis described in the utility model rescues unmanned plane, and the laser locating apparatus include that generating laser and laser are chased after Track device, when implementing rescue, is strafed by generating laser in rescue region, and laser traces are passed through after rescue target to be found Device can simultaneously obtain the particular location of rescue target, improve rescue efficiency.
Multiaxis described in the utility model rescues unmanned plane, and the camera head is thermal imaging high-definition camera, by it Thermal imaging is beneficial to find trapped personnel from woods dense.
Multiaxis described in the utility model rescues unmanned plane, and the wireless communication apparatus include micro-cells signal base station, It is convenient after trapped personnel is locked when rescue is implemented, and trapped personnel contact.Because some places do not have mobile phone signal, lead Cause misses optimal rescue opportunity, can just be contacted with rescue personnel by micro-cells base station, makes trapped personnel quilt faster Rescue, improve rescue efficiency.
Multiaxis described in the utility model rescues unmanned plane, and the power supply is fuel cell, using this battery efficiency more Height, more cleans, and renewable, can extend cruising time, can strive for that more times perform more rescue tasks.
Multiaxis described in the utility model rescues unmanned plane, and its engine is improved with fuselage by fixed-wing unmanned plane Connected mode so that multiaxis rescue unmanned plane described in the utility model has been provided simultaneously with the speed and multiaxis of fixed-wing unmanned plane Aircraft vertical landing and the function of hovering.Simultaneously by being applied in combination on unmanned plane camera head, laser locating apparatus, wireless Communication device, loudspeaker and parachute so that unmanned plane described in the utility model possesses quick positioning rescue target and prevents The advantage that standby air crash occurs, and it is simple to operate, it is suitable to popularization and application.
Brief description of the drawings
Fig. 1 is theory structure schematic block diagram of the present utility model;
Fig. 2 is connecting rod extended configuration schematic diagram described in the utility model;
Fig. 3 is connecting rod rotary state schematic diagram described in the utility model;
Wherein 1- wings, 2- steering wheels, 3- engines, 4- vertical rods, 5- rotating bars.
Specific embodiment
Below in conjunction with the accompanying drawings and embodiment is illustrated to the utility model:
A kind of multiaxis rescue unmanned plane described in the utility model, as shown in figure 1, including fixed-wing unmanned plane and engine 3;Also include camera head, laser locating apparatus, wireless communication apparatus, loudspeaker, power supply and parachute;The shooting dress Put, laser locating apparatus, wireless communication apparatus, loudspeaker and power supply may be contained within fixed-wing unmanned plane;The parachute sets It is placed at fixed-wing unmanned plane tail;The engine 3 is flexibly connected by connecting rod with fixed-wing unmanned plane;As shown in Fig. 2 The connecting rod is made up of vertical rod 4 and rotating bar 5;The vertical rod 4 is fixedly connected by its upper end with body, its lower end with The upper end of rotating bar 5 is connected by transmission device, and rotating bar 5 can be rotated around transmission device;The transmission device is steering wheel 2, described The lower end of vertical rod 4 is fixedly connected with engine 3.As shown in figure 3, the rotating bar 5 of connecting rod is through the rotational angle of foregoing steering wheel 2 90°;The longitudinal section for rotating rear connecting rod is L-shape;The engine 3 is turbogenerator 3;The turbogenerator 3 is included Three, it is respectively arranged at immediately below both sides wing 1 and immediately below tail.The laser locating apparatus include generating laser and swash Light tracker, the camera head is thermal imaging high-definition camera, and wireless communication apparatus include micro-cells signal base station, described Power supply is fuel cell.
When rescue is implemented, power supply provides electric energy for unmanned plane, for engine 3 thereon and various device normal works, three Individual turbogenerator 3 can independently work, and realize that multiaxis rescues unmanned plane by any combination of three turbogenerators 3 Highly difficult flight control, so that it can be compared with implementation rescue under complex environment.It is higher using fuel cell efficiency, more clean, And it is renewable, cruising time can be extended, can strive for that more times perform more rescue tasks.Video camera is used to clap Take the photograph region picture described in unmanned plane and look for rescue target, camera head is thermal imaging high-definition camera, is beneficial to by its thermal imaging Trapped personnel is found from woods dense.Laser locating apparatus look for positioning rescue target, laser locating apparatus for auxiliary Including generating laser and laser traces device, strafed in rescue region by generating laser, after rescue target to be found The particular location of rescue target can be simultaneously obtained by laser traces device, rescue efficiency is improved.Wireless communication apparatus are used to receive For the control signal of unmanned plane, while can be used for the temporary communications with the rescue target looked for, wireless communication apparatus include Micro-cells signal base station, it is convenient after trapped personnel is locked when rescue is implemented, and trapped personnel contact.Because some ground Side has led to miss optimal rescue opportunity without mobile phone signal, can just be contacted with rescue personnel by micro-cells base station, makes Trapped personnel is rescued faster, improves rescue efficiency.Loudspeaker is used for unmanned plane and trapped personnel proximity communication;Parachute For guarding against the urgent aviation accident for occurring in the air.Connecting rod is in extended configuration, and when not rotating, unmanned plane normally flies OK;After connecting rod is rotated, according to the direction that engine 3 is rotated with vertical rod 4, unmanned plane can change of flight direction, work as connecting rod Vertical rod 4 is located along the same line with rotating bar 5 during in extended configuration, and engine 3 is the level of state;When rotating bar 5 is rotated After the completion of, one 90 ° of angles are formed between rotating bar 5 and vertical rod 4, engine 3 in vertical state, makes unmanned plane to realize vertically Landing and the function of hovering, to adapt to the rescue environment of complexity.

Claims (8)

1. a kind of multiaxis rescues unmanned plane, including fixed-wing unmanned plane and engine(3);It is characterized in that:Also include shooting Device, laser locating apparatus, wireless communication apparatus, loudspeaker, power supply and parachute;The camera head, laser locating apparatus, Wireless communication apparatus, loudspeaker and power supply may be contained within fixed-wing unmanned plane;The parachute is arranged at fixed-wing unmanned plane At tail;The engine(3)It is flexibly connected with fixed-wing unmanned plane by connecting rod;The connecting rod is by vertical rod(4)With Rotating bar(5)Composition;The vertical rod(4)It is fixedly connected with body by its upper end, its lower end and rotating bar(5)Upper end passes through Transmission device is connected, rotating bar(5)Can be rotated around transmission device;The vertical rod(4)Lower end and engine(3)It is fixedly connected.
2. multiaxis according to claim 1 rescues unmanned plane, it is characterised in that:The transmission device is steering wheel(2).
3. multiaxis according to claim 2 rescues unmanned plane, it is characterised in that:The rotating bar of the connecting rod(5)It is premenstrual State steering wheel(2)Rotational angle be 90 °;The longitudinal section for rotating rear connecting rod is L-shape.
4. multiaxis according to claim 3 rescues unmanned plane, it is characterised in that:The engine(3)It is turbogenerator; The turbogenerator includes three, is respectively arranged at both sides wing(1)Immediately below underface and tail.
5. multiaxis according to claim 4 rescues unmanned plane, it is characterised in that:The laser locating apparatus are sent out including laser Emitter and laser traces device.
6. multiaxis according to claim 5 rescues unmanned plane, it is characterised in that:The camera head is taken the photograph for thermal imaging high definition As head.
7. multiaxis according to claim 6 rescues unmanned plane, it is characterised in that:The wireless communication apparatus include miniature hand Machine signal base station.
8. multiaxis according to claim 7 rescues unmanned plane, it is characterised in that:The power supply is fuel cell.
CN201620898594.7U 2016-08-18 2016-08-18 A kind of multiaxis rescues unmanned plane Expired - Fee Related CN206288236U (en)

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Application Number Priority Date Filing Date Title
CN201620898594.7U CN206288236U (en) 2016-08-18 2016-08-18 A kind of multiaxis rescues unmanned plane

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CN201620898594.7U CN206288236U (en) 2016-08-18 2016-08-18 A kind of multiaxis rescues unmanned plane

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108492525A (en) * 2018-05-10 2018-09-04 湖北师范大学 A kind of the indoor human body tumble position monitor rescue skills and system of Multi-information acquisition

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108492525A (en) * 2018-05-10 2018-09-04 湖北师范大学 A kind of the indoor human body tumble position monitor rescue skills and system of Multi-information acquisition

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170630

Termination date: 20210818