CN216186024U - Multi-functional photovoltaic power unmanned aerial vehicle - Google Patents

Multi-functional photovoltaic power unmanned aerial vehicle Download PDF

Info

Publication number
CN216186024U
CN216186024U CN202122194578.3U CN202122194578U CN216186024U CN 216186024 U CN216186024 U CN 216186024U CN 202122194578 U CN202122194578 U CN 202122194578U CN 216186024 U CN216186024 U CN 216186024U
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
support
damping spring
photovoltaic power
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN202122194578.3U
Other languages
Chinese (zh)
Inventor
杨睿
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Haian Rongke Textile Co Ltd
Original Assignee
Haian Rongke Textile Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Haian Rongke Textile Co Ltd filed Critical Haian Rongke Textile Co Ltd
Priority to CN202122194578.3U priority Critical patent/CN216186024U/en
Application granted granted Critical
Publication of CN216186024U publication Critical patent/CN216186024U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Photovoltaic Devices (AREA)

Abstract

The utility model discloses a multifunctional photovoltaic power unmanned aerial vehicle which comprises a machine body, wherein a solar photovoltaic panel is detachably connected to the upper portion of the machine body, a chute A is formed in the lower portion of the machine body, a support rod is connected to the inner side of the chute A in a sliding mode, a damping spring A is installed above the support rod, a connecting frame is detachably connected to the lower portion of the support rod, a support is welded to the lower portion of the connecting frame, a damping spring B is installed below the support, a support frame is installed on one side of the damping spring B, a chute B is formed in the inner side of the support frame, the inner side of the chute B is matched with the two ends of the support, an arm is detachably connected to the outer side of the machine body, and a paddle is detachably connected to the upper portion of the arm. According to the utility model, when the unmanned aerial vehicle lands on the ground, the machine body is damped, and the machine body is prevented from being damaged by the aid of the supporting frame, the sliding chute A, the sliding chute B, the supporting rod, the bracket, the connecting frame, the damping spring A, the non-slip mat and the damping spring B.

Description

Multi-functional photovoltaic power unmanned aerial vehicle
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a multifunctional photovoltaic power unmanned aerial vehicle.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Patent No. 201820256370.5 discloses an unmanned aerial vehicle, when this unmanned aerial vehicle was in non-flight state, can be through drawing in the accommodation space of locating on the fuselage with the horn in to reduce unmanned aerial vehicle's whole volume.
This unmanned aerial vehicle has following drawback: when the unmanned aerial vehicle is used, the camera cannot be taken into the interior of the body when the unmanned aerial vehicle descends, and the camera cannot be protected, so that the use is influenced; simultaneously when unmanned aerial vehicle descends to the ground, relatively to the shock attenuation effect of organism, influence the life of organism.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims to provide a multifunctional photovoltaic power unmanned aerial vehicle which can effectively solve the problems in the background technology.
In order to achieve the purpose, the utility model adopts the technical scheme that:
the utility model provides a multi-functional photovoltaic power unmanned aerial vehicle, includes the organism, the organism top can be dismantled and be connected with the solar photovoltaic board, spout A has been seted up to the organism below, spout A inboard sliding connection has branch, damping spring A is installed to the branch top, branch below can be dismantled and be connected with the link, the welding of link below has the support, damping spring B is installed to the support below, damping spring B installs the support frame in one side, spout B has been seted up to the support frame inboard, and spout B is inboard identical with the support both ends, the organism outside can be dismantled and be connected with the horn, the horn top can be dismantled and be connected with the paddle, the motor is installed on the inside top of organism.
Further, a rotating shaft is detachably connected below the motor, a threaded rod is detachably connected below the rotating shaft, a threaded sleeve is mounted on the outer side of the threaded rod, a fixed block is mounted on one side of the threaded sleeve, and a camera is detachably connected below the fixed block; through motor, pivot, thread bush, threaded rod and the fixed block of installation, when unmanned aerial vehicle descends, be convenient for take in the organism with the camera inside, protect the camera.
Furthermore, an anti-skid pad can be detachably connected below the supporting frame; through the slipmat of installation, avoid the support frame to take place to slide.
Further, the power output end of the motor is connected with the power input end of the rotating shaft; the threaded rod is driven to rotate by the installed motor and the rotating shaft.
Furthermore, the input ends of the motor and the camera are electrically connected with the output end of the solar photovoltaic panel; the electric equipment is used to work normally through the installed solar photovoltaic panel.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the unmanned aerial vehicle, the motor switch arranged at the top end in the machine body is turned on when the unmanned aerial vehicle descends, then the motor converts received electric energy into mechanical energy to drive the threaded rod below the rotating shaft to rotate, then the threaded rod drives the threaded sleeve on the outer side to move, then the threaded sleeve drives the camera arranged below the fixed block to move, and then the camera is collected into the machine body, so that the camera is protected conveniently.
2. According to the utility model, by the aid of the installed support frame, the chute A, the chute B, the supporting rod, the support, the connecting frame, the damping spring A, the non-slip mat and the damping spring B, when the unmanned aerial vehicle lands on the ground, the support installed below the connecting frame slides downwards in the chute B formed in the inner side of the support frame, then the damping spring B installed below the support presses downwards, then the damping spring B drives the connecting frame installed above the support to move upwards, then the supporting rod installed above the connecting frame slides in the chute A formed below the machine body, and then the damping spring A installed above the supporting rod starts to compress to generate elastic force, so that the purpose of shock absorption is achieved, and the machine body is prevented from being damaged.
Drawings
Fig. 1 is a schematic view of the overall structure of a multifunctional photovoltaic power unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic view of a front view cross-sectional structure of the multifunctional photovoltaic power unmanned aerial vehicle of the utility model;
fig. 3 is a schematic side view of a cross-sectional structure of a multifunctional photovoltaic unmanned aerial vehicle according to the present invention;
in the figure: 1. a solar photovoltaic panel; 2. a body; 3. a connecting frame; 4. a support frame; 5. a non-slip mat; 6. a horn; 7. a paddle; 8. a damping spring A; 9. a chute A; 10. a strut; 11. a damping spring B; 12. a support; 13. a chute B; 14. a motor; 15. a rotating shaft; 16. a threaded rod; 17. a camera; 18. a threaded sleeve; 19. and (5) fixing blocks.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.
As shown in fig. 1-3, a multi-functional photovoltaic power unmanned aerial vehicle, including organism 2, 2 tops of organism can be dismantled and be connected with solar photovoltaic board 1, spout a9 has been seted up to 2 below of organism, spout a9 inboard sliding connection has branch 10, damping spring A8 is installed to branch 10 top, branch 10 below can be dismantled and be connected with link 3, the welding of link 3 below has support 12, damping spring B11 is installed to support 12 below, support frame 4 is installed to damping spring B11 one side, spout B13 has been seted up to support frame 4 inboard, and spout B13 is inboard identical with support 12 both ends, 2 outside of organism can be dismantled and be connected with horn 6, 6 tops of horn can be dismantled and be connected with paddle 7, motor 14 is installed on 2 inside tops of organism.
A rotating shaft 15 is detachably connected below the motor 14, a threaded rod 16 is detachably connected below the rotating shaft 15, a threaded sleeve 18 is mounted on the outer side of the threaded rod 16, a fixed block 19 is mounted on one side of the threaded sleeve 18, and a camera 17 is detachably connected below the fixed block 19; through motor 14, pivot 15, thread bush 18, threaded rod 16 and the fixed block 19 of installation, when unmanned aerial vehicle descends, be convenient for take in camera 17 inside organism 2, protect camera 17.
Wherein, the lower part of the supporting frame 4 can be detachably connected with an anti-skid pad 5; the sliding of the support frame 4 is avoided by the installed non-slip mat 5.
Wherein, the power output end of the motor 14 is connected with the power input end of the rotating shaft 15; the threaded rod 16 is driven to rotate by the motor 14 and the rotating shaft 15.
The input ends of the motor 14 and the camera 17 are electrically connected with the output end of the solar photovoltaic panel 1; the electric equipment is used to work normally through the installed solar photovoltaic panel 1.
It should be noted that, when the multifunctional photovoltaic power unmanned aerial vehicle is used, when the unmanned aerial vehicle descends, a switch of a motor 14 installed at the top end inside a machine body 2 is turned on, then the motor 14 converts received electric energy into mechanical energy to drive a threaded rod 16 below a rotating shaft 15 to rotate, then the threaded rod 16 drives a threaded sleeve 18 on the outer side to move, then the threaded sleeve 18 drives a camera 17 installed below a fixed block 19 to move, then the camera 17 is put into the machine body 2 to be convenient for protecting the camera 17, when the unmanned aerial vehicle descends to the ground, a support 12 installed below a connecting frame 3 slides downwards in a sliding groove B13 formed in the inner side of a support frame 4, then a damping spring B11 installed below the support 12 presses downwards, then the damping spring B11 drives the connecting frame 3 installed above the support 12 to move upwards, then a support rod 10 installed above the connecting frame 3 slides in a sliding groove A9 formed in the lower side of the machine body 2, then the damping spring A8 installed above the supporting rod 10 begins to compress to generate elastic force, thereby achieving the purpose of shock absorption and avoiding the machine body 2 from being damaged.
The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims (5)

1. The utility model provides a multi-functional photovoltaic power unmanned aerial vehicle, includes organism (2), its characterized in that, organism (2) top can be dismantled and be connected with solar photovoltaic board (1), spout A (9) have been seted up to organism (2) below, spout A (9) inboard sliding connection has branch (10), damping spring A (8) are installed to branch (10) top, but branch (10) below is dismantled and is connected with link (3), the welding of link (3) below has support (12), damping spring B (11) are installed to support (12) below, damping spring B (11) one side is installed support frame (4), spout B (13) have been seted up to support frame (4) inboard, and spout B (13) inboard is identical with support (12) both ends, organism (2) outside can be dismantled and be connected with horn (6), the paddle (7) is detachably connected to the upper portion of the machine arm (6), and the motor (14) is installed at the top end inside the machine body (2).
2. The multifunctional photovoltaic power unmanned aerial vehicle of claim 1, wherein: motor (14) below is detachable to be connected with pivot (15), pivot (15) below is detachable to be connected with threaded rod (16), threaded sleeve (18) are installed in threaded rod (16) outside, fixed block (19) are installed to threaded sleeve (18) one side, fixed block (19) below is detachable to be connected with camera (17).
3. The multifunctional photovoltaic power unmanned aerial vehicle of claim 1, wherein: the lower part of the support frame (4) can be detachably connected with an anti-skid pad (5).
4. The multifunctional photovoltaic power unmanned aerial vehicle of claim 1, wherein: and the power output end of the motor (14) is connected with the power input end of the rotating shaft (15).
5. The multifunctional photovoltaic power unmanned aerial vehicle of claim 1, wherein: the input ends of the motor (14) and the camera (17) are electrically connected with the output end of the solar photovoltaic panel (1).
CN202122194578.3U 2021-09-11 2021-09-11 Multi-functional photovoltaic power unmanned aerial vehicle Expired - Fee Related CN216186024U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122194578.3U CN216186024U (en) 2021-09-11 2021-09-11 Multi-functional photovoltaic power unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122194578.3U CN216186024U (en) 2021-09-11 2021-09-11 Multi-functional photovoltaic power unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN216186024U true CN216186024U (en) 2022-04-05

Family

ID=80919267

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202122194578.3U Expired - Fee Related CN216186024U (en) 2021-09-11 2021-09-11 Multi-functional photovoltaic power unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN216186024U (en)

Similar Documents

Publication Publication Date Title
CN209097009U (en) A kind of damping device of unmanned plane during flying device
CN216186024U (en) Multi-functional photovoltaic power unmanned aerial vehicle
CN211001803U (en) Can dismantle unmanned aerial vehicle anticollision support
CN216546682U (en) Unmanned aerial vehicle for collecting plant samples
CN218877559U (en) Adjustable flexible blade subassembly that aircraft was used
CN216332732U (en) Scalable comprehensive protection device of unmanned aerial vehicle
CN215794502U (en) A cloud platform elevating system for surveying and mapping unmanned aerial vehicle
CN216861845U (en) Combined unmanned aerial vehicle
CN213200087U (en) Carbon fiber unmanned machine shell
CN210284606U (en) Unmanned aerial vehicle wing is with flexible protective structure
CN113895622A (en) Unmanned aerial vehicle's safety protection structure
CN211107970U (en) Unmanned aerial vehicle is with frame shock-absorbing structure that plays
CN210338273U (en) Survey and survey unmanned aerial vehicle to complicated mountain area topography
CN210971520U (en) Unmanned aerial vehicle horn structure capable of improving flight stability
CN211630857U (en) Unmanned aerial vehicle mows
CN214930596U (en) Scalable shooting unmanned aerial vehicle
CN213323660U (en) Portable many rotor unmanned aerial vehicle
CN216232952U (en) Filtering device for efficient damping of power system of unmanned aerial vehicle
CN215043689U (en) Unmanned aerial vehicle with shock-absorbing function
CN214986034U (en) Shock absorption support for unmanned aerial vehicle
CN214216171U (en) Unmanned aerial vehicle frame supporting device for life cycle test of unmanned aerial vehicle
CN211568292U (en) Special undercarriage of small-size reconnaissance unmanned aerial vehicle
CN211107960U (en) Shock absorption support for lifting of surveying and mapping unmanned aerial vehicle
CN214776533U (en) A take off and land device for mooring unmanned aerial vehicle
CN108910055A (en) A kind of unmanned plane with high security

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
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: 20220405