CN214524380U - Buffering formula unmanned aerial vehicle equipment that rises and falls - Google Patents
Buffering formula unmanned aerial vehicle equipment that rises and falls Download PDFInfo
- Publication number
- CN214524380U CN214524380U CN202023188345.4U CN202023188345U CN214524380U CN 214524380 U CN214524380 U CN 214524380U CN 202023188345 U CN202023188345 U CN 202023188345U CN 214524380 U CN214524380 U CN 214524380U
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- CN
- China
- Prior art keywords
- gomphosis
- mounting bracket
- pole
- unmanned aerial
- aerial vehicle
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- 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
Links
- 230000003139 buffering effect Effects 0.000 title claims abstract description 13
- 238000013016 damping Methods 0.000 claims abstract description 10
- 238000003466 welding Methods 0.000 claims abstract description 3
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 230000000630 rising effect Effects 0.000 abstract description 2
- 238000013461 design Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model provides a buffering formula unmanned aerial vehicle equipment of rising and falling, including supporting mounting bracket, mounting platform and horizontal diaphragm, the mounting platform is equipped with the connecting bolt of being connected with the unmanned aerial vehicle bottom, support the mounting bracket with the mounting platform welding, horizontal diaphragm both ends are equipped with integrated into one piece's buffer tube respectively, horizontal diaphragm top is equipped with T font gomphosis pole, buffer tube's top is equipped with the abrasive rubber piece, the top of T font gomphosis pole with support the bottom gomphosis of mounting bracket, T font gomphosis pole through connecting the screw pole with it is fixed to support the mounting bracket, the abrasive rubber piece with support the bottom gomphosis of mounting bracket, be equipped with damping spring in the inside sliding chamber of buffer tube, the sliding chamber is equipped with the inserted bar rather than pegging graft, the inserted bar both sides are equipped with the limiting plate respectively. The first section of the damping spring is provided with an embedded block, the embedded block is embedded into the concave part at the top end of the inserted bar, and the bottom end of the inserted bar is provided with a connecting column.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment technical field, concretely relates to buffering formula unmanned aerial vehicle equipment that rises and falls.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, 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; the method is currently 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, movie and television shooting, romantic manufacturing and the like.
In prior art, civilian unmanned aerial vehicle usage is more, and unmanned aerial vehicle all needs good buffering when descending, otherwise can cause the damage or even the damage to the organism, but general unmanned aerial vehicle buffer structure all is fixed and inconvenient dismantlement, and buffering effect is general, and the effect is not good when unmanned aerial vehicle lands firmly.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims to provide a buffer type unmanned aerial vehicle lifting device, which solves the problems in the prior art;
in order to solve the technical problem, the utility model provides a following technical scheme:
the utility model provides a buffering formula unmanned aerial vehicle equipment of rising and falling, is including supporting mounting bracket, mounting platform and horizontal diaphragm, and mounting platform is equipped with the connecting bolt of being connected with the unmanned aerial vehicle bottom, support the mounting bracket with the mounting platform welding, horizontal diaphragm both ends are equipped with integrated into one piece's buffer tube respectively, horizontal diaphragm top is equipped with T font gomphosis pole, buffer tube's top is equipped with the abrasive rubber piece, the top of T font gomphosis pole with support the bottom gomphosis of mounting bracket, T font gomphosis pole through connect the screw pole with it is fixed to support the mounting bracket, the abrasive rubber piece with support the bottom gomphosis of mounting bracket, be equipped with damping spring in the inside smooth chamber of buffer tube, smooth chamber is equipped with the inserted bar rather than pegging graft, the inserted bar both sides are equipped with the limiting plate respectively. The bottom end of the damping spring is provided with an embedded block, the embedded block is embedded into the concave part at the top end of the inserted link, the bottom end of the inserted link is provided with a connecting column, and the bottom end of the connecting column is provided with a supporting caster.
To the utility model discloses further description, support the mounting bracket with still be equipped with the stiffener between the mounting platform.
It is right to the utility model discloses further description, it is equipped with T font gomphosis mouth to support the mounting bracket, T font gomphosis pole with T font gomphosis mouth gomphosis, connection screw pole bottom is screw thread portion, support the mounting bracket be equipped with the screw thread perforation of T font gomphosis mouth intercommunication, screw thread portion passes the screw thread perforation and rather than threaded connection, the inside thread groove that is equipped with in top of T font gomphosis mouth, screw thread portion with thread groove threaded connection.
Right the utility model discloses further description, the support mounting bracket still be equipped with the gomphosis mouth that the wear-resisting rubber piece corresponds.
Compared with the prior art, the utility model has the advantages of:
the defects that the traditional buffering equipment is inconvenient to disassemble and has a general buffering effect are overcome; the detachable connection design is adopted, so that the installation and the subsequent disassembly are convenient, and the replacement and the maintenance are facilitated; adopt built-in buffering design, can fully cushion, improve unmanned aerial vehicle's shock-absorbing capacity.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the connection between the inserted link and the buffer sleeve of the present invention;
fig. 3 is a schematic view of the internal connection of the T-shaped embedded rod supporting and mounting frame of the present invention.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Example 1, as shown in figures 1-3:
a buffer type unmanned aerial vehicle lifting device comprises a supporting and mounting frame 4, a mounting platform 1 and a horizontal transverse plate 11, wherein the mounting platform 1 is provided with a connecting bolt 2 connected with the bottom end of an unmanned aerial vehicle, the supporting and mounting frame 4 is welded with the mounting platform 1, two ends of the horizontal transverse plate 11 are respectively provided with an integrally formed buffer sleeve 8, the top end of the horizontal transverse plate 11 is provided with a T-shaped embedded rod 6, the top end of the buffer sleeve 8 is provided with a wear-resistant rubber block 7, the top end of the T-shaped embedded rod 6 is embedded with the bottom end of the supporting and mounting frame 4, the T-shaped embedded rod 6 is fixed with the supporting and mounting frame 4 through a connecting screw rod 5, the wear-resistant rubber block 7 is embedded with the bottom end of the supporting and mounting frame 4, a damping spring 12 is arranged in a sliding cavity 801 inside the buffer sleeve 8, the sliding cavity 801 is provided with an inserted rod 14 inserted with the sliding cavity 801, two sides of the inserted rod 14 are respectively provided with a limiting plate 15, and the bottom end of the damping spring 12 is provided with an embedded block 13, the embedded block 13 is embedded into the inner recess at the top end of the inserted rod 14, the bottom end of the inserted rod 14 is provided with a connecting column 9, and the bottom end of the connecting column 9 is provided with a supporting caster 10. In order to enhance the overall strength, a reinforcing rod 3 is arranged between the support mounting frame 4 and the mounting platform 1. In order to facilitate the installation and dismantle, support mounting bracket 4 and be equipped with T font gomphosis mouth 402, T font gomphosis pole 6 and the gomphosis of T font gomphosis mouth 402, 5 bottoms of connection screw pole are screw thread portion 501, support mounting bracket 4 is equipped with the screw thread perforation 401 with T font gomphosis mouth 402 intercommunication, screw thread portion 501 passes screw thread perforation 401 and rather than threaded connection, the inside thread groove 601 that is equipped with in top of T font gomphosis mouth 402, screw thread portion 501 and thread groove 601 threaded connection, support mounting bracket 4 still is equipped with the gomphosis mouth that corresponds with abrasion-resistant rubber piece 7.
In the embodiment, the unmanned aerial vehicle is installed and connected with the unmanned aerial vehicle through the connecting bolt 2;
when the unmanned aerial vehicle is used, in the landing process of the unmanned aerial vehicle, the caster 10 contacts the ground, the connecting column 9 drives the inserted rod 14 to move along the sliding cavity 801 in the buffering sleeve 8, and the damping spring 12 exists in the sliding cavity 801, so that effective buffering and damping can be performed;
when the unmanned aerial vehicle needs to be disassembled for maintenance or replaced, the connecting bolt 2 can be disassembled to be separated from the unmanned aerial vehicle; the connection screw 5 can be screwed so that the screw portion 5 at the bottom end thereof is separated from the screw hole 401 and the screw groove 601, and at this time, the restriction of the T-shaped fitting rod 6 and the support mounting bracket 4 is released, and the T-shaped fitting rod 6 can be pulled out and separated from the T-shaped fitting opening 402.
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. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified 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 by those skilled in the art.
Claims (4)
1. The utility model provides a buffering formula unmanned aerial vehicle equipment that rises and falls, includes support mounting bracket (4), mounting platform (1) and horizontal diaphragm (11), and mounting platform (1) is equipped with connecting bolt (2) of being connected with the unmanned aerial vehicle bottom, and characterized in that, support mounting bracket (4) with mounting platform (1) welding, horizontal diaphragm (11) both ends are equipped with integrated into one piece's buffer sleeve (8) respectively, horizontal diaphragm (11) top is equipped with T font gomphosis pole (6), the top of buffer sleeve (8) is equipped with wear-resisting rubber piece (7), the top of T font gomphosis pole (6) with the bottom gomphosis of support mounting bracket (4), T font gomphosis pole (6) through connecting screw pole (5) with support mounting bracket (4) are fixed, wear-resisting rubber piece (7) with the bottom gomphosis of support mounting bracket (4), be equipped with damping spring (12) in smooth chamber (801) of buffer tube (8) inside, smooth chamber (801) is equipped with inserted bar (14) rather than pegging graft, inserted bar (14) both sides are equipped with limiting plate (15) respectively, damping spring's (12) bottom is equipped with gomphosis piece (13), gomphosis piece (13) embedding in the indent on inserted bar (14) top, the bottom of inserted bar (14) is equipped with spliced pole (9), the bottom of spliced pole (9) is equipped with supporting wheel foot (10).
2. A cushioned drone landing device according to claim 1, characterised in that a reinforcing bar (3) is also provided between the support mounting (4) and the mounting platform (1).
3. A cushioned unmanned aircraft landing gear according to claim 1, wherein the support mounting bracket (4) is provided with a T-shaped engagement opening (402), the T-shaped engagement rod (6) is engaged with the T-shaped engagement opening (402), the bottom end of the connection screw rod (5) is provided with a threaded portion (501), the support mounting bracket (4) is provided with a threaded hole (401) communicated with the T-shaped engagement opening (402), the threaded portion (501) passes through the threaded hole (401) and is in threaded connection with the threaded hole, a threaded groove (601) is provided inside the top end of the T-shaped engagement opening (402), and the threaded portion (501) is in threaded connection with the threaded groove (601).
4. A cushioned drone landing device according to claim 1, wherein the support mounting (4) is also provided with a fitting mouth corresponding to the wear-resistant rubber block (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023188345.4U CN214524380U (en) | 2020-12-26 | 2020-12-26 | Buffering formula unmanned aerial vehicle equipment that rises and falls |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023188345.4U CN214524380U (en) | 2020-12-26 | 2020-12-26 | Buffering formula unmanned aerial vehicle equipment that rises and falls |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214524380U true CN214524380U (en) | 2021-10-29 |
Family
ID=78296715
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023188345.4U Expired - Fee Related CN214524380U (en) | 2020-12-26 | 2020-12-26 | Buffering formula unmanned aerial vehicle equipment that rises and falls |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214524380U (en) |
-
2020
- 2020-12-26 CN CN202023188345.4U patent/CN214524380U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211029 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |