CN220199621U - Landing gear for aerial unmanned aerial vehicle - Google Patents
Landing gear for aerial unmanned aerial vehicle Download PDFInfo
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- CN220199621U CN220199621U CN202320916856.8U CN202320916856U CN220199621U CN 220199621 U CN220199621 U CN 220199621U CN 202320916856 U CN202320916856 U CN 202320916856U CN 220199621 U CN220199621 U CN 220199621U
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- buffer
- aerial vehicle
- unmanned aerial
- fixedly connected
- supporting
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- 230000003139 buffering effect Effects 0.000 claims abstract description 6
- 238000009434 installation Methods 0.000 claims description 20
- 230000000694 effects Effects 0.000 abstract description 6
- 238000005259 measurement Methods 0.000 description 5
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses a landing frame for an aerial unmanned aerial vehicle, which comprises a supporting mechanism for supporting the aerial unmanned aerial vehicle, wherein the supporting mechanism comprises a supporting table, four corners at the bottom of the supporting table are fixedly connected with mounting lugs, and a U-shaped supporting leg is rotatably arranged between the two mounting lugs positioned on the same side; a buffer gear for unmanned aerial vehicle buffering protection takes photo by plane, buffer gear includes the buffer station, and the four corners department of buffer station bottom all is through slidable mounting subassembly and supporting bench sliding connection. The utility model discloses not only through the rotatable U type landing leg of design, conveniently when not using, fold and accomodate supporting mechanism to reduced the occupation in space, through setting up fixing bolt, can fix U type landing leg moreover, consequently guaranteed the stability when U type landing leg supports or accomodates; and through setting up buffer spring, can fall on the buffer station to unmanned aerial vehicle and play the cushioning effect to have played good protection to unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle landing gears, in particular to an aerial photography landing gear for an unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using a radio remote control device and an automatic program control device, and when aerial photographing measurement is carried out, aerial photographing measurement is carried out by using unmanned aerial vehicle carrying aerial photographing measurement equipment, and when the unmanned aerial vehicle is lifted, landing gear is required to be used for supporting.
The application number is as follows: CN202221100123.9 discloses an unmanned aerial vehicle undercarriage for aerial photography measurement, relates to aerial photography measurement technical field, including the mounting panel, the top surface of mounting panel is close to edge position department and is provided with the mounting hole, the bottom surface of mounting panel is fixed with the bottom block, the side rotation of bottom block is connected with the undercarriage body, the one end of undercarriage body is fixed with the drum, square groove has been seted up to the one end of drum, the bottom surface of mounting panel is close to edge position department fixed mounting and has vertical block, the side of vertical block runs through and is provided with the slide, the one end of slide is fixed with the square, the other end fixed mounting of slide has the handle. According to the utility model, the unmanned aerial vehicle can be stably supported through the landing gear body, and when the unmanned aerial vehicle needs to be stored, a worker can conveniently fold the landing gear body by only pulling the pull handle, so that the occupied space of the unmanned aerial vehicle is reduced, the transportation cost is reduced, the operation is simple and quick, and the practicability is higher.
Although the above comparative case solves the corresponding technical problems, the above comparative case has the following drawbacks:
above-mentioned technical scheme does not have special buffer structure to unmanned aerial vehicle, and is comparatively limited to unmanned aerial vehicle's protection when falling to the ground.
Disclosure of Invention
The landing gear for the aerial unmanned aerial vehicle is not only convenient to fold and store the supporting mechanism when not in use by designing the rotatable U-shaped supporting leg, so that space occupation is reduced, but also the U-shaped supporting leg can be fixed by arranging the fixing bolt, and therefore stability of the U-shaped supporting leg during supporting or storing is ensured; and through setting up buffer spring, can fall on the buffer station to unmanned aerial vehicle and play the cushioning effect to have played good protection to unmanned aerial vehicle.
In order to achieve the above purpose, the main technical scheme adopted by the utility model comprises the following steps:
an undercarriage for an aerial unmanned aerial vehicle, comprising:
the support mechanism comprises a support table, wherein four corners of the bottom of the support table are fixedly connected with mounting lugs, and a U-shaped supporting leg is rotatably arranged between the two mounting lugs positioned on the same side;
a buffer gear for unmanned aerial vehicle buffering protection takes photo by plane, buffer gear includes the buffer station, the four corners department of buffer station bottom all through slidable mounting subassembly with supporting bench sliding connection, buffer subassembly is still installed to the center department of buffer station bottom.
Above-mentioned undercarriage for unmanned aerial vehicle takes photo by plane, wherein, sliding mounting subassembly includes fixed connection the installation sliding sleeve on the brace table, sliding connection has the installation slide bar on the installation sliding sleeve, just the top of installation slide bar with the bottom fixed connection of brace table.
Above-mentioned undercarriage for unmanned aerial vehicle takes photo by plane, wherein, buffer assembly includes fixed connection be in the installation shell of brace table bottom, the bottom fixedly connected with symmetry of installation shell inner wall sets up two buffer springs, two buffer spring's top is through buffer block fixed connection, just the buffer block with the inner wall sliding connection of installation shell, the top fixedly connected with buffer rod of buffer block, just the top of buffer rod with the bottom fixed connection of brace table.
Above-mentioned undercarriage for unmanned aerial vehicle takes photo by plane, wherein, the bottom fixedly connected with supporting pad of U type landing leg.
Above-mentioned undercarriage for unmanned aerial vehicle takes photo by plane, wherein, the top fixedly connected with blotter of buffering platform.
Above-mentioned undercarriage for unmanned aerial vehicle takes photo by plane, wherein, the bottom of installation ear just corresponds the fixing bolt is installed to the position screw thread of U type landing leg.
Above-mentioned undercarriage for unmanned aerial vehicle takes photo by plane, wherein, the notch department of installation shell just corresponds the position fixedly connected with stopper of buffer block.
The utility model has at least the following beneficial effects:
according to the landing gear for the aerial unmanned aerial vehicle, the rotatable U-shaped supporting legs are designed, so that the supporting mechanism is convenient to fold and store when not in use, space occupation is reduced, and the U-shaped supporting legs can be fixed by arranging the fixing bolts, so that the stability of the U-shaped supporting legs during supporting or storing is ensured; and through setting up buffer spring, can fall on the buffer station to unmanned aerial vehicle and play the cushioning effect to have played good protection to unmanned aerial vehicle.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiments of the application and together with the description serve to explain the application and do not constitute an undue limitation to the application. In the drawings:
FIG. 1 is a schematic structural view of a landing gear for an aerial unmanned aerial vehicle of the present utility model;
FIG. 2 is a schematic cross-sectional view of the landing gear for an aerial unmanned aerial vehicle according to the present utility model;
FIG. 3 is a schematic view of the structure of a slide mount assembly in landing gear for an aerial unmanned aerial vehicle of the present utility model;
FIG. 4 is a schematic view of the structure of a buffer assembly in landing gear for an aerial unmanned aerial vehicle according to the present utility model;
fig. 5 is a schematic view of a partial enlarged structure at a in fig. 2 according to the present utility model.
Reference numerals illustrate:
1. a support mechanism; 2. a buffer mechanism;
101. a support table; 102. a mounting ear; 103. u-shaped supporting legs; 104. a fixing bolt; 1031. a support pad;
201. a buffer stage; 2011. a cushion pad; 202. a slide mounting assembly; 203. a buffer assembly;
2021. installing a sliding sleeve; 2022. installing a sliding rod;
2031. a mounting shell; 2032. a buffer spring; 2033. a buffer block; 2034. a buffer rod; 2035. and a limiting block.
Detailed Description
The embodiments of the present application will be described in detail below with reference to the accompanying drawings and examples, so that the implementation process of how the technical means are applied to solve the technical problems and achieve the technical effects of the present application can be fully understood and implemented accordingly.
Referring to fig. 1 to 5, an landing gear for an aerial unmanned aerial vehicle according to an embodiment of the present utility model includes: the support mechanism 1 is used for supporting the aerial unmanned aerial vehicle and the buffer mechanism 2 is used for buffering and protecting the aerial unmanned aerial vehicle;
the supporting mechanism 1 comprises a supporting table 101, wherein four corners of the bottom of the supporting table 101 are fixedly connected with mounting lugs 102, and a U-shaped supporting leg 103 is rotatably arranged between the two mounting lugs 102 positioned on the same side;
the buffer mechanism 2 comprises a buffer table 201, four corners of the bottom of the buffer table 201 are slidably connected with the supporting table 101 through sliding mounting assemblies 202, and a buffer assembly 203 is further mounted at the center of the bottom of the buffer table 201;
the sliding installation assembly 202 comprises an installation sliding sleeve 2021 fixedly connected to the supporting table 101, an installation sliding rod 2022 is connected to the installation sliding sleeve 2021 in a sliding manner, and the top of the installation sliding rod 2022 is fixedly connected with the bottom of the supporting table 101;
the buffer assembly 203 comprises a mounting shell 2031 fixedly connected to the bottom of the supporting table 101, two symmetrically arranged buffer springs 2032 are fixedly connected to the bottom of the inner wall of the mounting shell 2031, the tops of the two buffer springs 2032 are fixedly connected through a buffer block 2033, the buffer block 2033 is slidably connected with the inner wall of the mounting shell 2031, a buffer rod 2034 is fixedly connected to the top of the buffer block 2033, and the top of the buffer rod 2034 is fixedly connected with the bottom of the supporting table 101;
through adopting above-mentioned technical scheme, not only through the rotatable U type landing leg 103 of design, conveniently when not using, fold and accomodate supporting mechanism 1 to reduced the occupation in space, through setting up fixing bolt 104, can fix U type landing leg 103 moreover, consequently guaranteed the stability when U type landing leg 103 supports or accomodates; and through setting up buffer spring 2032, can play the cushioning effect to unmanned aerial vehicle falls on buffer station 201 to play good protection to unmanned aerial vehicle.
Wherein, the bottom of the U-shaped supporting leg 103 is fixedly connected with a supporting pad 1031;
by adopting the technical scheme, the U-shaped supporting leg 103 is additionally supported and stabilized on the ground.
Wherein, the top of the buffer table 201 is fixedly connected with a buffer pad 2011;
through adopting above-mentioned technical scheme, increased unmanned aerial vehicle's buffering protection.
Wherein, the bottom of the mounting lug 102 is provided with a fixing bolt 104 corresponding to the position of the U-shaped supporting leg 103 in a threaded manner;
through adopting above-mentioned technical scheme, conveniently fix U type landing leg 103 to stability when having improved U type landing leg 103 and supporting or accomodating.
Wherein, a limiting block 2035 is fixedly connected at the notch of the mounting shell 2031 and at the position corresponding to the buffer block 2033;
by adopting the above technical scheme, the buffer block 2033 is limited, and the buffer block 2033 is prevented from being separated from the installation shell 2031 in the sliding process.
The working principle of the utility model is as follows: not only is the rotatable U-shaped supporting leg 103 designed to facilitate folding and storage of the supporting mechanism 1 when not in use, so that space occupation is reduced, but also the U-shaped supporting leg 103 can be fixed by arranging the fixing bolt 104, and therefore stability of the U-shaped supporting leg 103 during supporting or storage is ensured; and through setting up buffer spring 2032, can play the cushioning effect to unmanned aerial vehicle falls on buffer station 201 to play good protection to unmanned aerial vehicle.
While the foregoing description illustrates and describes the preferred embodiments of the present utility model, it is to be understood that the utility model is not limited to the forms disclosed herein, but is not to be construed as limited to other embodiments, and is capable of numerous other combinations, modifications and environments and is capable of changes or modifications within the scope of the inventive concept as described herein, either as a result of the foregoing teachings or as a result of the knowledge or technology in the relevant art. And that modifications and variations which do not depart from the spirit and scope of the utility model are intended to be within the scope of the appended claims.
Claims (7)
1. Landing gear for unmanned aerial vehicle takes photo by plane, characterized by comprising:
the support mechanism (1) is used for supporting the aerial unmanned aerial vehicle, the support mechanism (1) comprises a support table (101), mounting lugs (102) are fixedly connected to four corners of the bottom of the support table (101), and U-shaped supporting legs (103) are rotatably arranged between the two mounting lugs (102) located on the same side;
a buffer gear (2) for unmanned aerial vehicle buffering protection takes photo by plane, buffer gear (2) include buffer station (201), the four corners department of buffer station (201) bottom all through slidable mounting subassembly (202) with supporting bench (101) sliding connection, buffer subassembly (203) are still installed to the center department of buffer station (201) bottom.
2. Landing gear for an aerial unmanned aerial vehicle according to claim 1, wherein: the sliding installation assembly (202) comprises an installation sliding sleeve (2021) fixedly connected to the supporting table (101), an installation sliding rod (2022) is connected to the installation sliding sleeve (2021) in a sliding mode, and the top of the installation sliding rod (2022) is fixedly connected with the bottom of the supporting table (101).
3. Landing gear for an aerial unmanned aerial vehicle according to claim 2, wherein: the buffer component (203) comprises a mounting shell (2031) fixedly connected to the bottom of the supporting table (101), two buffer springs (2032) symmetrically arranged are fixedly connected to the bottom of the inner wall of the mounting shell (2031), the tops of the two buffer springs (2032) are fixedly connected through a buffer block (2033), the buffer block (2033) is in sliding connection with the inner wall of the mounting shell (2031), a buffer rod (2034) is fixedly connected to the top of the buffer block (2033), and the top of the buffer rod (2034) is fixedly connected with the bottom of the supporting table (101).
4. A landing gear for an aerial unmanned aerial vehicle according to claim 3, wherein: the bottom of U type landing leg (103) is fixedly connected with supporting pad (1031).
5. The landing gear for an aerial unmanned aerial vehicle of claim 4, wherein: the top of the buffer table (201) is fixedly connected with a buffer pad (2011).
6. The landing gear for an aerial unmanned aerial vehicle of claim 5, wherein: and a fixing bolt (104) is arranged at the bottom of the mounting lug (102) and corresponds to the position of the U-shaped supporting leg (103) in a threaded manner.
7. The landing gear for an aerial unmanned aerial vehicle of claim 6, wherein: and a limiting block (2035) is fixedly connected at the notch of the mounting shell (2031) and at the position corresponding to the buffer block (2033).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320916856.8U CN220199621U (en) | 2023-04-22 | 2023-04-22 | Landing gear for aerial unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320916856.8U CN220199621U (en) | 2023-04-22 | 2023-04-22 | Landing gear for aerial unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220199621U true CN220199621U (en) | 2023-12-19 |
Family
ID=89143265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320916856.8U Active CN220199621U (en) | 2023-04-22 | 2023-04-22 | Landing gear for aerial unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220199621U (en) |
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2023
- 2023-04-22 CN CN202320916856.8U patent/CN220199621U/en active Active
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