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CN-224225322-U - GPS quick detach structure and use its unmanned aerial vehicle

CN224225322UCN 224225322 UCN224225322 UCN 224225322UCN-224225322-U

Abstract

The application discloses a GPS quick-release structure and an unmanned aerial vehicle applying the same, and relates to the technical field of unmanned aerial vehicles. The application relates to an unmanned aerial vehicle, which comprises a machine body, a GPS module and a GPS quick-release structure, wherein the GPS quick-release structure comprises an installation arm, an installation position is arranged on the installation arm, and the GPS module is detachably arranged on the installation position. According to the unmanned aerial vehicle, when the unmanned aerial vehicle is impacted or damaged, maintenance personnel can rapidly maintain and replace the GPS module, and the maintenance efficiency of the unmanned aerial vehicle is effectively improved.

Inventors

  • YANG XIAOYING

Assignees

  • 深圳市九天展翼科技有限公司

Dates

Publication Date
20260512
Application Date
20250530

Claims (8)

  1. 1. The GPS quick-dismantling structure is used for quickly dismantling and installing a GPS module (7) and is characterized by comprising an installing arm (1), wherein an installing position is arranged on the installing arm (1), and the GPS module (7) is detachably arranged on the installing position; The GPS device comprises a GPS module (7), wherein a mounting arm (1) is provided with a mounting groove (2) for accommodating the GPS module (7), the mounting groove (2) is positioned at the mounting position, at least one side of the mounting groove (2) is provided with a deformable limiting part (3), and the limiting part (3) is in contact with the GPS module (7); one side of the limiting part (3) facing the GPS module (7) is provided with a limiting groove (4), the limiting groove (4) is provided with a first groove wall (4 a) and a second groove wall (4 b), and the first groove wall (4 a) and the second groove wall (4 b) respectively abut against two adjacent side parts of the GPS module (7).
  2. 2. The GPS quick release structure according to claim 1, wherein at least one end of the mounting groove (2) is provided with an operation port (5), and at least one end of the GPS module (7) is exposed in the operation port (5).
  3. 3. An unmanned aerial vehicle comprising a main body (6) and a GPS module (7), wherein the unmanned aerial vehicle further comprises the GPS quick release structure according to any one of claims 1-2 arranged on the main body (6).
  4. 4. A drone according to claim 3, characterized in that the mounting arm (1) has a first end (1 a) and a second end (1 b), the first end (1 a) being in rotational connection with the fuselage (6), the second end (1 b) being in detachable connection with the fuselage (6), the mounting location being arranged at the second end (1 b).
  5. 5. The unmanned aerial vehicle of claim 3, wherein the main body (6) comprises a casing (6 a), a camera module (6 b) arranged at one end of the casing (6 a), and a mounting chamber (6 c) arranged in the casing (6 a), wherein a picture transmission module (6 d) and a control module (6 e) are respectively arranged at two ends of the mounting chamber (6 c), and the picture transmission module (6 d) is arranged close to the camera module (6 b).
  6. 6. The unmanned aerial vehicle of claim 5, wherein at least one side of the housing (6 a) is provided with a heat dissipation air duct (8) communicated with the installation chamber (6 c), and one end of the heat dissipation air duct (8) is provided with an air inlet (9).
  7. 7. An unmanned aerial vehicle according to claim 3, wherein the wings (10) are respectively arranged on two opposite sides of the main body (6), the wings (10) are provided with third end parts (10 a) rotatably connected with the main body (6), two limiting blocks (11) are further arranged on the main body (6), the two limiting blocks (11) are in one-to-one correspondence with the two third end parts (10 a), and each limiting block (11) is respectively positioned on the corresponding rotating path of the third end part (10 a).
  8. 8. The unmanned aerial vehicle of claim 7, wherein the unmanned aerial vehicle body (6) is provided with two first pin holes (12), each first pin hole (12) is respectively inserted with a pin, the two first pin holes (12) are in one-to-one correspondence with the two wings (10), the third end part (10 a) is provided with a second pin hole (13), the wings (10) are also provided with empty slots (14) extending along the length direction of the wings, the wings (10) have an unfolding state and a folding state in the rotating stroke of the wings, when the wings (10) are in the unfolding state, the two pins are respectively in positive butt joint with the two second pin holes (13), and when the wings (10) are in the folding state, the two pins are respectively inserted into the two empty slots (14).

Description

GPS quick detach structure and use its unmanned aerial vehicle Technical Field The application relates to the technical field of unmanned aerial vehicles, in particular to a GPS quick-release structure and an unmanned aerial vehicle using the same. Background Unmanned aircraft is abbreviated as "unmanned aircraft", which is a unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programmed control device. At present, a GPS module is generally configured on the unmanned aerial vehicle, and functions of positioning, navigation, flight control, safety guarantee and the like of the unmanned aerial vehicle are realized through the GPS module. The existing unmanned aerial vehicle, GPS module and fuselage on it are the undetachable overall structure usually, receive impact or damage when unmanned aerial vehicle in the flight, maintenance personnel can't be quick maintain and change GPS module, this very big reduction unmanned aerial vehicle's maintenance efficiency. Disclosure of utility model The first object of the present application is to provide a GPS quick-release structure capable of achieving quick release and attachment of a GPS module. The application provides a GPS quick-dismantling structure, which adopts the following technical scheme: A GPS quick detach structure for carry out quick assembly disassembly to the GPS module, including the installation arm, arrange the installation position on the installation arm, the detachable setting of GPS module in on the installation position. Through adopting above-mentioned technical scheme, when unmanned aerial vehicle receives impact or damage, maintenance personal can be quick maintain and change the GPS module, the effectual maintenance efficiency who improves unmanned aerial vehicle. In a specific implementation manner, the mounting arm is provided with a mounting groove for accommodating the GPS module, the mounting groove is located at the mounting position, at least one side of the mounting groove is provided with a deformable limiting portion, and the limiting portion is in contact with the GPS module. By adopting the technical scheme, when the GPS module is accommodated in the mounting groove, the limit part can prop against the GPS module to improve the mounting strength of the GPS module, and when a maintainer dismounts the GPS module, the limit part can realize the abdication of the GPS module under the deformation of the limit part so as to complete the quick dismounting of the GPS module. In a specific implementation manner, a limit groove is formed in one side, facing the GPS module, of the limit portion, the limit groove is provided with a first groove wall and a second groove wall, and the first groove wall and the second groove wall respectively abut against two adjacent side portions of the GPS module. Through adopting above-mentioned technical scheme for first cell wall and second cell wall can carry out spacingly to the adjacent both sides portion of GPS module respectively, the effectual installation strength who improves the GPS module. In a specific embodiment, at least one end of the mounting slot is provided with an operation port, and at least one end of the GPS module is exposed to the operation port. Through adopting above-mentioned technical scheme for maintenance personnel can outwards push out the GPS module through the operation mouth, reduced the dismantlement degree of difficulty of GPS module, improved the dismantlement efficiency of GPS module. A second object of the application is to provide a drone. The unmanned aerial vehicle provided by the application adopts the following technical scheme: The utility model provides an unmanned aerial vehicle, includes machine body and GPS module, unmanned aerial vehicle is still including locating GPS quick detach structure as described above on the machine body. Through adopting above-mentioned technical scheme, when unmanned aerial vehicle receives impact or damage, maintenance personal can be quick maintain and change the GPS module, the effectual maintenance efficiency who improves unmanned aerial vehicle. In a specific embodiment, the mounting arm has a first end rotatably connected to the machine body and a second end detachably connected to the machine body, the mounting location being arranged at the second end. Through adopting above-mentioned technical scheme for maintenance personnel can upwards rise the second tip and carry out the dismouting to the GPS module on it, with avoid the body to cause the interference to the dismouting of GPS module, the effectual dismouting efficiency that improves the GPS module. In a specific implementation manner, the camera body comprises a casing, a camera module arranged at one end of the casing and an installation chamber arranged in the casing, wherein the two ends of the installation chamber are respectively provided with a picture transmission module and a control module, and the picture transmis