CN214824108U - Unmanned aerial vehicle with detachable wings - Google Patents
Unmanned aerial vehicle with detachable wings Download PDFInfo
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- CN214824108U CN214824108U CN202120750970.9U CN202120750970U CN214824108U CN 214824108 U CN214824108 U CN 214824108U CN 202120750970 U CN202120750970 U CN 202120750970U CN 214824108 U CN214824108 U CN 214824108U
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Abstract
The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to indicate a wing can disassemble unmanned aerial vehicle, it includes the unmanned aerial vehicle body, wing connection port, the socket, the wing dead lever, the screw, connecting wire and frame, wing connection port and socket all set up in the both sides of unmanned aerial vehicle body, wing connection port is located the top of socket, wing connection port is used for the thread tightening wing dead lever, the socket is used for fixed and electric connection connecting wire, the one end threaded connection of wing connection port and wing dead lever, the other end and the screw fixed connection of wing dead lever, the screw passes through the connecting wire and the socket electricity is connected, the bottom fixed connection of frame and unmanned aerial vehicle body, the inside of unmanned aerial vehicle body is provided with main control system and battery, battery and socket all are connected with the main control system electricity. The utility model provides a detachable unmanned aerial vehicle of wing disassemble with assemble simple and conveniently, be convenient for accomodate.
Description
Technical Field
The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to indicate a wing can disassemble unmanned aerial vehicle.
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. The unmanned aerial vehicle that can disassemble to the wing that uses at present disassembles and assembles inconvenience.
Disclosure of Invention
The to-be-solved technical problem of the utility model is to provide a wing can disassemble unmanned aerial vehicle, this wing can disassemble unmanned aerial vehicle and disassemble and assemble simple and conveniently, is convenient for accomodate.
In order to solve the technical problem, the utility model discloses a following technical scheme:
the utility model provides an unmanned aerial vehicle can be disassembled to wing, it includes the unmanned aerial vehicle body, wing connection port, the socket, the wing dead lever, the screw, connecting wire and frame, wing connection port and socket all set up in the both sides of unmanned aerial vehicle body, wing connection port is located the top of socket, wing connection port is used for the thread tightening wing dead lever, the socket is used for fixed and electricity to connect the connecting wire, the one end threaded connection of wing connection port and wing dead lever, the other end and the screw fixed connection of wing dead lever, the screw passes through the connecting wire and the socket electricity is connected, the bottom fixed connection of frame and unmanned aerial vehicle body, the inside of unmanned aerial vehicle body is provided with main control system and battery, battery and socket all are connected with the main control system electricity.
Further, the bottom of unmanned aerial vehicle body is provided with the surveillance camera head, the surveillance camera head is located between the frame, the surveillance camera head is connected with the main control system electricity.
Further, a fixed block is arranged at the bottom of the wing fixing rod, and the connecting wire penetrates through the fixed block and is fixed.
Further, the both sides of unmanned aerial vehicle body are provided with the protection casing, the protection casing is located the socket under, the protection casing can cover and locate the socket.
Further, the front end surface of unmanned aerial vehicle body inlays and is equipped with connection status indicator, connection status indicator sets up with the socket one-to-one, connection status indicator is connected with the main control system electricity.
The utility model has the advantages that: during the in-service use, the unmanned aerial vehicle body is used for the device of erection joint, wing connection port is used for fixed wing dead lever, through the thread tightening, it is detachable to realize the wing, be convenient for place and accomodate, the wing dead lever is used for installing the screw, the screw provides flight support to the unmanned aerial vehicle body, the connecting wire is used for being connected screw and socket electricity and supplies power and make it receive the control of main control system, the socket is used for inserting and fixed connection line, can carry out the plug simultaneously, the frame is used for supporting the unmanned aerial vehicle body. The utility model provides a detachable unmanned aerial vehicle of wing disassemble with assemble simple and conveniently, be convenient for accomodate.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Description of reference numerals: unmanned aerial vehicle body 1, surveillance camera head 11, protection casing 12, status indicator 13, wing connection port 2, socket 3, wing dead lever 4, fixed block 41, screw 5, connecting wire 6, frame 7.
Detailed Description
In order to facilitate understanding of those skilled in the art, the present invention will be further described with reference to the following examples and drawings, which are not intended to limit the present invention.
As shown in figure 1, the utility model provides an unmanned aerial vehicle with detachable wings, which comprises an unmanned aerial vehicle body 1, a wing connecting port 2 and a socket 3, wing dead lever 4, screw 5, connecting wire 6 and frame 7, wing connection port 2 and socket 3 all set up in the both sides of unmanned aerial vehicle body 1, wing connection port 2 is located socket 3's top, wing connection port 2 is used for thread tightening wing dead lever 4, socket 3 is used for fixed and electricity to connect connecting wire 6, the one end threaded connection of wing connection port 2 and wing dead lever 4, the other end and the 5 fixed connection of screw of wing dead lever 4, screw 5 is connected through connecting wire 6 and 3 electricity of socket, the bottom fixed connection of frame 7 and unmanned aerial vehicle body 1, the inside of unmanned aerial vehicle body 1 is provided with main control system and battery, battery and socket 3 all are connected with the main control system electricity.
During the in-service use, unmanned aerial vehicle body 1 is used for the device of erection joint, wing connection port 2 is used for fixed wing dead lever 4, through the thread tightening, it can disassemble to realize the wing, be convenient for place and accomodate, wing dead lever 4 is used for installing screw 5, screw 5 provides flight support to unmanned aerial vehicle body 1, connecting wire 6 is used for being connected screw 5 and 3 electricity of socket and supplies power and make it receive the control of main control system to screw 5, socket 3 is used for inserting and fixed connection line 6, the plug can be carried out simultaneously, frame 7 is used for supporting unmanned aerial vehicle body 1.
The utility model provides a detachable unmanned aerial vehicle of wing disassemble with assemble simple and conveniently, be convenient for accomodate.
As shown in fig. 1, in this embodiment, the bottom of the unmanned aerial vehicle body 1 is provided with a monitoring camera 11, the monitoring camera 11 is located between the frames 7, and the monitoring camera 11 is electrically connected with the control host. During the in-service use, through setting up surveillance camera head 11, can support unmanned aerial vehicle body 1 to realize aerial control shooting.
As shown in fig. 1, in this embodiment, a fixing block 41 is disposed at the bottom of the wing fixing rod 4, and the connecting wire 6 is inserted into the fixing block 41 and fixed. During the in-service use, fixed block 41 is used for fixed connection 6, fixes connection 6 on wing dead lever 4, and the taking in of connection 6 of being convenient for makes it can not influence the normal flight of unmanned aerial vehicle body 1.
As shown in fig. 1, in this embodiment, two sides of the unmanned aerial vehicle body 1 are provided with protective covers 12, the protective covers 12 are located under the sockets 3, and the protective covers 12 can cover the sockets 3. During the in-service use, protection casing 12 is used for protecting socket 3, and is waterproof dustproof for socket 3 uses when idle.
As shown in fig. 1, in this embodiment, a connection status indicator lamp 13 is embedded in the front end surface of the unmanned aerial vehicle body 1, the connection status indicator lamps 13 are arranged in one-to-one correspondence with the sockets 3, and the connection status indicator lamps 13 are electrically connected with the control host. During the in-service use, connection status indicator 13 is used for showing the operating condition of present unmanned aerial vehicle body 1's socket 3, and corresponding connecting wire 6 inserts socket 3, and then the connection status indicator 13 that corresponds will light, and the people of being convenient for directly look over whether connect properly.
All the technical features in the embodiment can be freely combined according to actual needs.
The above embodiments are preferred implementations of the present invention, and in addition, the present invention includes other implementations, and any obvious replacement is within the protection scope of the present invention without departing from the concept of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle can be disassembled to wing which characterized in that: including the unmanned aerial vehicle body, wing connection port, the socket, the wing dead lever, the screw, connecting wire and frame, wing connection port and socket all set up in the both sides of unmanned aerial vehicle body, wing connection port is located the top of socket, wing connection port is used for thread tightening wing dead lever, the socket is used for fixed and electricity to connect the connecting wire, the one end threaded connection of wing connection port and wing dead lever, the other end and the screw fixed connection of wing dead lever, the screw passes through the connecting wire and the socket electricity is connected, the bottom fixed connection of frame and unmanned aerial vehicle body, the inside of unmanned aerial vehicle body is provided with main control system and battery, battery and socket all are connected with the main control system electricity.
2. The wing-dismantlable drone of claim 1, wherein: the bottom of unmanned aerial vehicle body is provided with the surveillance camera head, the surveillance camera head is located between the frame, the surveillance camera head is connected with the main control system electricity.
3. The wing-dismantlable drone of claim 1, wherein: the bottom of the wing fixing rod is provided with a fixing block, and the connecting wire penetrates through the fixing block and is fixed.
4. The wing-dismantlable drone of claim 1, wherein: the both sides of unmanned aerial vehicle body are provided with the protection casing, the protection casing is located the socket under, the protection casing can cover and locate the socket.
5. The wing-dismantlable drone of claim 1, wherein: the front end surface of unmanned aerial vehicle body inlays and is equipped with connection status indicator, connection status indicator sets up with the socket one-to-one, connection status indicator is connected with the main control system electricity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120750970.9U CN214824108U (en) | 2021-04-13 | 2021-04-13 | Unmanned aerial vehicle with detachable wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120750970.9U CN214824108U (en) | 2021-04-13 | 2021-04-13 | Unmanned aerial vehicle with detachable wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214824108U true CN214824108U (en) | 2021-11-23 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120750970.9U Active CN214824108U (en) | 2021-04-13 | 2021-04-13 | Unmanned aerial vehicle with detachable wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214824108U (en) |
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2021
- 2021-04-13 CN CN202120750970.9U patent/CN214824108U/en active Active
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