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CN-224225320-U - Generalized unmanned aerial vehicle

CN224225320UCN 224225320 UCN224225320 UCN 224225320UCN-224225320-U

Abstract

The utility model discloses a generalized unmanned aerial vehicle, which belongs to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body is provided with a rack, the rack comprises a rack body, a standard interface is arranged on the rack body, and the standard interface can be detachably connected with an application standard component matched with the standard interface. The standard interfaces with the shapes of rectangular and the like are reserved in the center of the unmanned aerial vehicle main body, the outer walls of the application standard parts are detachably connected with the standard interfaces, and the function modules of the application standard parts can be designed into different functions, so that the application standard parts with the different function modules can be filled according to actual application scenes, and the application standard parts and the unmanned aerial vehicle with the main body flight platform can be fused to complete diversified tasks.

Inventors

  • MA LONGMIN
  • WEI KAIJING
  • Wen Binxin

Assignees

  • 广西座头鲸无人机科技有限公司

Dates

Publication Date
20260512
Application Date
20250512

Claims (10)

  1. 1. The universal unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body is provided with a rack, and the rack comprises a rack body and is characterized in that a standard interface is arranged on the rack body, and the standard interface can be detachably connected with an application standard component matched with the standard interface.
  2. 2. The generalized unmanned aerial vehicle of claim 1, wherein the standard interface is arranged in the middle of the frame body, the standard interface is in a rectangular or regular polygon structure, the standard interface is arranged in a vertically penetrating manner, and the unmanned aerial vehicle body is provided with an organism which is arranged on the frame body.
  3. 3. The generalized unmanned aerial vehicle of claim 2, wherein the outer wall of the middle part of the application standard component is of a rectangular or regular polygon structure matched with the standard interface so as to be inserted into the standard interface, and the top end of the application standard component protrudes outwards to form a hat brim-shaped structure.
  4. 4. The generalized unmanned aerial vehicle of claim 1, wherein the frame further comprises a tightening piece, the tightening piece comprises a tightening sub-piece and a tightening parent piece, the tightening parent pieces are arranged on the outer side of the standard interface of the frame body, the tightening sub-pieces can be arranged on the application standard piece, and the tightening sub-piece and the tightening parent piece are matched for use to be detachably connected.
  5. 5. The generalized unmanned aerial vehicle of claim 4, wherein the tightening piece is a buckle, the tightening female piece is a buckle, the tightening sub piece is a hook, and the buckle is capable of being connected to the hook in a buckled manner.
  6. 6. The generalized unmanned aerial vehicle of claim 5, wherein the clasp is a stainless steel flat-mouth clasp, an elongated clasp, a snap-on clasp, or an adjustment clasp.
  7. 7. The generalized unmanned aerial vehicle of claim 4, wherein the locking member is a latch lock, the locking female member is a latch member, the locking sub-member is a lock nose, the latch member is horizontally arranged, and the latch can extend or retract to be connected to the lock nose in a plugging manner.
  8. 8. The generalized unmanned aerial vehicle of claim 4, wherein the locking member is an electronic lock, the locking master member is an electronic control lock body, the locking sub-member is a lock set, and the electronic control lock body is electrically connected to a controller of the unmanned aerial vehicle body.
  9. 9. The generalized unmanned aerial vehicle of claim 8, wherein the electronic lock is an electric mortise lock, and an electric control lock body of the electric mortise lock is horizontally arranged and can extend or retract to be connected to the lock sleeve member in a plug-in connection manner.
  10. 10. The generalized unmanned aerial vehicle of claim 8, wherein the electronic lock is a magnetic lock, and an electric control lock body of the magnetic lock can be powered on to adsorb a lock set or powered off to release the lock set.

Description

Generalized unmanned aerial vehicle Technical Field The utility model relates to the technical field of unmanned aerial vehicles, in particular to a generalized unmanned aerial vehicle. Background Along with the development of unmanned aerial vehicle technology, the unmanned aerial vehicle has a wider application range, for example, a camera is arranged on a rotor unmanned aerial vehicle, the unmanned aerial vehicle is remotely controlled to cruise through a mobile phone and the like, shooting is carried out at the same time, for example, a stretching arm is required to be arranged on the rotor unmanned aerial vehicle for building detection, maintenance and the like, even a sucker structure is arranged at the front end of the stretching arm, the stretching arm is used for stretching, absorbing and fixing on the surface of a building, and carrying out detection operation, for example, an object is lifted and thrown at a designated position. The general unmanned aerial vehicle in market includes organism, frame, landing leg frame, trailing arm and rotor etc. is furnished with control system and power, and remote control unmanned aerial vehicle such as accessible remote control or cell-phone takes off, then cruises and carries out operation, returns to the journey, descends. For example, in the chinese patent literature, "a crack detection unmanned aerial vehicle, bulletin number CN216509120U", an example of a crack detection scheme for a building by a four-rotor unmanned aerial vehicle is described, and a cantilever arm and a crack detection mechanism including a mechanical working arm, a crack detector, and the like are disposed on the unmanned aerial vehicle body, and can slide and extend forward and backward along the cantilever arm, and further crack detection is realized by the crack detector, and landing gear is disposed for landing. As described above, although a general unmanned aerial vehicle has a chance to install the corresponding work components according to the actual work, it is difficult to replace and assemble the work components without disposing a general installation structure. Disclosure of utility model The utility model aims to solve the problems, and provides a generalized unmanned aerial vehicle which can be filled with application standard components of different functional modules according to actual application scenes to realize replacement and assembly of each operation component. In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows: The utility model provides a universalization unmanned aerial vehicle, includes the unmanned aerial vehicle body, and the unmanned aerial vehicle body disposes the frame, and the frame includes the support body, is provided with standard interface on the support body, and standard interface can be dismantled and be connected with the application standard spare with standard interface looks adaptation. The standard interface is arranged in the middle of the frame body and is of a rectangular or regular polygon structure. The standard interface can be a blind hole structure arranged at the top or bottom of the frame body, and the operation parts can only be stretched out above or below the unmanned aerial vehicle body to operate, preferably, the standard interface is arranged in a vertically penetrating mode so as to be convenient to plug in and complete assembly through the upper and lower spaces of the interface, and the operation parts can be plugged in the standard interface to complete assembly through the application of the standard parts no matter the operation parts are operated above the unmanned aerial vehicle body or operated below the unmanned aerial vehicle body. The middle outer wall of the application standard component is in a rectangular or regular polygon structure matched with the standard interface so as to be inserted into the standard interface. The top of the application standard piece protrudes outwards to form a hat brim-shaped structure, and the protruding hat brim can be put on the frame body to bear load, so that the fixing stability of the detachable connection structure is improved. The unmanned aerial vehicle body is provided with an organism, and the organism is arranged on the frame body. Specifically, the standard component is inserted into the standard interface of the frame body, and the frame body is connected with the outer wall (the back side of the standard interface) of the frame body through bolts or welded. In order to realize dismantling the connection and fixing, the frame still includes the binding member, and the binding member includes binding sub-piece and binding parent-piece, and a plurality of binding parent-piece is installed in the outside of the standard interface of support body, and a plurality of binding sub-piece can be installed in application standard spare, and binding sub-piece and binding parent-piece pair the use with dismantling the connec