CN214296450U - Connect formula unmanned aerial vehicle wing truck soon - Google Patents
Connect formula unmanned aerial vehicle wing truck soon Download PDFInfo
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- CN214296450U CN214296450U CN202022315950.7U CN202022315950U CN214296450U CN 214296450 U CN214296450 U CN 214296450U CN 202022315950 U CN202022315950 U CN 202022315950U CN 214296450 U CN214296450 U CN 214296450U
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- wing
- trunk
- unmanned aerial
- aerial vehicle
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- 238000009434 installation Methods 0.000 claims abstract description 17
- 239000002245 particle Substances 0.000 claims description 13
- 238000009826 distribution Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 4
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 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
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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Abstract
The utility model discloses a rotary-connection type unmanned aerial vehicle wing trunk, which comprises a wing trunk, a conducting strip and a wing trunk mounting unit; wing trunk: the left end of the wing body is provided with a mounting frame, a mounting channel is formed in the wing body, a motor is mounted in the mounting frame, blades are mounted on an output shaft of the motor, a wire is arranged at the lower end of the motor and penetrates through the mounting channel on the inner side of the wing body, the conducting strip is fixedly connected to the right end of the wire and movably sleeved with the right end of the mounting channel on the inner side of the wing body, a spring is fixedly connected to the left end of the conducting strip, the left end of the spring is fixedly connected with the right part of the mounting channel on the inner side of the wing body, and a raised circular ring is arranged on the right part of the outer side surface of the wing body; a wing torso mounting unit. This connect formula unmanned aerial vehicle wing truck soon, when installation and dismantlement, very simple to save time, it is very convenient.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a connect formula unmanned aerial vehicle wing truck soon.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", 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. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. 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; at present, the unmanned aerial vehicle is 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, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology. Unmanned aerial vehicle uses up the back, need dismantle unmanned aerial vehicle and deposit, but current unmanned aerial vehicle wing truck is very loaded down with trivial details in installation and dismantlement to waste time, it is very inconvenient.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome current defect, provide a connect formula unmanned aerial vehicle wing truck soon, in installation and dismantlement, very simple to save time, it is very convenient, can effectively solve the problem in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: a rotary joint type unmanned aerial vehicle wing trunk comprises a wing trunk, a conducting strip and a wing trunk mounting unit;
wing trunk: the left end of the wing body is provided with a mounting frame, a mounting channel is formed in the wing body, a motor is mounted in the mounting frame, blades are mounted on an output shaft of the motor, a wire is arranged at the lower end of the motor and penetrates through the mounting channel on the inner side of the wing body, the conducting strip is fixedly connected to the right end of the wire and movably sleeved with the right end of the mounting channel on the inner side of the wing body, a spring is fixedly connected to the left end of the conducting strip, the left end of the spring is fixedly connected with the right part of the mounting channel on the inner side of the wing body, and a raised circular ring is arranged on the right part of the outer side surface of the wing body;
wing trunk installation unit: the right part of the outer side surface of the wing trunk is arranged;
wherein: still include the fuselage, the fuselage is located the right-hand side of wing truck, the left end of fuselage is provided with the screw hole to the bottom of screw hole is provided with electrically conductive groove and two evenly distributed's draw-in groove.
Further, wing truck installation unit contains sleeve pipe and screwed pipe, the medial surface of screwed pipe rotates the lateral surface right-hand member of connection at the wing truck, the left part of screwed pipe rotates with the ring rotation in the wing truck outside and is connected, the sleeve pipe activity cup joints the outside at the wing truck, sheathed tube right-hand member and the left end fixed connection of screwed pipe, the screwed pipe is connected with the screw hole screw thread of fuselage left end. Through rotating the sleeve pipe, the sleeve pipe rotates and can drive the screwed pipe and rotate, and the screwed pipe rotates and can be connected with the screw hole threaded connection of fuselage left end, then installs the wing truck on the fuselage.
Further, still include the friction grain, the friction grain sets up on the lateral surface of sleeve pipe, the friction grain is in the array distribution on the lateral surface of sleeve pipe. When the wing trunk is installed, the friction particles can be used for facilitating and facilitating installation.
Further, still include the rubber circle, rubber circle fixed connection is in the lateral surface left part of screwed pipe, the left end cooperation of rubber circle and fuselage. When the wing trunk is installed, the right end of the wing trunk can be prevented from causing friction loss to the fuselage through the rubber ring.
Further, still include the card axle, card axle fixed connection is at the right-hand member of wing trunk, the card axle has two and evenly distributed. When the wing trunk is installed, the clamping shaft can be clamped in the clamping groove of the fuselage through the clamping shaft, so that the wing trunk is installed more stably.
Further, still include the stationary blade, the stationary blade is the right angle stationary blade, stationary blade fixed connection is in the upper end of mounting bracket, the stationary blade has three and angular distribution such as. When the wing trunk is used, the motor can be clamped on the upper portion of the fixing sheet through the fixing sheet, and therefore the motor is firmer.
Compared with the prior art, the beneficial effects of the utility model are that: this connect formula unmanned aerial vehicle wing truck soon has following benefit:
1. the wing trunk of the rotary connection type unmanned aerial vehicle is provided with the wing trunk installation unit, the sleeve rotates to drive the threaded pipe to rotate through rotating the sleeve, the threaded pipe can be in threaded connection with a threaded hole in the left end of the body through rotating, and then the wing trunk is installed on the body;
2. the friction particles and the rubber rings are arranged on the wing trunk of the rotary joint type unmanned aerial vehicle, when the wing trunk is installed, the installation can be more convenient and quicker through the friction particles, and the friction loss of the right end of the wing trunk to the body can be prevented through the rubber rings;
3. this connect formula unmanned aerial vehicle wing truck soon, when installation and dismantlement, it is very simple to save time, it is very convenient, can effectively solve the problem in the background art.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a wing trunk cutting structure of the utility model;
FIG. 3 is a schematic view of the right side structure of the wing body of the present invention;
fig. 4 is an enlarged schematic view of the a position of the present invention.
In the figure: the airplane wing comprises a wing body 1, a mounting frame 2, a motor 3, blades 4, a lead 5, a spring 6, a conducting strip 7, a fuselage 8, a wing body mounting unit 9, a sleeve 91, a threaded pipe 92, friction particles 10, a rubber ring 11, a clamping shaft 12 and a fixing sheet 13.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, 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. 1-4, the present invention provides a technical solution: a rotary joint type unmanned aerial vehicle wing trunk comprises a wing trunk 1, a conducting strip 7 and a wing trunk mounting unit 9;
wing trunk 1: the left end of the wing body 1 is provided with a mounting frame 2, a mounting channel is formed in the wing body 1, a motor 3 is mounted in the mounting frame 2, an output shaft of the motor 3 is provided with a blade 4, the lower end of the motor 3 is provided with a wire 5, the wire 5 penetrates through the mounting channel on the inner side of the wing body 1, a conducting strip 7 is fixedly connected to the right end of the wire 5, the conducting strip 7 is movably sleeved with the right end of the mounting channel on the inner side of the wing body 1, the left end of the conducting strip 7 is fixedly connected with a spring 6, the left end of the spring 6 is fixedly connected with the right part of the mounting channel on the inner side of the wing body 1, and the right part of the outer side surface of the wing body 1 is provided with a raised circular ring; still include card axle 12, card axle 12 fixed connection is at the right-hand member of wing trunk 1, and card axle 12 has two and evenly distributed. Still include stationary blade 13, stationary blade 13 is the right angle stationary blade, and stationary blade 13 fixed connection has three and angular distribution such as at the upper end of mounting bracket 2, stationary blade 13. When the wing trunk 1 is installed, the clamping shaft 12 can be clamped in the clamping groove of the fuselage 8 through the clamping shaft 12, so that the installation of the wing trunk 1 is more stable. When the wing trunk 1 is used, the motor 3 can be clamped on the upper part of the fixing sheet 13 through the fixing sheet 13, so that the motor 3 is firmer;
wing trunk mounting unit 9: is arranged at the right part of the outer side surface of the wing body 1; wing trunk installation unit 9 contains sleeve pipe 91 and screwed pipe 92, and the medial surface of screwed pipe 92 rotates to be connected at the lateral surface right-hand member of wing trunk 1, and the left part of screwed pipe 92 rotates with the ring in the wing trunk 1 outside to be connected, and sleeve pipe 91 activity cup joints in the outside of wing trunk 1, and the right-hand member of sleeve pipe 91 and the left end fixed connection of screwed pipe 92, screwed pipe 92 and the screw hole threaded connection of fuselage 8 left end. The friction particle friction structure further comprises friction particles 10, wherein the friction particles 10 are arranged on the outer side face of the sleeve 91, and the friction particles 10 are distributed on the outer side face of the sleeve 91 in an array mode. Still include rubber circle 11, rubber circle 11 fixed connection is in the lateral surface left part of screwed pipe 92, and the left end cooperation of rubber circle 11 and fuselage 8. By rotating the sleeve 91, the sleeve 91 rotates to drive the threaded pipe 92 to rotate, the threaded pipe 92 rotates to be in threaded connection with a threaded hole at the left end of the fuselage 8, and then the wing trunk 1 is installed on the fuselage 8. When the wing trunk 1 is installed, the friction particles 10 can be used for facilitating and improving installation. When the wing trunk 1 is installed, the right end of the wing trunk 1 can be prevented from causing friction loss on the fuselage 8 through the rubber ring 11;
wherein: still include fuselage 8, fuselage 8 is located the right-hand side of wing trunk 1, and the left end of fuselage 8 is provided with the screw hole to the bottom of screw hole is provided with electrically conductive groove and two evenly distributed's draw-in groove.
Claims (6)
1. The utility model provides a connect formula unmanned aerial vehicle wing truck soon which characterized in that: comprises a wing trunk (1), a conducting strip (7) and a wing trunk mounting unit (9);
wing trunk (1): mounting bracket (2) is installed at the left end, the installation channel has been seted up to the inside of wing truck (1), install motor (3) in mounting bracket (2), install blade (4) on the output shaft of motor (3), the lower extreme of motor (3) is provided with wire (5), wire (5) pass the inboard installation channel of wing truck (1), conducting strip (7) fixed connection is at the right-hand member of wire (5), conducting strip (7) and the inboard installation channel right-hand member activity of wing truck (1) cup joint, the left end fixedly connected with spring (6) of conducting strip (7), the left end of spring (6) and the inboard installation channel right part fixed connection of wing truck (1), the lateral surface right part of wing truck (1) is provided with bellied ring;
wing trunk mounting unit (9): is arranged at the right part of the outer side surface of the wing trunk (1);
wherein: still include fuselage (8), fuselage (8) are located the right-hand side of wing truck (1), the left end of fuselage (8) is provided with the screw hole to the bottom of screw hole is provided with electrically conductive groove and two evenly distributed's draw-in groove.
2. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 1, wherein: wing trunk installation unit (9) contain sleeve pipe (91) and screwed pipe (92), the medial surface of screwed pipe (92) rotates the lateral surface right-hand member of connection at wing trunk (1), the left part of screwed pipe (92) rotates with the ring in wing trunk (1) outside to be connected, sleeve pipe (91) activity cup joints the outside at wing trunk (1), the right-hand member of sleeve pipe (91) and the left end fixed connection of screwed pipe (92), screwed pipe (92) and the screw hole threaded connection of fuselage (8) left end.
3. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 2, wherein: the friction particle array is characterized by further comprising friction particles (10), wherein the friction particles (10) are arranged on the outer side face of the sleeve (91), and the friction particles (10) are distributed on the outer side face of the sleeve (91) in an array mode.
4. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 2, wherein: still include rubber circle (11), rubber circle (11) fixed connection is in the lateral surface left part of screwed pipe (92), the left end cooperation of rubber circle (11) and fuselage (8).
5. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 1, wherein: still include card axle (12), card axle (12) fixed connection is at the right-hand member of wing trunk (1), card axle (12) have two and evenly distributed.
6. The wing trunk of a swivel-joint unmanned aerial vehicle of claim 1, wherein: still include stationary blade (13), stationary blade (13) are the right angle stationary blade, stationary blade (13) fixed connection is in the upper end of mounting bracket (2), stationary blade (13) have three and angular distribution such as.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022315950.7U CN214296450U (en) | 2020-10-18 | 2020-10-18 | Connect formula unmanned aerial vehicle wing truck soon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022315950.7U CN214296450U (en) | 2020-10-18 | 2020-10-18 | Connect formula unmanned aerial vehicle wing truck soon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214296450U true CN214296450U (en) | 2021-09-28 |
Family
ID=77840650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022315950.7U Expired - Fee Related CN214296450U (en) | 2020-10-18 | 2020-10-18 | Connect formula unmanned aerial vehicle wing truck soon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214296450U (en) |
-
2020
- 2020-10-18 CN CN202022315950.7U patent/CN214296450U/en not_active Expired - Fee Related
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| 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: 20210928 |
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| CF01 | Termination of patent right due to non-payment of annual fee |