CN218751490U - Unmanned aerial vehicle floor stand - Google Patents
Unmanned aerial vehicle floor stand Download PDFInfo
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- CN218751490U CN218751490U CN202223553015.XU CN202223553015U CN218751490U CN 218751490 U CN218751490 U CN 218751490U CN 202223553015 U CN202223553015 U CN 202223553015U CN 218751490 U CN218751490 U CN 218751490U
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- 210000001503 joint Anatomy 0.000 claims description 24
- 239000000463 material Substances 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 5
- 238000009434 installation Methods 0.000 description 5
- 230000003139 buffering effect Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 230000002633 protecting effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle falls to ground support, the on-line screen storage device comprises a base, the top fixedly connected with fixing base of base, the top of fixing base is provided with bracing piece one, the bottom fixedly connected with screw thread head of bracing piece one, the top of fixing base is provided with screw thread groove one, be screw-thread fit setting between screw thread head one and the screw thread groove one, the top fixedly connected with buffer beam of bracing piece one, and the top of bracing piece one is provided with bracing piece two, be provided with the dashpot in the bracing piece two, nested sliding connection has the buffer block in the dashpot, and is connected with buffer spring between buffer block inner wall and the buffer block surface, the top of buffer beam and the bottom fixed connection of buffer block. The utility model discloses in, through the base of rubber material, can be when unmanned aerial vehicle falls to the ground, whole support earlier with the ground contact, can eliminate the striking vibration that part touched ground and produced, reduce the vibrations damage of effort to unmanned aerial vehicle part structure.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle support technical field especially relates to an unmanned aerial vehicle falls to ground support.
Background
Unmanned aerial vehicle, be the unmanned aerial vehicle that utilizes radio remote control equipment and the program control device of self-contained to control, or by the vehicle-mounted computer completely or intermittently independently operate, because unmanned aerial vehicle itself possesses good space mobility characteristic, consequently in the field of taking photo by plane, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, the disaster relief, movie & TV is shot, make romantic etc. all need very extensive application, unmanned aerial vehicle can receive the operation influence when the flight falls to the ground usually, produce the striking when falling to the ground easily, consequently in order to promote unmanned aerial vehicle's safety in utilization, there is certain demand to the unmanned aerial vehicle that promotes unmanned aerial vehicle and falls to the ground support that the security falls to the ground.
Some unmanned aerial vehicle of having now fall to the ground support, most do not have buffering effect, consequently when unmanned aerial vehicle falls to the ground, receive the inertia effect that ground topography and unmanned aerial vehicle itself fall to the ground for unmanned aerial vehicle can produce the striking vibrations, leads to the not hard up circumstances of damaging of the inside spare part of unmanned aerial vehicle very easily, and the support of conventionality is the integral type mostly moreover, can't convenient when not using be received and deposited, uses and lacks the convenience.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle that provides falls to the ground support.
In order to realize the purpose, the utility model adopts the following technical scheme: the utility model provides an unmanned aerial vehicle falls to ground support, includes the base, the top fixedly connected with fixing base of base, the top of fixing base is provided with bracing piece one, the first bottom fixedly connected with thread head of bracing piece one, the top of fixing base is provided with thread groove one, be screw-thread fit setting between thread head one and the thread groove one, the top fixedly connected with buffer beam of bracing piece one, and the top of bracing piece one is provided with bracing piece two, be provided with the dashpot in the bracing piece two, nested sliding connection has the buffer block in the dashpot, and is connected with buffer spring between dashpot inner wall and the buffer block surface, the top of buffer beam and the bottom fixed connection of buffer block, the top of bracing piece two is rotated and is connected with the operation block, and the top of bracing piece two is provided with the supporting seat, the top fixedly connected with thread head two of operation block, the bottom of supporting seat is provided with thread groove two, be screw-thread fit setting between thread head two and the thread groove two, the top of supporting seat is provided with the unmanned aerial vehicle frame, and the top fixedly connected with butt joint piece of supporting seat, the position that meets with the inside groove, be provided with the anti-off spring is connected with the anti-off the inner wall of the fixed connection of supporting seat.
As a further description of the above technical solution:
the base all is provided with two and corresponds the bottom both sides position of position unmanned aerial vehicle frame, every bracing piece one, bracing piece two between base and the supporting seat all are provided with two.
As a further description of the above technical solution:
the base is made of rubber.
As a further description of the above technical solution:
the supporting seat is provided with a through groove communicated with the inner groove, and the connecting rod is connected with the through groove in a nested sliding mode.
As a further description of the above technical solution:
one end of the connecting rod is fixedly connected with an operating ring at the position outside the supporting seat.
As a further description of the above technical solution:
the butt joint piece and the butt joint groove are arranged in a splicing matching mode, and the anti-falling block and the anti-falling groove are arranged in a splicing matching mode.
The utility model discloses following beneficial effect has:
this unmanned aerial vehicle floor stand:
1. through the base made of rubber, when the unmanned aerial vehicle falls to the ground, the whole support is firstly contacted with the ground, the impact vibration sense generated by partial contact with the ground can be eliminated, the vibration damage of acting force to an unmanned aerial vehicle component structure is reduced, and meanwhile, the impact effect and the inertia effect generated when the unmanned aerial vehicle falls to the ground can be effectively buffered and reduced by matching with the arrangement of the buffer block and the buffer spring lamp structure, so that the stable protection work for falling of the unmanned aerial vehicle is realized, and the falling safety of the unmanned aerial vehicle is greatly improved;
2. through the thread head structure that sets up and to the cooperation setting of butt joint piece, butt joint groove, anticreep piece, anticreep groove isotructure, can make whole supporting structure can stabilize the aggregate erection and convenient installation in the unmanned aerial vehicle frame, also can carry out quick convenient dismantlement operation simultaneously, structural connection is stable, and easy operation is convenient, uses nimble convenience very.
Drawings
Fig. 1 is a schematic view of an overall structure of a landing support of an unmanned aerial vehicle according to the present invention;
fig. 2 is a front view of the landing support of the unmanned aerial vehicle according to the present invention;
fig. 3 is the utility model provides an unmanned aerial vehicle falls to ground a's enlargements in fig. 2 of support.
Illustration of the drawings:
1. a base; 2. a fixed seat; 3. a first supporting rod; 4. a first thread head; 5. a first thread groove; 6. a buffer rod; 7. a second supporting rod; 8. a buffer tank; 9. a buffer block; 10. a buffer spring; 11. an operation block; 12. a supporting base; 13. a second thread head; 14. a second thread groove; 15. an unmanned aerial vehicle frame; 16. a docking member; 17. an inner tank; 18. a movable block; 19. a connecting rod; 20. a through groove; 21. an operating ring; 22. a positioning spring; 23. an anti-drop block; 24. a butt joint groove; 25. and (4) an anti-drop groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely 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 efforts all belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-3, the present invention provides an embodiment: an unmanned aerial vehicle landing support comprises a base 1, a fixed seat 2 is fixedly connected to the top of the base 1, a first support rod 3 is arranged above the fixed seat 2, a first screw thread head 4 is fixedly connected to the bottom end of the first support rod 3, a first screw thread groove 5 is arranged at the top of the fixed seat 2, the first screw thread head 4 is matched with the first screw thread groove 5 to enable the first support rod 3 to be stably installed in a butt joint mode with the base 1, so that the whole support structure can be stably installed and conveniently disassembled, the first support rod 4 can be conveniently stored when the unmanned aerial vehicle landing support is not used, a first screw thread groove 5 is arranged between the first screw thread head 4 and the first screw thread groove, a second buffer rod 6 is fixedly connected to the top end of the first support rod 3, a second support rod 7 is arranged above the first support rod 3, a buffer block 9 is arranged in the second support rod 7 in a nested and sliding connection mode, a buffer spring 10 is connected between the inner wall of the buffer block 8 and the outer surface of the buffer block 9, the top end of the buffer rod 6 is fixedly connected with the bottom end of the buffer block 9, the buffer block 7 can be conveniently operated when the base 1 is in contact with the ground, the collision force, the support structure, the support rod 14 is arranged, the buffer block 11, the buffer block can be conveniently operated, and the buffer block 14, the buffer block can be conveniently operated, the buffer block 14, the buffer block can be conveniently arranged, the buffer block can be conveniently operated, the buffer block 11, the buffer block can be operated, the buffer block can be conveniently operated by the buffer block 12, the top of supporting seat 12 is provided with unmanned aerial vehicle frame 15, and the top fixedly connected with butt joint 16 of supporting seat 12, butt joint 16 and supporting seat 12 position of meeting are provided with inside groove 17, sliding connection has movable block 18 in the inside groove 17, fixedly connected with connecting rod 19 on the movable block 18, and be connected with positioning spring 22 between the surface of movable block 18 and the inside groove 17 inner wall, positioning spring 22 all is located the same one side of movable block 18 surface with connecting rod 19, fixedly connected with anticreep piece 23 on the movable block 18, anticreep piece 23 then is located movable block 18 surface and keeps away from positioning spring 22 one side, and keep away from connecting rod 19 one end, the bottom of unmanned aerial vehicle frame 15 is provided with butt joint groove 24, butt joint groove 24 inner wall is provided with anticreep groove 25.
The base 1 is made of rubber, and when the rubber is wear-resistant and durable, the base can also absorb some impact shock generated by contacting the ground when falling to the ground, so that a good buffering and protecting effect is achieved.
The supporting seat 12 is provided with a through groove 20 communicated with the inner groove 17, the connecting rod 19 is in nested sliding connection with the through groove 20, and the connecting rod 19 can be stably operated and used due to the arrangement of the structure.
One end of the connecting rod 19 is fixedly connected with an operating ring 21 at the outer side of the supporting seat 12, and the operation convenience of the whole structure can be improved due to the arrangement of the operating ring 21.
For pegging graft cooperation setting between interfacing part 16 and the butt joint groove 24, for pegging graft cooperation setting between anticreep piece 23 and the anticreep groove 25, the setting of this structure can be so that whole supporting structure can be stable with unmanned aerial vehicle frame 15 butt joint installation together, also can conveniently dismantle simultaneously and get off, conveniently take in and deposit.
The working principle is as follows: when using unmanned aerial vehicle to fall to the ground support, twist into screw thread groove one 5 with first 4 screw thread heads, can be with bracing piece one 3 and base 1 butt joint installation, rotate operation piece 11, make in screw thread head two 13 twists screw thread groove two 14, can accomplish the butt joint of bracing piece two 7 and supporting seat 12, from this can be with mounting structure combination installation, pulling operation ring 21, operation ring 21 drives anticreep piece 23 shrink through connecting rod 19 pulling movable block 18 compression positioning spring 22 simultaneously, go into butt joint 16 card in butt joint groove 24, unclamp operation ring 21 after the card is gone into, positioning spring 22 resets and drives anticreep piece 23 card and go into anticreep groove 25, can accomplish the butt joint installation of mounting structure and unmanned aerial vehicle frame 15, when unmanned aerial vehicle falls to the ground, base 1 contacts with ground earlier, the striking touching sense of a part production can be subducted to base 1 of rubber material, while the effort of inertia in the frame drives bracing piece two 7 to remove, the reaction compression buffer spring 10 of buffer bar 6, can slowly cushion the effort, thereby can play fine protection effect to unmanned aerial vehicle subduct, whole mounting structure can dismantle in the same reason operation, it is convenient to deposit.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions on some technical features, and any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle falls to ground support, includes base (1), its characterized in that: the top of the base (1) is fixedly connected with a fixing seat (2), a first support rod (3) is arranged above the fixing seat (2), a first screw thread head (4) is fixedly connected to the bottom end of the first support rod (3), a first screw thread groove (5) is arranged at the top of the fixing seat (2), a first screw thread head (4) and a first screw thread groove (5) are arranged in a screw thread fit manner, a buffer rod (6) is fixedly connected to the top of the first support rod (3), a second support rod (7) is arranged above the first support rod (3), a buffer groove (8) is arranged in the second support rod (7), the buffer block (9) is slidably connected in the buffer groove (8) in a nested manner, a buffer spring (10) is connected between the inner wall of the buffer groove (8) and the outer surface of the buffer block (9), the top end of the buffer rod (6) is fixedly connected with the bottom end of the buffer block (9), the top of the second support rod (7) is rotatably connected with an operation block (11), a support seat (12) is arranged above the second support rod (7), a second screw thread head (13) is fixedly connected to the top of the operation block (11), and a second screw thread groove (14) is arranged between the screw thread groove (14), the top of supporting seat (12) is provided with unmanned aerial vehicle frame (15), and the top fixedly connected with butt joint piece (16) of supporting seat (12), butt joint piece (16) and supporting seat (12) meet the position and be provided with inside groove (17), sliding connection has movable block (18) in inside groove (17), fixedly connected with connecting rod (19) are gone up in movable block (18), and are connected with positioning spring (22) between the surface of movable block (18) and inside groove (17) inner wall, fixedly connected with anticreep piece (23) are gone up in movable block (18), the bottom of unmanned aerial vehicle frame (15) is provided with butt joint groove (24), butt joint groove (24) inner wall is provided with anticreep groove (25).
2. An unmanned aerial vehicle floor stand according to claim 1, wherein: base (1) and supporting seat (12) all are provided with two and correspond the bottom both sides position of position unmanned aerial vehicle frame (15), every bracing piece (3), bracing piece two (7) between base (1) and supporting seat (12) all are provided with two.
3. An unmanned aerial vehicle floor stand according to claim 1, wherein: the base (1) is made of rubber.
4. An unmanned aerial vehicle floor stand according to claim 1, wherein: the supporting seat (12) is provided with a through groove (20) communicated with the inner groove (17), and the connecting rod (19) is connected with the through groove (20) in a nested sliding manner.
5. An unmanned aerial vehicle floor stand according to claim 1, wherein: one end of the connecting rod (19) is fixedly connected with an operating ring (21) at the position outside the supporting seat (12).
6. An unmanned aerial vehicle floor stand according to claim 1, wherein: the butt joint piece (16) and the butt joint groove (24) are arranged in a splicing matching mode, and the anti-falling block (23) and the anti-falling groove (25) are arranged in a splicing matching mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223553015.XU CN218751490U (en) | 2022-12-29 | 2022-12-29 | Unmanned aerial vehicle floor stand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223553015.XU CN218751490U (en) | 2022-12-29 | 2022-12-29 | Unmanned aerial vehicle floor stand |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218751490U true CN218751490U (en) | 2023-03-28 |
Family
ID=85687375
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223553015.XU Active CN218751490U (en) | 2022-12-29 | 2022-12-29 | Unmanned aerial vehicle floor stand |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218751490U (en) |
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2022
- 2022-12-29 CN CN202223553015.XU patent/CN218751490U/en active Active
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