CN210212793U - Dual-mode switching unmanned aerial vehicle - Google Patents
Dual-mode switching unmanned aerial vehicle Download PDFInfo
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- CN210212793U CN210212793U CN201920914624.2U CN201920914624U CN210212793U CN 210212793 U CN210212793 U CN 210212793U CN 201920914624 U CN201920914624 U CN 201920914624U CN 210212793 U CN210212793 U CN 210212793U
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Abstract
The application discloses unmanned aerial vehicle is switched to bimodulus belongs to the unmanned aerial vehicle field. Including unmanned aerial vehicle organism, mooring power supply system and non-mooring power supply system, the unmanned aerial vehicle organism includes equipment fixing board and slide rail, the slide rail sets up in equipment fixing board bottom, and form the power supply storehouse between equipment fixing board and the slide rail, mooring power supply system and non-mooring power supply system all can insert in the power supply storehouse and fix along the slide rail. This application utilizes the slide rail to form the power supply storehouse in equipment fixing board bottom, and mountable is tied and is stayed power supply system and non-and is tied and stay power supply system, can compatible advantage between them, enlarges unmanned aerial vehicle's application range, reduces use cost, and simultaneously, this switching mode simple structure, easy dismounting can realize the fast switch-over of two kinds of modes.
Description
Technical Field
The application relates to the field of unmanned aerial vehicles, in particular to a dual-mode switching unmanned aerial vehicle.
Background
Consumption level, the many rotor unmanned aerial vehicle of industrial level on the existing market are mostly mooring unmanned aerial vehicle and non-mooring unmanned aerial vehicle two kinds. The tethered unmanned aerial vehicle is powered by the tethered cable, has the advantage of long-time hovering, but is limited by the length of the tethered cable, so that the flying radius of the tethered unmanned aerial vehicle is smaller; the non-mooring unmanned aerial vehicle is not restricted by cables due to the adoption of a battery power supply mode, the flying radius is large, but the battery energy density is limited due to the limitation of the current battery technology, so that the endurance time of the unmanned aerial vehicle is short. Therefore, it is necessary to design a drone capable of switching between two modes (tethered mode and non-tethered mode).
SUMMERY OF THE UTILITY MODEL
The application provides a dual-mode switching unmanned aerial vehicle to solve the problem that proposes in the background art.
The utility model provides a bimodulus switches unmanned aerial vehicle, includes unmanned aerial vehicle organism, moors power supply system and non-mooring power supply system, the unmanned aerial vehicle organism includes equipment fixing board and slide rail, the slide rail sets up in equipment fixing board bottom, and form the power supply storehouse between equipment fixing board and the slide rail, mooring power supply system and non-mooring power supply system all can insert in the power supply storehouse and fix along the slide rail. This application utilizes the slide rail to form the power supply storehouse in equipment fixing board bottom, and mountable is tied and is stayed power supply system and non-and is tied and stay power supply system, can compatible advantage between them, enlarges unmanned aerial vehicle's application range, reduces use cost, and simultaneously, this switching mode simple structure, easy dismounting can realize the fast switch-over of two kinds of modes.
Preferably, mooring power supply system includes radiating bottom plate, mooring power supply shell, emergency battery, voltage conversion module, power monitoring module, comprehensive power supply connector and cable return bend, radiating bottom plate and mooring power supply shell are connected and are constituteed closed shell, emergency battery, voltage conversion module, power monitoring module and comprehensive power supply connector all are located mooring power supply shell to install on radiating bottom plate, the cable return bend sets up in radiating bottom plate bottom.
Preferably, a heat radiation fan is further arranged at the bottom of the heat radiation bottom plate. Can dispel the heat to the power supply system that moors through radiator fan, guarantee that the power supply system that moors can long-time operation.
Preferably, the non-tethered power supply system comprises a base plate, a non-tethered power supply housing, a lithium battery and a comprehensive power supply connector, the base plate and the non-tethered power supply housing are connected to form a closed housing, and the lithium battery and the comprehensive power supply connector are both located in the non-tethered power supply housing and are mounted on the base plate.
Preferably, the unmanned aerial vehicle organism still includes the upper plate, the upper plate sets up in equipment mounting panel top, and form the equipment cabin between upper plate and the equipment mounting panel.
Preferably, the flight control navigation system further comprises a flight control navigation system, wherein the flight control navigation system comprises a flight control module, a navigation module and an antenna, the flight control module and the navigation module are both positioned in the equipment cabin and are fixedly installed on the equipment installation plate, and the antenna is fixedly installed on the upper plate.
Preferably, the unmanned aerial vehicle further comprises a power system, wherein the power system comprises a horn, a disc type motor, a paddle and an electronic speed regulator, one end of the horn is connected with the unmanned aerial vehicle body, the other end of the horn is connected with the disc type motor, the paddle is fixedly connected with the disc type motor, and the electronic speed regulator is fixedly installed on the equipment installation plate.
Preferably, the paddle is a carbon fiber paddle. The carbon fiber has the advantages of light weight, high strength, high modulus, chemical corrosion resistance, small thermal expansion coefficient and the like, and has longer service life.
Preferably, unmanned aerial vehicle bottom of the body is equipped with the landing gear subassembly, the landing gear subassembly includes that undercarriage standpipe and undercarriage violently manage, the one end and the unmanned aerial vehicle bottom of the body of undercarriage standpipe are connected, and the other end is connected the undercarriage and is violently managed.
To sum up, the dual-mode switching unmanned aerial vehicle that this application provided, mountable mooring power supply system and non-mooring power supply system can compatible advantage between them, enlarges unmanned aerial vehicle's application range, reduces use cost, and simultaneously, this switching mode simple structure, easy dismounting can realize the fast switch-over of two kinds of modes.
Drawings
Fig. 1 is a schematic external view of a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 2 is a schematic internal structural diagram of a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 3 is a schematic structural diagram of a power supply cabin in a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 4 is a schematic external view of a tethered power supply system in a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 5 is a schematic view of an internal structure of a tethered power supply system in a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 6 is a schematic external view of a non-tethered power supply system in a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 7 is a schematic internal structural diagram of a non-tethered power supply system in a dual-mode switching unmanned aerial vehicle according to an embodiment of the present application;
fig. 8 is a schematic diagram of a dual-mode handover process of a dual-mode handover drone according to an embodiment of the present application.
Wherein: 10-unmanned aerial vehicle body, 101-equipment mounting plate, 102-sliding rail, 103-power supply cabin, 104-upper plate, 105-equipment cabin, 106-cabin connecting piece, 107-hood, 108-arm support, 109-motor base, 20-mooring power supply system, 201-radiating bottom plate, 202-mooring power supply shell, 203-emergency battery, 204-voltage conversion module, 205-power supply monitoring module, 206-comprehensive power supply connector, 207-cable elbow, 208-radiating fan, 30-non-mooring power supply system, 301-bottom plate, 302-non-mooring power supply shell, 303-lithium battery, 40-flight control navigation system, 401-flight control module, 402-navigation module, 403-antenna, 404-antenna support, 50-power system, 501-horn, 502-disc motor, 503-blade, 504-electronic governor, 60-landing assembly, 601-landing gear vertical tube, 602-landing gear horizontal tube, 603-landing gear connector, 604-landing gear support.
Detailed Description
In the following, the technical solutions in the embodiments will be clearly and completely described with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1 to 3, the application provides a dual-mode switching unmanned aerial vehicle, including unmanned aerial vehicle organism 10, mooring power supply system 20 and non-mooring power supply system 30, unmanned aerial vehicle organism 10 includes equipment mounting panel 101 and slide rail 102, equipment mounting panel 101 and the outside cover of slide rail 102 have aircraft bonnet 107, slide rail 102 sets up in equipment mounting panel 101 bottom, and connect through cabin connecting piece 106, form power supply bin 103 between slide rail 102 and equipment mounting panel 101, mooring power supply system 20 and non-mooring power supply system 30 all can insert in the power supply bin 103 and fix along slide rail 102, namely unmanned aerial vehicle is in the use, mooring power supply system 20 and non-mooring power supply system 30 all can be dismantled with power supply bin 103 and be connected, for example, fix on slide rail 102 through the thumb screw, realize freely switching.
The application provides a pair of dual-mode switches unmanned aerial vehicle, mountable mooring power supply system 20 and non-mooring power supply system 30, can compatible advantage between them, enlarge unmanned aerial vehicle's application range, both can hover for a long time, can carry out remote flight again, reduce use cost, simultaneously, this switching mode simple structure, easy dismounting can realize the fast switch-over of two kinds of modes.
Referring to fig. 2 and 3, the unmanned aerial vehicle body 10 further includes an upper plate 104, the upper plate 104 is disposed on the top of the equipment mounting plate 101 and connected by a horn support 108, and an equipment compartment 105 is formed between the upper plate 104 and the equipment mounting plate 101. The dual-mode switching unmanned aerial vehicle further comprises a flight control navigation system 40, the flight control navigation system 40 comprises a flight control module 401, a navigation module 402 and an antenna 403, the flight control module 401 and the navigation module 402 are located in the equipment cabin 105 and are installed and fixed on the equipment installation plate 101, and the antenna 403 is installed and fixed on the upper plate 104 through an antenna support 404.
With reference to fig. 1 to 3, the dual-mode switching unmanned aerial vehicle provided by the application further comprises a power system 50, the embodiment of the application uses a six-rotor unmanned aerial vehicle as an example, the power system 50 comprises 6 booms 501, 6 disc motors 502, a plurality of paddles 503 and an electronic governor 504, one end of each boom 501 is connected with the unmanned aerial vehicle body 10 through a boom support 108, the other end is connected with the disc motor 502 through a motor base 109, and the paddles 503 are fixedly connected with the disc motors 502, wherein the paddles 503 are carbon fiber paddles, because carbon fibers have a series of advantages of light weight, high strength, high modulus, chemical corrosion resistance, small thermal expansion coefficient and the like, the unmanned aerial vehicle has a long service life due to the design, and the electronic governor 504 is installed and fixed on the device mounting plate 101.
Referring to fig. 1, the dual mode switching unmanned aerial vehicle provided by the present application further includes landing gear assembly 60, and landing gear assembly 60 includes landing gear standpipe 601 and landing gear horizontal pipe 602, and landing gear horizontal pipe 602 is connected with landing gear standpipe 601 through landing gear connecting piece 603, and landing gear standpipe 601 passes through landing gear support 604 and links to each other with unmanned aerial vehicle organism 10 bottom.
Referring to fig. 4 and 5, among the dual-mode switching unmanned aerial vehicle that this application provided, mooring power supply system 20 includes radiating bottom plate 201, mooring power supply shell 202, emergency battery 203, voltage conversion module 204, power monitoring module 205, comprehensive power connector 206 and cable return bend 207, radiating bottom plate 201 and mooring power supply shell 202 are connected and are constituteed closed shell, improve the rain-proof dustproof performance of mooring power supply system 20, emergency battery 203, voltage conversion module 204, power monitoring module 205 and comprehensive power connector 206 all are located mooring power supply shell 202, and install on radiating bottom plate 201, cable return bend 207 sets up in radiating bottom plate 201 bottom, the line of control mooring cable, alleviate the influence of cable to unmanned aerial vehicle.
Referring to fig. 5, a heat dissipation fan 208 is further disposed at the bottom of the heat dissipation bottom plate 201 to dissipate heat of the tethered power supply system 20, so as to ensure long-term operation of the system.
Referring to fig. 6 and 7, the non-tethered power supply system 30 includes a bottom plate 301, a non-tethered power supply housing 302, a lithium battery 303 and a comprehensive power supply connector 206, the bottom plate 301 and the non-tethered power supply housing 302 are connected to form a closed housing, so as to improve the dust-proof and rain-proof performance of the non-tethered power supply system 30, and the lithium battery 303 and the comprehensive power supply connector 206 are both located in the non-tethered power supply housing 302 and are mounted on the bottom plate 301.
Referring to fig. 8, the dual-mode switching process of the dual-mode switching drone provided by the present application is as follows, taking the tethered power supply system 20 to switch to the non-tethered power supply system 30 as an example: firstly, the rear cover of the hood 107 is opened, the fasteners are taken down, the tethered power supply system 20 is pulled out from the slide rail 102, then the non-tethered power supply system 30 is pushed into the power supply bin 103 along the slide rail 102 until the comprehensive power supply connector 206 is butted and connected, the fasteners are used for screwing and fixing, and finally the rear cover of the hood 107 is closed, namely the whole switching process is completed. The switching process from the non-tethered power supply system 30 to the tethered power supply system 20 is based on the same principle and will not be described in detail.
Other embodiments of the present application will be apparent to those skilled in the art from consideration of the specification and practice of the application disclosed herein. This application is intended to cover any variations, uses, or adaptations of the invention following, in general, the principles of the application and including such departures from the present disclosure as come within known or customary practice within the art to which the invention pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the application being indicated by the following claims.
It will be understood that the present application is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the application is limited only by the appended claims.
Claims (9)
1. The utility model provides an unmanned aerial vehicle is switched to bimodulus, its characterized in that, includes unmanned aerial vehicle organism (10), moors power supply system (20) and non-moors power supply system (30), unmanned aerial vehicle organism (10) are including equipment mounting panel (101) and slide rail (102), slide rail (102) set up in equipment mounting panel (101) bottom, and form power supply storehouse (103) between equipment mounting panel (101) and slide rail (102), moor power supply system (20) and non-moors power supply system (30) all can insert in power supply storehouse (103) and fix along slide rail (102).
2. The dual-mode switching unmanned aerial vehicle of claim 1, wherein the tethered power supply system (20) comprises a heat dissipation bottom plate (201), a tethered power supply housing (202), an emergency battery (203), a voltage conversion module (204), a power monitoring module (205), a comprehensive power connector (206), and a cable elbow (207), the heat dissipation bottom plate (201) and the tethered power supply housing (202) are connected to form a closed housing, the emergency battery (203), the voltage conversion module (204), the power monitoring module (205), and the comprehensive power connector (206) are all located in the tethered power supply housing (202) and are installed on the heat dissipation bottom plate (201), and the cable elbow (207) is disposed at the bottom of the heat dissipation bottom plate (201).
3. The dual-mode switching unmanned aerial vehicle of claim 2, wherein a heat dissipation fan (208) is further arranged at the bottom of the heat dissipation bottom plate (201).
4. The dual-mode switching unmanned aerial vehicle of claim 1, wherein the non-tethered power supply system (30) comprises a base plate (301), a non-tethered power supply housing (302), a lithium battery (303), and a comprehensive power supply connector (206), wherein the base plate (301) and the non-tethered power supply housing (302) are connected to form a closed housing, and the lithium battery (303) and the comprehensive power supply connector (206) are both located in the non-tethered power supply housing (302) and are mounted on the base plate (301).
5. The dual-mode switching drone of claim 1, wherein the drone body (10) further includes an upper plate (104), the upper plate (104) being disposed on top of the equipment mounting plate (101) and forming an equipment bay (105) between the upper plate (104) and the equipment mounting plate (101).
6. The dual-mode switching unmanned aerial vehicle of claim 5, further comprising a flight control navigation system (40), wherein the flight control navigation system (40) comprises a flight control module (401), a navigation module (402), and an antenna (403), the flight control module (401) and the navigation module (402) are both located in the equipment compartment (105) and are fixedly installed on the equipment mounting plate (101), and the antenna (403) is fixedly installed on the upper plate (104).
7. The dual-mode switching unmanned aerial vehicle of claim 1, further comprising a power system (50), wherein the power system (50) comprises a horn (501), a disc motor (502), a blade (503) and an electronic governor (504), one end of the horn (501) is connected with the unmanned aerial vehicle body (10), the other end of the horn is connected with the disc motor (502), the blade (503) is fixedly connected with the disc motor (502), and the electronic governor (504) is fixedly mounted on the device mounting plate (101).
8. The dual mode switching drone of claim 7, wherein the paddle (503) is a carbon fiber paddle.
9. The dual-mode switching unmanned aerial vehicle of claim 1, wherein a landing gear assembly (60) is arranged at the bottom of the unmanned aerial vehicle body (10), the landing gear assembly (60) comprises a landing gear vertical pipe (601) and a landing gear horizontal pipe (602), one end of the landing gear vertical pipe (601) is connected with the bottom of the unmanned aerial vehicle body (10), and the other end of the landing gear vertical pipe is connected with the landing gear horizontal pipe (602).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920914624.2U CN210212793U (en) | 2019-06-18 | 2019-06-18 | Dual-mode switching unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920914624.2U CN210212793U (en) | 2019-06-18 | 2019-06-18 | Dual-mode switching unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN210212793U true CN210212793U (en) | 2020-03-31 |
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| CN201920914624.2U Active CN210212793U (en) | 2019-06-18 | 2019-06-18 | Dual-mode switching unmanned aerial vehicle |
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| CN (1) | CN210212793U (en) |
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