CN210364364U - Unmanned aerial vehicle take-off and landing buffering support device - Google Patents
Unmanned aerial vehicle take-off and landing buffering support device Download PDFInfo
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- CN210364364U CN210364364U CN201921025871.3U CN201921025871U CN210364364U CN 210364364 U CN210364364 U CN 210364364U CN 201921025871 U CN201921025871 U CN 201921025871U CN 210364364 U CN210364364 U CN 210364364U
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- support frame
- aerial vehicle
- unmanned aerial
- supporting seat
- support
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Abstract
The utility model relates to a take-off and landing buffer device, in particular to an unmanned aerial vehicle take-off and landing buffer bracket device with reasonable structure, simple and convenient assembly and reliable operation, it is characterized in that the support frame is connected with a buffer which consists of a connecting sleeve, a supporting seat and a spring, the upper end of the connecting sleeve is provided with an arc-shaped clamp for clamping the supporting frame, both ends of the arc-shaped clamp are provided with screw holes, and is fixedly connected with the supporting frame through the screw, the upper portion of the connecting sleeve is provided with a fixing hole for hooking the top end of the spring, the supporting seat is provided with a cylindrical hollow seat body with an upper end opening, the outer diameter of the hollow seat body of the supporting seat is smaller than the inner diameter of the connecting sleeve, the lower portion of the supporting seat is provided with a fixing hole for hooking the lower end of the spring, the spring is arranged in the connecting sleeve and the hollow seat body, and the hollow seat body is sleeved at the lower end of the connecting sleeve.
Description
The technical field is as follows:
the utility model relates to a take-off and landing buffer device, specific unmanned aerial vehicle take-off and landing buffer bracket device that has reasonable structure, simple and convenient assembly and reliable operation that says so.
Background art:
an unmanned aerial vehicle is flight equipment operated by utilizing a radio remote control device and a self-contained program control device, generally carries airborne camera shooting equipment, and is widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-shooting, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting and the like at present.
Unmanned aerial vehicle equipment takes off and land through radio remote control operation by the user, and the in-process of taking off and land inevitable bumps with ground, if misoperation, aggravate the collision dynamics easily, and then lead to airborne equipment to damage, in order to alleviate the impact of taking off and land, the above-mentioned problem is solved through laying flexible platform of taking off and land to some vendors, however this kind of method can't adapt to adverse circumstances and use, and carries inconveniently.
The invention content is as follows:
the utility model discloses shortcoming and not enough to exist among the prior art has provided an unmanned aerial vehicle take off and land buffering support device rational in infrastructure, easy and simple to handle, reliable operation.
The utility model discloses can reach through following measure:
the utility model provides an unmanned aerial vehicle buffering support device that takes off and land, is equipped with the support frame, and the connection buffering is equipped with the buffer on its characterized in that support frame, the buffer comprises adapter sleeve, supporting seat, spring, the upper end of adapter sleeve is equipped with the arc anchor clamps that are used for the joint support frame, and the screw hole is seted up at arc anchor clamps both ends to through screw and support frame fixed connection, adapter sleeve upper portion is equipped with the fixed orifices that is used for hook spring top, and the supporting seat has the cylindrical cavity pedestal of upper end open-ended, and the cavity pedestal external diameter of supporting seat is less than the internal diameter of adapter sleeve, and the supporting seat lower part is equipped with the fixed orifices that is used for hook spring lower extreme.
Arc anchor clamps on adapter sleeve upper portion are for being greater than the circular-arc of half circumference for press from both sides tight support frame, and with support frame fixed connection.
The bottom of cavity pedestal is the round platform form of invering, and further, the bottom surface of cavity base can be equipped with silica gel rubber blotter.
The support frame is cross support frame or I shape support frame or a style of calligraphy support frame, is equipped with two at least buffers on every branch of support frame.
The branch of support frame can adopt prismatic branch, is triangle-shaped or square branch like the cross-section, and corresponding sets up the recess corresponding with branch at adapter sleeve upper portion arc anchor clamps inner wall, and the adapter sleeve can effectively avoid the adapter sleeve to rotate around branch under the effect of the impact force when anchor clamps are fixed on branch this moment, and then avoids whole buffer to become invalid.
The utility model discloses when using, the support frame is installed in unmanned aerial vehicle's bottom, through set up the buffer more than two on the branch of support frame, effectively alleviates the influence of unmanned aerial vehicle take-off and land in-process impact force to equipment, has rational in infrastructure, assembles portably, uses advantages that are showing such as reliable.
Description of the drawings:
fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural diagram of the connecting sleeve of the present invention.
Fig. 3 is a schematic structural diagram of the middle support seat of the present invention.
Reference numerals: support frame 1, buffer 2, adapter sleeve 3, supporting seat 4, fixed orifices 5, arc anchor clamps 6.
The specific implementation mode is as follows:
the present invention will be further described with reference to the accompanying drawings.
As shown in the accompanying drawing 1, the utility model provides an unmanned aerial vehicle buffering support device that takes off and land is equipped with support frame 1, and the connection buffering is equipped with buffer 2 on its characterized in that support frame 1, buffer 2 comprises adapter sleeve 3, supporting seat 4, spring, the upper end of adapter sleeve 3 is equipped with arc anchor clamps 6 that are used for the joint support frame, and the screw hole is seted up at 6 both ends of arc anchor clamps to through screw and 1 fixed connection of support frame, 3 upper portions of adapter sleeve are equipped with the fixed orifices 5 that are used for hook spring top, and supporting seat 4 has the cylindrical cavity pedestal of upper end open-ended, and the cavity pedestal external diameter of supporting seat 4 is less than adapter sleeve 3's internal diameter, and 4 lower parts of supporting seat are equipped with the fixed orifices 5 that are used for hook spring lower extreme, and the spring setting cup joints at.
Arc anchor clamps 6 on 3 upper portions of adapter sleeve are for being greater than the circular-arc of half circumference for press from both sides tight support frame 1, and with 1 fixed connection of support frame.
The bottom of cavity pedestal is the round platform form of invering, and further, the bottom surface of cavity base can be equipped with silica gel rubber blotter.
The support frame is cross support frame or I shape support frame or a style of calligraphy support frame, is equipped with two at least buffers on every branch of support frame.
The utility model discloses when using, the support frame is installed in unmanned aerial vehicle's bottom, through set up the buffer more than two on the branch of support frame, effectively alleviates the influence of unmanned aerial vehicle take-off and land in-process impact force to equipment, has rational in infrastructure, assembles portably, uses advantages that are showing such as reliable.
Claims (6)
1. The utility model provides an unmanned aerial vehicle buffering support device that takes off and land, is equipped with the support frame, and the connection buffering is equipped with the buffer on its characterized in that support frame, the buffer comprises adapter sleeve, supporting seat, spring, the upper end of adapter sleeve is equipped with the arc anchor clamps that are used for the joint support frame, and the screw hole is seted up at arc anchor clamps both ends to through screw and support frame fixed connection, adapter sleeve upper portion is equipped with the fixed orifices that is used for hook spring top, and the supporting seat has the cylindrical cavity pedestal of upper end open-ended, and the cavity pedestal external diameter of supporting seat is less than the internal diameter of adapter sleeve, and the supporting seat lower part is equipped with the fixed orifices that is used for hook spring lower extreme.
2. The take-off and landing buffering support device for the unmanned aerial vehicle as claimed in claim 1, wherein the arc-shaped clamp at the upper part of the connecting sleeve is arc-shaped with a circumference larger than half of a circumference.
3. The take-off and landing buffering support device for the unmanned aerial vehicle as claimed in claim 1, wherein the bottom of the hollow base body is in the shape of an inverted circular truncated cone.
4. The take-off and landing buffering support device for the unmanned aerial vehicle as claimed in claim 3, wherein a silica gel/rubber cushion pad is disposed on the bottom surface of the hollow base.
5. The take-off and landing buffering support device for the unmanned aerial vehicle as claimed in claim 1, wherein the support frame is a cross-shaped support frame, an I-shaped support frame or a square support frame, and each support rod of the support frame is provided with at least two buffers.
6. The take-off and landing buffering support device for the unmanned aerial vehicle as claimed in claim 1, wherein the support rods of the support frame are prismatic support rods, the cross sections of the prismatic support rods are triangular or square support rods, and grooves corresponding to the support rods are correspondingly formed in the inner walls of the arc-shaped clamps on the upper portions of the connection sleeves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921025871.3U CN210364364U (en) | 2019-07-03 | 2019-07-03 | Unmanned aerial vehicle take-off and landing buffering support device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921025871.3U CN210364364U (en) | 2019-07-03 | 2019-07-03 | Unmanned aerial vehicle take-off and landing buffering support device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210364364U true CN210364364U (en) | 2020-04-21 |
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ID=70269041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921025871.3U Active CN210364364U (en) | 2019-07-03 | 2019-07-03 | Unmanned aerial vehicle take-off and landing buffering support device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210364364U (en) |
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2019
- 2019-07-03 CN CN201921025871.3U patent/CN210364364U/en active Active
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