CN220448168U - Simple dismounting structure for unmanned aerial vehicle wing - Google Patents
Simple dismounting structure for unmanned aerial vehicle wing Download PDFInfo
- Publication number
- CN220448168U CN220448168U CN202322035988.2U CN202322035988U CN220448168U CN 220448168 U CN220448168 U CN 220448168U CN 202322035988 U CN202322035988 U CN 202322035988U CN 220448168 U CN220448168 U CN 220448168U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- wing
- block
- installation piece
- 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
- 230000007246 mechanism Effects 0.000 claims abstract description 21
- 238000009434 installation Methods 0.000 claims abstract description 16
- 230000006978 adaptation Effects 0.000 claims abstract description 3
- 238000000034 method Methods 0.000 abstract description 3
- 230000008569 process Effects 0.000 abstract description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a simple dismounting structure of an unmanned aerial vehicle wing, which comprises the following components: unmanned aerial vehicle body connects dismouting mechanism, connect dismouting mechanism setting on the unmanned aerial vehicle body, connect dismouting mechanism including the installation piece, the installation piece is installed on the right side of unmanned aerial vehicle body, the right side of installation piece is provided with the wing body, the fixture block is installed in the left side of wing body, the draw-in groove with fixture block looks adaptation has been seted up on the right side of installation piece and the position that corresponds the fixture block. According to the utility model, the wing and the unmanned aerial vehicle are conveniently detached through the mutual matching of the mounting blocks, the wing body, the clamping blocks, the clamping grooves, the fixing grooves, the threaded rods, the rotating blocks, the movable plates, the positioning rods and the limiting plates, so that the disassembly and assembly processes are simple and convenient, the occupied space of a user carrying the unmanned aerial vehicle to use the wing is reduced, the convenience in the later stage is improved, the wing is conveniently disassembled for overhauling and maintaining in the later stage, and the flexibility in use is improved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle wings, in particular to a simple dismounting structure of an unmanned aerial vehicle wing.
Background
Unmanned aircraft is abbreviated as "unmanned aerial vehicle", is unmanned aircraft that utilizes radio remote control equipment and self-contained program control device to control, and unmanned aerial vehicle is in fact unmanned aircraft's generic term, can divide into from technical angle definition: unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parachute wing aircraft and the like, and the fuselage and wings of a traditional unmanned aerial vehicle are mostly integrated.
According to the application number: CN202020352590.5, a take off and land unmanned aerial vehicle camera protection device perpendicularly, including main part, take off the module, withdraw protection piece power module, motor start module, main control module, descending module, emit protection piece power module, tail, the bottom fixed mounting of main part has the support frame of symmetric distribution, the top rotation of main part is connected with unmanned aerial vehicle front fan, the both sides fixed mounting of main part has the wing of symmetric distribution, the upper surface intermediate position of wing has unmanned aerial vehicle take off and land the fan thick stick through screw fixed mounting, the lower fixed surface of main part installs camera lens, the outside fixed mounting of camera lens has the protection piece, the right side of protection piece has the transmission shaft through threaded connection, the transmission shaft rotates to be connected in the worm.
Above-mentioned case unmanned aerial vehicle's fuselage and wing state as an organic wholely, because the area is great after the wing expandes to inconvenient people outdoor carrying can influence people's outdoor trip, then lead to then unable dismantlement of damaged wing to examine and repair and maintain when the wing appears damaging moreover, reduced the flexibility of practicality, and for this reason, we provide a simple and easy dismouting structure of unmanned aerial vehicle wing.
Disclosure of Invention
The utility model aims to provide a simple dismounting structure for an unmanned aerial vehicle wing, which aims to solve the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: simple and easy dismouting structure of unmanned aerial vehicle wing includes:
an unmanned aerial vehicle body;
the connection disassembly and assembly mechanism is arranged on the unmanned aerial vehicle body and comprises a mounting block, the mounting block is arranged on the right side of the unmanned aerial vehicle body, the right side of the mounting block is provided with a wing body, a clamping block is arranged on the left side of the wing body, a clamping groove matched with the clamping block is formed in the right side of the mounting block and corresponds to the position of the clamping block, and the left side of the clamping block penetrates through the clamping groove and extends to the inner wall of the clamping groove to be in contact with the inner wall of the clamping groove;
the limiting and fixing mechanism is arranged on the mounting block.
Preferably, the limiting and fixing mechanism comprises two fixing grooves, the number of the fixing grooves is two, the fixing grooves are respectively formed in the top and the bottom of the right side of the mounting block, and threaded rods are movably connected in grooves in the inner wall of the fixing grooves through bearings.
Preferably, one end of the threaded rod, which is far away from the clamping block, penetrates through the fixing groove and extends to the outside of the fixing groove, and one end of the threaded rod, which is far away from the clamping block, is provided with the rotating block.
Preferably, the surface threaded connection of threaded rod has the fly leaf, the left side of fixed slot inner wall top and bottom is through locating lever fixed connection, the surface of locating lever and the inner wall sliding contact of fly leaf.
Preferably, the right side of the movable plate penetrates through the fixed groove and extends to the outside of the fixed groove, the limiting plate is arranged on the right side of the movable plate, and the limiting plate is L-shaped.
Preferably, one side of the limiting plate, which is close to the wing body, is in contact with the wing body, one side of the limiting plate, which is close to the clamping block, is in contact with the clamping block, and one side of the limiting plate, which is close to the mounting block, is in sliding contact with the mounting block.
Compared with the prior art, the utility model has the following beneficial effects:
according to the utility model, the wing and the unmanned aerial vehicle are conveniently detached through the mutual matching of the mounting blocks, the wing body, the clamping blocks, the clamping grooves, the fixing grooves, the threaded rods, the rotating blocks, the movable plates, the positioning rods and the limiting plates, so that the disassembly and assembly processes are simple and convenient, the occupied space of a user carrying the unmanned aerial vehicle to use the wing is reduced, the convenience in the later stage is improved, the wing is conveniently disassembled for overhauling and maintaining in the later stage, and the flexibility in use is improved.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is an exploded view of the three-dimensional structure of the mounting block and wing body of the present utility model;
fig. 3 is a sectional view showing the structure of the front view of the connecting and dismounting mechanism and the limit fixing mechanism of the utility model.
In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a 2-connection dismounting mechanism, a 21 mounting block, a 22 wing body, a 23 clamping block, a 24 clamping groove, a 3-limit fixing mechanism, a 31 fixing groove, a 32 threaded rod, a 33 rotating block, a 34 movable plate, a 35 positioning rod and a 36 limiting plate.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-3, a simple dismounting structure for an unmanned aerial vehicle wing, comprising: unmanned aerial vehicle body 1 and connect dismouting mechanism 2, connect dismouting mechanism 2 setting on unmanned aerial vehicle body 1, connect dismouting mechanism 2 including installation piece 21, installation piece 21 installs on the right side of unmanned aerial vehicle body 1, the right side of installation piece 21 is provided with wing body 22, the left side fixedly connected with fixture block 23 of wing body 22, the draw-in groove 24 with fixture block 23 looks adaptation has been seted up on the right side of installation piece 21 and the position that corresponds fixture block 23, the left side of fixture block 23 runs through draw-in groove 24 and extends to its inside and the inner wall mutual contact of draw-in groove 24.
The limiting and fixing mechanism 3 is arranged on the mounting block 21, the limiting and fixing mechanism 3 comprises fixing grooves 31, the number of the fixing grooves 31 is two, the top and the bottom of the right side of the mounting block 21 are respectively arranged in grooves of the inner wall of the fixing grooves 31, threaded rods 32 are movably connected with the grooves 31 through bearings, one ends of the threaded rods 32, which are far away from the clamping blocks 23, penetrate through the fixing grooves 31 and extend to the outer parts of the fixing grooves, one ends of the threaded rods 32, which are far away from the clamping blocks 23, are fixedly connected with rotating blocks 33, one sides of the rotating blocks 33, which are close to the mounting block 21, are in rotary contact with the mounting block 21, the surfaces of the threaded rods 32 are in threaded connection with movable plates 34, one sides of the movable plates 34, which are close to the inner walls of the fixing grooves 31, are in contact with the inner walls of the fixing grooves 31, the left sides of the top and the bottom of the inner walls of the fixing grooves 31 are fixedly connected with positioning rods 35 through positioning rods 35, the surfaces of the movable plates 34 are in sliding contact with the inner walls of the movable plates 34, the right sides of the movable plates 34 penetrate through the fixing grooves 31 and extend to the outer parts, the right sides of the movable plates 34 are fixedly connected with limiting plates 36, the shapes of the limiting plates 36 are L-shaped, one sides of the limiting plates 36, which are close to the wing body 22 are in contact with the sliding blocks 22, one sides of the limiting plates 23, and one sides of the limiting plates 23 are in contact with the sliding blocks 21, and one side, which are close to the limiting blocks 23, which are in contact with the sliding blocks 23, and contacted with the sliding blocks 23.
Further, by providing the positioning rod 35, stability of the movable plate 34 when it moves is improved.
Specifically, during installation, the wing body 22 drives the clamping block 23 to be inserted into the clamping groove 24, then the rotating block 33 is rotated, the rotating block 33 drives the threaded rod 32 to rotate, the threaded rod 32 drives the limiting plate 36 to move close to the wing body 22 through the movable plate 34, and the limiting plate 36 is respectively contacted with the wing body 22 and the clamping block 23, so that the installation of the wing body 22 can be completed.
Through the mutually supporting of installation piece 21, wing body 22, fixture block 23, draw-in groove 24, fixed slot 31, threaded rod 32, rotatory piece 33, fly leaf 34, locating lever 35 and limiting plate 36 to conveniently tear wing and unmanned aerial vehicle open, make its dismouting process simple and convenient, reduced the space that the user carried unmanned aerial vehicle to use the wing to occupy, improved the convenience of later stage, the convenience of later stage is dismantled the wing moreover and is overhauld and maintain, has improved the flexibility when using.
When the wing assembly is used, the rotating block 33 is rotated, the rotating block 33 drives the threaded rod 32 to rotate, the threaded rod 32 drives the movable plate 34 to be far away from the clamping block 23, the movable plate 34 drives the limiting plate 36 to be far away from the wing body 22 to move, the limiting plate 36 is separated from the clamping block 23 and the wing body 22 respectively, then the wing body 22 is pulled rightwards, the wing body 22 drives the clamping block 23 to move rightwards, and the clamping block 23 and the clamping groove 24 are separated to finish disassembly.
To sum up: this simple and easy dismouting structure of unmanned aerial vehicle wing has solved the problem that proposes among the above-mentioned background art through the mutually supporting of installation piece 21, wing body 22, fixture block 23, draw-in groove 24, fixed slot 31, threaded rod 32, rotatory piece 33, fly leaf 34, locating lever 35 and limiting plate 36.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. Simple and easy dismouting structure of unmanned aerial vehicle wing, its characterized in that includes:
an unmanned plane body (1);
connect dismouting mechanism (2), connect dismouting mechanism (2) to set up on unmanned aerial vehicle body (1), connect dismouting mechanism (2) including installation piece (21), installation piece (21) are installed on the right side of unmanned aerial vehicle body (1), the right side of installation piece (21) is provided with wing body (22), fixture block (23) are installed on the left side of wing body (22), fixture block (24) with fixture block (23) looks adaptation are seted up on the right side of installation piece (21) and the position that corresponds fixture block (23), the left side of fixture block (23) runs through fixture groove (24) and extends to its inside and the inner wall mutual contact of fixture groove (24);
the limiting and fixing mechanism (3), and the limiting and fixing mechanism (3) is arranged on the mounting block (21).
2. The unmanned aerial vehicle wing simple dismounting structure of claim 1, wherein: the limiting and fixing mechanism (3) comprises fixing grooves (31), the number of the fixing grooves (31) is two, the two fixing grooves are respectively formed in the top and the bottom of the right side of the mounting block (21), and threaded rods (32) are movably connected in grooves in the inner wall of the fixing grooves (31) through bearings.
3. The unmanned aerial vehicle wing simple dismounting structure of claim 2, wherein: one end of the threaded rod (32) far away from the clamping block (23) penetrates through the fixing groove (31) and extends to the outside of the fixing groove, and one end of the threaded rod (32) far away from the clamping block (23) is provided with the rotating block (33).
4. A simple unmanned aerial vehicle wing disassembly and assembly structure according to claim 3, wherein: the surface threaded connection of threaded rod (32) has fly leaf (34), the left side of fixed slot (31) inner wall top and bottom is through locating lever (35) fixed connection, the surface of locating lever (35) and the inner wall sliding contact of fly leaf (34).
5. The unmanned aerial vehicle wing simple dismounting structure of claim 4, wherein: the right side of the movable plate (34) penetrates through the fixed groove (31) and extends to the outside of the fixed groove, a limiting plate (36) is arranged on the right side of the movable plate (34), and the limiting plate (36) is L-shaped.
6. The unmanned aerial vehicle wing simple dismounting structure of claim 5, wherein: one side of the limiting plate (36) close to the wing body (22) is in contact with the wing body (22), one side of the limiting plate (36) close to the clamping block (23) is in contact with the clamping block (23), and one side of the limiting plate (36) close to the mounting block (21) is in sliding contact with the mounting block (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322035988.2U CN220448168U (en) | 2023-08-01 | 2023-08-01 | Simple dismounting structure for unmanned aerial vehicle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322035988.2U CN220448168U (en) | 2023-08-01 | 2023-08-01 | Simple dismounting structure for unmanned aerial vehicle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220448168U true CN220448168U (en) | 2024-02-06 |
Family
ID=89732397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322035988.2U Active CN220448168U (en) | 2023-08-01 | 2023-08-01 | Simple dismounting structure for unmanned aerial vehicle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220448168U (en) |
-
2023
- 2023-08-01 CN CN202322035988.2U patent/CN220448168U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN112874759B (en) | Portable unmanned aerial vehicle for power grid inspection | |
| CN205273842U (en) | Unmanned aerial vehicle undercarriage folding joint structure that can expand fast and retrieve | |
| CN220448168U (en) | Simple dismounting structure for unmanned aerial vehicle wing | |
| CN106586010A (en) | Inspection device based on quadrotor unmanned aerial vehicle | |
| CN110743179A (en) | Model airplane and use method thereof | |
| CN209192224U (en) | A kind of easy-to-dismount propeller of unmanned plane | |
| CN209921610U (en) | Solar vertical take-off and landing type unmanned aerial vehicle | |
| CN110654538B (en) | Weather detection unmanned aerial vehicle | |
| CN112357072A (en) | Multi-rotor unmanned aerial vehicle | |
| CN212637895U (en) | Unmanned aerial vehicle horn device | |
| CN207106879U (en) | One kind controls the servo control mechanism that verts | |
| CN220041281U (en) | Cabin cover take-off and landing device for full-size airplane model dynamic display | |
| CN218949526U (en) | Unmanned aerial vehicle is patrolled and examined to electric power | |
| CN208484823U (en) | A kind of rotation folding structure of unmanned plane foot prop | |
| CN206288234U (en) | A kind of inspection device for being based on four rotor unmanned aircrafts | |
| CN219192575U (en) | Light unmanned aerial vehicle photoelectric nacelle | |
| CN205345317U (en) | Many rotor crafts of convenient to detach formula | |
| CN217424372U (en) | Aviation three-dimensional geographic information collector | |
| CN218750334U (en) | Unmanned aerial vehicle independently parks wireless charging device | |
| CN218113013U (en) | Unmanned aerial vehicle is used in cadastral survey and drawing | |
| CN220110402U (en) | Assembled airplane model | |
| CN212709931U (en) | Wingspan-direction folding mechanism of unmanned aerial vehicle | |
| CN218385751U (en) | Glass fiber reinforced plastic antenna housing structure | |
| CN220662875U (en) | Unmanned aerial vehicle aircraft | |
| CN112278240B (en) | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |