CN222202941U - Unmanned aerial vehicle with bradyseism support - Google Patents
Unmanned aerial vehicle with bradyseism support Download PDFInfo
- Publication number
- CN222202941U CN222202941U CN202420488246.7U CN202420488246U CN222202941U CN 222202941 U CN222202941 U CN 222202941U CN 202420488246 U CN202420488246 U CN 202420488246U CN 222202941 U CN222202941 U CN 222202941U
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- bradyseism
- aerial vehicle
- unmanned aerial
- support
- 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.)
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Links
- 230000035939 shock Effects 0.000 claims abstract description 17
- 239000003381 stabilizer Substances 0.000 claims abstract description 15
- 239000006096 absorbing agent Substances 0.000 claims description 3
- 238000010521 absorption reaction Methods 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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- Vibration Dampers (AREA)
Abstract
The utility model provides an unmanned aerial vehicle with bradyseism support, includes unmanned aerial vehicle main part, bradyseism support, connecting rod and connecting rod bradyseism cover, and unmanned aerial vehicle main part downside is equipped with respectively through the last mesa of bolt fixed connection bradyseism support, goes up the mesa both sides and is equipped with the stabilizer blade that has elasticity, and the stabilizer blade lower extreme that has elasticity is equipped with fore-and-aft connecting rod, and connecting rod bradyseism cover is established to the cover in the connecting rod outside, is equipped with the elastic connection face between two connecting rod bradyseism covers. The unmanned aerial vehicle has the advantages that the elastic support legs and the connecting rod cushioning sleeves are used for double-layer shock absorption, so that the impact on the interior of the unmanned aerial vehicle during landing is avoided, the connecting rod cushioning sleeves are convenient to detach and replace, the elastic connection surfaces can further support the unmanned aerial vehicle main body, and a certain support leg folding effect is achieved.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle with a cushioning bracket.
Background
The unmanned plane is a unmanned plane which is controlled by using radio remote control equipment and a self-provided program control device, or is operated completely or intermittently and autonomously by a vehicle-mounted computer, and an unmanned plane landing gear is an important device in the taking-off and landing process of the plane in the taking-off and landing process of the unmanned plane, has strict technical requirements on the weight, the buffering capacity, the installation mode and the reliability of the unmanned plane, otherwise, the whole taking-off and landing process is adversely affected, and even the damage problem inside the unmanned plane is caused.
Disclosure of utility model
The utility model aims to solve the defects in the prior art, and provides an unmanned aerial vehicle with a cushioning bracket.
In order to achieve the aim, the unmanned aerial vehicle with the shock absorbing support comprises an unmanned aerial vehicle main body, the shock absorbing support, a connecting rod and a connecting rod shock absorbing sleeve, wherein the lower side of the unmanned aerial vehicle main body is fixedly connected with an upper table top of the shock absorbing support through bolts, elastic support legs are respectively arranged on two sides of the upper table top, a longitudinal connecting rod is arranged at the lower end of each elastic support leg, the connecting rod shock absorbing sleeve is sleeved on the outer side of each connecting rod, and an elastic connecting surface is arranged between the two connecting rod shock absorbing sleeves.
Further, the two elastic support legs are symmetrically arranged.
Further, the two elastic supporting legs are elastic sheets.
Further, the connecting rod cushioning sleeve is a cushioning block with two ends fixedly connected with the connecting rod.
Further, the longitudinal length of the connecting rod exceeds the length of the lower end of the elastic support leg.
Further, the two elastic support legs are inclined outwards and form an isosceles trapezoid with the upper table top.
Further, the joint of the connecting rod cushioning sleeve corresponds to the joint of the connecting rod and the lower end of the elastic support leg.
The unmanned aerial vehicle has the beneficial effects that the double-layer shock absorption is realized through the elastic support legs and the connecting rod shock absorption sleeve, so that the impact on the interior of the unmanned aerial vehicle during landing is avoided, the connecting rod shock absorption sleeve is convenient to detach and replace, and the elastic connection surface can further support the unmanned aerial vehicle main body and has a certain support leg folding effect.
Drawings
Fig. 1 is a schematic diagram of the structure of the device.
Fig. 2 is a schematic diagram of the structure of the device.
FIG. 3 is an expanded view of the connecting rod cushioning sleeve.
Detailed Description
The technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to fig. 1 to 3 of the embodiments of the present utility model, and it is obvious that the described embodiments are only some embodiments of the present utility model, but not all embodiments.
Embodiment 1 is with reference to fig. 1-3, an unmanned aerial vehicle with bradyseism support, including unmanned aerial vehicle main part 1, bradyseism support, connecting rod 2 and connecting rod bradyseism cover 3, the unmanned aerial vehicle main part downside passes through the last mesa 4 of bolt fixed connection bradyseism support, goes up mesa both sides and is equipped with respectively and has elastic stabilizer blade 5, and the stabilizer blade lower extreme that has elasticity is equipped with fore-and-aft connecting rod, and connecting rod bradyseism cover is established to the cover in the connecting rod outside, is equipped with elastic connection face 6 between two connecting rod bradyseism covers.
Unmanned aerial vehicle with bradyseism support, two stabilizer blades that have elasticity are symmetrical setting.
Unmanned aerial vehicle with bradyseism support, two stabilizer blades that have elasticity are the elastic sheet.
Unmanned aerial vehicle with bradyseism support, but connecting rod bradyseism cover is the bradyseism piece of both ends fixed connection parcel connecting rod.
An unmanned aerial vehicle with a shock absorption support, wherein the longitudinal length of a connecting rod exceeds the length of the lower end of a supporting leg with elasticity. The elastic support leg is copper.
An unmanned aerial vehicle with cushioning support, two stabilizer blades that have elasticity are inclined outwards and go up mesa isosceles trapezoid for the inclined plane.
Unmanned aerial vehicle with shock absorber support, the junction that corresponds the connecting rod in the seam crossing of connecting rod shock absorber cover and has elastic stabilizer blade lower extreme.
Unmanned aerial vehicle with bradyseism support, through having the double-deck shock attenuation of elastic stabilizer blade and connecting rod bradyseism cover, to the inside impact of unmanned aerial vehicle when avoiding taking off and landing, and conveniently dismantle and change connecting rod bradyseism cover.
Unmanned aerial vehicle with bradyseism support, elastic connection face can further support unmanned aerial vehicle main part, has certain stabilizer blade and draws in the effect.
Unmanned aerial vehicle with bradyseism support, bradyseism piece are slice rubber, and the seam crossing is current connection structure 7. One of the two connecting structures is arranged at one end of the front surface, and the other connecting structure is arranged at the other end of the back surface.
The present utility model is not limited to the above-mentioned embodiments, and any person skilled in the art, based on the technical solution of the present utility model and the inventive concept thereof, can be replaced or changed within the scope of the present utility model.
Claims (3)
1. The utility model provides an unmanned aerial vehicle with bradyseism support, including unmanned aerial vehicle main part, bradyseism support, connecting rod and connecting rod bradyseism cover, wherein unmanned aerial vehicle main part downside passes through the last mesa of bolt fixed connection bradyseism support, go up mesa both sides and be equipped with respectively and have elastic stabilizer blade, it is equipped with fore-and-aft connecting rod to have elastic stabilizer blade lower extreme, connecting rod outside cover is established connecting rod bradyseism cover, two have elastic stabilizer blade be the symmetry setting, two have elastic stabilizer blade be the elastic piece, be equipped with the elastic connection face between two connecting rod bradyseism covers, two have elastic stabilizer blade be inclined outwards slope and last mesa isosceles trapezoid, but the bradyseism piece of connecting rod bradyseism cover for both ends fixed connection parcel connecting rod, the bradyseism piece is sheet rubber, the seam is current connection structure, two connection structures one sets up in positive one, another sets up the opposite side other.
2. The unmanned aerial vehicle with a shock absorber support of claim 1, wherein the longitudinal length of the connecting rod exceeds the length of the lower ends of the elastic support legs.
3. The unmanned aerial vehicle with the shock absorbing support according to claim 2, wherein the joint of the connecting rod shock absorbing sleeve corresponds to the joint of the connecting rod and the lower end of the elastic supporting leg.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202420488246.7U CN222202941U (en) | 2024-03-13 | 2024-03-13 | Unmanned aerial vehicle with bradyseism support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202420488246.7U CN222202941U (en) | 2024-03-13 | 2024-03-13 | Unmanned aerial vehicle with bradyseism support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN222202941U true CN222202941U (en) | 2024-12-20 |
Family
ID=93860800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202420488246.7U Active CN222202941U (en) | 2024-03-13 | 2024-03-13 | Unmanned aerial vehicle with bradyseism support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN222202941U (en) |
-
2024
- 2024-03-13 CN CN202420488246.7U patent/CN222202941U/en active Active
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