CN214690229U - Unmanned aerial vehicle load quick detach device - Google Patents
Unmanned aerial vehicle load quick detach device Download PDFInfo
- Publication number
- CN214690229U CN214690229U CN202023253513.3U CN202023253513U CN214690229U CN 214690229 U CN214690229 U CN 214690229U CN 202023253513 U CN202023253513 U CN 202023253513U CN 214690229 U CN214690229 U CN 214690229U
- Authority
- CN
- China
- Prior art keywords
- load
- pair
- aerial vehicle
- unmanned aerial
- bracket
- 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.)
- Active
Links
- 238000003780 insertion Methods 0.000 claims description 2
- 230000037431 insertion Effects 0.000 claims description 2
- 210000001503 joint Anatomy 0.000 abstract description 2
- 238000003032 molecular docking Methods 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model provides an unmanned aerial vehicle load quick release device, which comprises a load support, a guide rail support, a quick release host terminal, a quick release load terminal and a clamping assembly, wherein the unmanned aerial vehicle load is fixed at the bottom end of the load support; unmanned aerial vehicle load quick detach device in this scheme includes load support and rail brackets, docks between load support and the rail brackets through docking between quick detach host computer terminal and the quick detach load terminal, simultaneously between the two through the vice quick butt joint and the dismantlement of realizing between the two of sliding connection who forms to utilize the chucking subassembly to realize the locking function of the two.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle load quick detach device.
Background
An unmanned plane is an unmanned plane which is operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and along with the maturity of the unmanned plane technology, the unmanned plane is also widely applied to the fields of aerial photography, agriculture, plant protection, express transportation and the like.
However, the load overload structure that it carried of current unmanned aerial vehicle is for fixing the connection structure of difficult dismantlement, leads to having a great deal of inconvenient nature defect in installation and dismantlement in-process.
Disclosure of Invention
An object of the utility model is to provide an unmanned aerial vehicle load quick detach device, its installation of this unmanned aerial vehicle load quick detach device is simple swift with the dismantlement.
The utility model provides an unmanned aerial vehicle load quick detach device, unmanned aerial vehicle load quick detach device includes the load support, and the unmanned aerial vehicle load is fixed load support bottom department, unmanned aerial vehicle load quick detach device still includes:
the guide rail bracket and the load bracket form a sliding connection pair;
the quick-release host terminal is fixedly arranged at the bottom end of the guide rail bracket;
the quick-release load terminal is fixed at the top end of the load support, and the quick-release host terminal is connected with the quick-release load terminal in a clamping manner; and
and the clamping assembly is arranged between the guide rail bracket and the load bracket and used for realizing clamping connection between the guide rail bracket and the load bracket.
As a further improvement of the present invention, the sliding connection pair includes a pair of first sliding grooves and a pair of first guide rails, the first sliding grooves are formed in the bottom end of the rail bracket, and the first guide rails are formed in the top end of the load bracket.
As a further improvement, the chucking subassembly includes first button, and is a pair of first guide rail outside edge is installed respectively first button is a pair of be provided with on the first spout respectively with the first draw-in groove of first button looks chucking tight fit.
As a further improvement of the present invention, the clamping assembly further includes a first return spring, and the first return spring is disposed at the bottom end of the first button.
As a further improvement, the chucking assembly further comprises a second button and a second clamping groove, the second button is arranged on the quick-release load terminal, and the second clamping groove is arranged at the bottom end of the guide rail bracket.
As a further improvement of the utility model, unmanned aerial vehicle load quick detach device still includes a pair of second guide rail and a pair of second spout, and is a pair of the second spout is arranged the rail brackets bottom, and is a pair of the second guide rail is arranged the load support top.
As a further improvement of the present invention, a pair of the first sliding grooves are disposed adjacent to the two opposite side outer edges of the bottom end of the rail bracket, a pair of the second sliding grooves are disposed adjacent to the middle position of the bottom end of the rail bracket, the quick release host terminal is disposed between a pair of the second sliding grooves, a pair of the first guiding rails are disposed adjacent to the two opposite side outer edges of the top end of the load bracket, and a pair of the second guiding rails are disposed adjacent to the two opposite side outer edges of the top end of the quick release load terminal.
As a further improvement of the present invention, the clamping assembly further comprises a second return spring, and the second return spring is disposed at the bottom end of the second button.
As a further improvement of the present invention, the notches of the first and second chutes are respectively provided with a guide portion for inserting the first and second guide rails.
The utility model discloses following beneficial effect has: unmanned aerial vehicle load quick detach device in this scheme includes load support and rail brackets, docks between load support and the rail brackets through docking between quick detach host computer terminal and the quick detach load terminal, simultaneously between the two through the vice quick butt joint and the dismantlement of realizing between the two of sliding connection who forms to utilize the chucking subassembly to realize the locking function of the two.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
Fig. 1 is the utility model provides an unmanned aerial vehicle load quick detach device installation decomposition structure schematic diagram.
Fig. 2 is a schematic view of a three-dimensional structure of a rail bracket of the present invention.
Fig. 3 is a schematic view of a three-dimensional structure of the load support of the present invention.
Fig. 4 is a partially enlarged schematic view of a portion a in fig. 1.
Fig. 5 is a schematic view of a part of the enlarged structure at B in fig. 1.
In the figure:
1-load support, 2-guide rail support, 3-quick-release host terminal, 4-quick-release load terminal, 5-guide part, 11-first guide rail, 12-first button, 13-second guide rail, 14-second button, 21-first sliding groove, 22-second sliding groove, 23-second clamping groove and 24-first clamping groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely below, and it should be understood that the described embodiments are only some embodiments of the present invention, but not all embodiments. 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.
Referring to fig. 1 to 3, the present embodiment provides an unmanned aerial vehicle load quick release device, which includes a load support 1, a rail support 2, a quick release host terminal 3, a quick release load terminal 4 and a clamping assembly, wherein the unmanned aerial vehicle load is fixed at the bottom end of the load support 1. In order to facilitate the quick connection between the load support 1 and the guide rail support 2, a sliding connection pair is formed between the load support 1 and the guide rail support 2, namely, during installation, the load support 1 can be installed on the guide rail support 2 through the sliding connection pair, so that quick installation and positioning are realized. Quick detach host terminal 3 fixed mounting is in 2 bottoms of rail brackets, and quick detach load terminal 4 is fixed on 1 tops of load support, and quick detach host terminal 3 links to each other with quick detach load terminal 4 block, and quick detach host terminal 3 inserts and closes 4 quick detach load terminals promptly, realizes linking to each other of the two. The clamping assembly is arranged between the load bracket 1 and the guide rail bracket 2 and is used for realizing the fastening connection between the load bracket and the guide rail bracket. When the device is used and installed, the load support 1 is quickly installed on the guide rail support 2 in a sliding mode through the sliding connection pair, and after the load support slides in place, the load support and the guide rail support are clamped through the clamping assembly.
Referring to fig. 1 and 2 in combination, the sliding connection pair in the present embodiment includes a pair of first sliding grooves 21 and a pair of first guide rails 11, the pair of first sliding grooves 21 is formed at the bottom end of the guide rail bracket 2, and the pair of first guide rails 11 is formed at the top end of the load bracket 1. In other embodiments, a pair of first sliding grooves 21 are formed on both sides of the outer edge of the bottom end of the rail bracket 2, and correspondingly, a pair of first guide rails 11 are formed on both sides of the outer edge of the top end of the load bracket 1.
Referring to fig. 1, the clamping assembly in this embodiment includes a first button 12, a pair of first guide rails 11 are respectively mounted with the first button 12 at outer edges thereof, and a pair of first sliding grooves 21 are respectively provided with a first locking groove 24 which is in locking fit with the first button 12. When the clamping device is used, the top end of the first button 12 enters the first clamping groove 24 by vertically and upwards sliding the first button 12, so that the clamping function is realized; when the button needs to be detached, the first button 12 slides downwards, and the first button 12 falls off from the first clamping groove 24, so that the loosening function is realized. In some embodiments, in order to enable the first button 12 to automatically return to the neutral position (i.e., the home position) when the upward pushing of the latch or the downward pushing of the latch performs the release function, a return spring is provided at the first button 12, the return spring functioning to urge the first button 12 to automatically return to the home position.
In order to play a double-safety function, the clamping assembly further comprises a second button 14 and a second clamping groove 23, the second button 14 is arranged on the quick-release load terminal 4, and the second clamping groove 23 is arranged at the bottom end of the guide rail bracket 2; also, in order to enable the second button 14 to be automatically reset, a second reset spring is provided at the second button 14; through the setting of two buttons, can prevent between load support 1 and the guide rail bracket 2 unexpected drop.
Referring to fig. 1 and 2 in combination, in some embodiments, in order to improve the stability of the sliding connection between the load support 1 and the rail support 2 and enable the whole device to have greater bearing capacity, the rapid unmanned aerial vehicle load dismantling device further includes a pair of second guide rails 13 and a pair of second sliding grooves 22, the pair of second sliding grooves 22 is arranged at the bottom end of the rail support 2, and the pair of second guide rails 13 is arranged at the top end of the load support 1. The second sliding groove 22 is arranged at the middle position of the bottom end of the guide rail bracket 2, the quick-release main machine terminal 3 is arranged between the pair of second sliding grooves 22, and the pair of second guide rails 13 are arranged at the outer edges of two opposite sides of the top end of the quick-release load terminal 4.
In order to facilitate the fitting between the slide grooves and the guide rails, guide portions 5 for facilitating the insertion of the first guide rail 11 and the second guide rail 13 are provided at the notches of the first slide groove 21 and the second slide groove 22, respectively.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (9)
1. The utility model provides an unmanned aerial vehicle load quick detach device, unmanned aerial vehicle load quick detach device includes the load support, and the unmanned aerial vehicle load is fixed load support bottom department, its characterized in that, unmanned aerial vehicle load quick detach device still includes:
the guide rail bracket and the load bracket form a sliding connection pair;
the quick-release host terminal is fixedly arranged at the bottom end of the guide rail bracket;
the quick-release load terminal is fixed at the top end of the load support, and the quick-release host terminal is connected with the quick-release load terminal in a clamping manner; and
and the clamping assembly is arranged between the guide rail bracket and the load bracket and used for realizing clamping connection between the guide rail bracket and the load bracket.
2. The rapid dismounting device for unmanned aerial vehicle load according to claim 1, wherein the sliding connection pair comprises a pair of first sliding grooves formed at a bottom end of the rail bracket and a pair of first guide rails formed at a top end of the load bracket.
3. The fast dismounting device for unmanned aerial vehicle load according to claim 2, wherein the clamping assembly comprises a first button, the first button is mounted on the outer edges of the pair of first guide rails respectively, and a first clamping groove is formed in the pair of first sliding grooves and is in clamping fit with the first button.
4. The rapid dismounting device for unmanned aerial vehicle load according to claim 3, wherein the clamping assembly further comprises a first return spring disposed at a bottom end of the first button.
5. The rapid dismounting device for load of unmanned aerial vehicle according to claim 1, wherein said clamping assembly further comprises a second button and a second clamping groove, said second button is disposed on said rapid dismounting load terminal, said second clamping groove is disposed at the bottom end of said rail bracket.
6. The rapid load release device for unmanned aerial vehicle of claim 3, further comprising a pair of second guide rails and a pair of second sliding grooves, the pair of second sliding grooves being disposed at the bottom end of the rail bracket, and the pair of second guide rails being disposed at the top end of the load bracket.
7. The rapid release device for unmanned aerial vehicle load according to claim 6, wherein a pair of the first sliding grooves are disposed adjacent to two opposite outer edges of the bottom end of the rail bracket, a pair of the second sliding grooves are disposed adjacent to a middle position of the bottom end of the rail bracket, the rapid release host terminal is disposed between a pair of the second sliding grooves, a pair of the first guide rails are disposed adjacent to two opposite outer edges of the top end of the load bracket, and a pair of the second guide rails are disposed adjacent to two opposite outer edges of the top end of the rapid release load terminal.
8. The rapid dismounting device for unmanned aerial vehicle load according to claim 5, wherein the clamping assembly further comprises a second return spring, and the second return spring is disposed at a bottom end of the second button.
9. The fast dismounting device for unmanned aerial vehicle load according to claim 6, wherein the notches of the first sliding chute and the second sliding chute are respectively provided with a guiding portion for facilitating insertion of the first guiding rail and the second guiding rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023253513.3U CN214690229U (en) | 2020-12-29 | 2020-12-29 | Unmanned aerial vehicle load quick detach device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023253513.3U CN214690229U (en) | 2020-12-29 | 2020-12-29 | Unmanned aerial vehicle load quick detach device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214690229U true CN214690229U (en) | 2021-11-12 |
Family
ID=78562026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023253513.3U Active CN214690229U (en) | 2020-12-29 | 2020-12-29 | Unmanned aerial vehicle load quick detach device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214690229U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114572409A (en) * | 2022-05-07 | 2022-06-03 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
-
2020
- 2020-12-29 CN CN202023253513.3U patent/CN214690229U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114572409A (en) * | 2022-05-07 | 2022-06-03 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
| CN114572409B (en) * | 2022-05-07 | 2022-07-29 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN214690229U (en) | Unmanned aerial vehicle load quick detach device | |
| CN102333419B (en) | Latch assembly and carrier with same | |
| CN117854979B (en) | Circuit breaker frame convenient to combination | |
| CN205588254U (en) | Instrument partial shipment platform | |
| CN205203369U (en) | Airborne elevator connection structure and have its aircraft | |
| KR970073861A (en) | Manual pallet changing device and method | |
| CN209921067U (en) | Current-receiving transition device and railway vehicle with same | |
| CN203544057U (en) | Part cart capable of transforming compartment as needed | |
| CN211628157U (en) | Novel computer machine case of easy dismouting | |
| CN210284652U (en) | Automatic fixture of unmanned aerial vehicle air park | |
| CN105736435A (en) | Integrally designed electrical control assembly in maglev centrifugal blower | |
| CN209274775U (en) | A kind of conveying assembly is with continuously taking electricity to communicate track | |
| CN210413545U (en) | Fixture switching and positioning mechanism | |
| CN216151641U (en) | Auxiliary assembly structure and transportation system of automobile front axle assembly | |
| CN108423176B (en) | Modularized fixed wing unmanned aerial vehicle | |
| CN102781767A (en) | Apparatus for assembling automobile parts | |
| CN221606103U (en) | Aircraft and battery mounting mechanism thereof | |
| CN208948219U (en) | A kind of track support frame connector of intelligence hangar system | |
| CN211466079U (en) | Splicing tooling plate based on rail type window plate | |
| CN215149064U (en) | Robot | |
| CN109319016A (en) | A kind of conveying assembly is with continuously taking electricity to communicate track | |
| CN204994129U (en) | Vehicle electrical apparatus box structure that commonality is strong | |
| CN212195042U (en) | Panoramic sunroof mechanism limiting clamping block structure and guide rail assembly thereof | |
| CN215967128U (en) | Vertical and horizontal positioning universal mechanism of inside and outside portal welding frock stand of fork truck | |
| CN211151839U (en) | Inverter assembly mounting mechanism of frequency converter cabinet |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 518000, 13th Floor, Building A4, Nanshan Zhiyuan, No. 1001 Xueyuan Avenue, Changyuan Community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Country or region after: China Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN FEIMA ROBOTICS Co.,Ltd. Country or region before: China |
|
| CP03 | Change of name, title or address |