CN214267956U

CN214267956U - Novel unmanned aerial vehicle rapid disassembly structure

Info

Publication number: CN214267956U
Application number: CN202120281463.5U
Authority: CN
Inventors: 李洪岐; 葛国俊
Original assignee: Avic Hongrui Beijing Aviation Technology Co ltd
Current assignee: Avic Hongrui Beijing Aviation Technology Co ltd
Priority date: 2021-02-01
Filing date: 2021-02-01
Publication date: 2021-09-24
Anticipated expiration: 2031-02-01

Abstract

The utility model discloses a novel unmanned aerial vehicle rapid disassembly structure, including base and blotter, base one side is provided with the blotter of symmetry, its characterized in that: the utility model discloses a safety protection device for unmanned aerial vehicle, including base, safety protection device, unmanned aerial vehicle rapid disassembly structure, the base is close to the both sides of blotter and installs protective structure, one side fixedly connected with locking mechanism of base is kept away from to protective structure, locking mechanism keeps away from the fixed establishment of placing various devices of one side fixedly connected with of protective structure, this unmanned aerial vehicle rapid disassembly structure is through installing protection device, ensure unmanned aerial vehicle during operation, the power is stabilized and is supplied power, this rapid disassembly structure has locking mechanism, can ensure that unmanned aerial vehicle can not the shake of horn and the emergence accident at the flight in-process, the set casing surface is provided with the screw hole, the installation of the set casing horn of being convenient for, through installing the blotter, cushion the shock attenuation is carried out to the set casing, prevent that unmanned aerial vehicle from taking place violent vibrations and influencing normal flight at the flight in-process.

Description

Novel unmanned aerial vehicle rapid disassembly structure

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a novel unmanned aerial vehicle rapid disassembly structure.

Background

Unmanned aerial vehicle is commonly known as: unmanned aircraft, unmanned aerial vehicles, unmanned combat aircraft, bee-type machines; the unmanned aerial vehicle is provided with an automatic pilot, a program control device and other equipment, and personnel on the ground, a naval vessel or a mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the unmanned aerial vehicle through radar and other equipment.

Novel unmanned aerial vehicle can both be used in a lot of places in our life, and novel unmanned aerial vehicle can all be used in outdoor control of unmanned aerial vehicle and unmanned aerial vehicle broadcast etc. and the connected mode of current unmanned aerial vehicle horn is very loaded down with trivial details, can not install fast, influences unmanned aerial vehicle's normal work efficiency.

Therefore, a novel rapid dismounting structure of the unmanned aerial vehicle is provided.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a stable in structure, install quick convenient neotype unmanned aerial vehicle rapid disassembly structure to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: including base and cushion, base one side is provided with the blotter of symmetry, the protection architecture is installed to the both sides that the base is close to the blotter, one side fixedly connected with locking mechanism of base is kept away from to the protection architecture, locking mechanism keeps away from the fixed establishment of placing various devices of one side fixedly connected with of protection architecture.

Preferably, the protection structure includes protection shield, fender rod, protective housing and connecting plate, one side fixedly connected with protection shield that locking mechanism was kept away from to the base, protection shield both sides fixedly connected with fender rod, fender rod inner wall fixedly connected with protective housing, one side fixedly connected with connecting plate that the fender rod kept away from the protection shield, and protective housing and connecting plate fixed connection.

Preferably, locking mechanism includes fixing base, rotor arm and compresses tightly to detain, the fixing base is an integrated design with the base, the fixing base both sides are rotated and are connected with the rotor arm, the rotor arm is connected with compressing tightly through the pivot and detain the rotation.

Preferably, the fixing mechanism comprises a fixing shell, a fixing plate and a fixing block, the fixing plate is installed at the front end of the fixing shell, and the fixing block is installed on two sides of the fixing shell and connected with the fixing shell in an integrated mode.

Preferably, the surface of the fixed shell is provided with a threaded connecting hole.

Preferably, the cushion pad is made of rubber.

Compared with the prior art, the beneficial effects of the utility model are that:

(1) the utility model discloses an installation protection device ensures unmanned aerial vehicle during operation, and the power is stabilized and is supplied power.

(2) The device has locking mechanism, can ensure that unmanned aerial vehicle can not the shake of horn and the emergence accident at the flight in-process.

(3) The surface of the fixed shell is provided with a threaded hole, so that the installation of the fixed shell arm is facilitated.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the structure of the rotating device of the present invention;

fig. 3 is a schematic structural view of the fixing device of the present invention.

In the figure: 1. a base; 2. a protective structure; 21. a protection plate; 22. a guard bar; 23. a protective shell; 24. a connecting plate; 3. a locking mechanism; 31. a fixed seat; 32. a rotating arm; 33. pressing and fastening; 4. a fixing mechanism; 41. a stationary case; 42. a fixing plate; 43. a fixed block; 5. a cushion pad.

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.

Please refer to fig. 1, a novel rapid disassembly structure of an unmanned aerial vehicle in the figure, includes a base 1 and a buffer pad 5, a symmetrical buffer pad 5 is provided on one side of the base 1, a protection structure 2 is installed on two sides of the base 1 close to the buffer pad 5, one side of the base 1 is kept away from by the protection structure 2 and is fixedly connected with a locking mechanism 3, one side of the locking mechanism 3, which is kept away from by the protection structure 2, is fixedly connected with a fixing mechanism 4 for fixedly placing various devices, a power supply is put into the protection structure 2, the base 1 and the unmanned aerial vehicle are fixed, and when the unmanned aerial vehicle works, the buffer pad 5 buffers and damps the fixing mechanism 4.

Please refer to fig. 2, the protection structure 2 includes a protection plate 21, a protection rod 22, a protection shell 23 and a connection plate 24, the base 1 is far away from one side fixedly connected with protection plate 21 of the locking mechanism 3, the protection plate 21 is fixedly connected with protection rod 22 on two sides, the protection rod 22 is fixedly connected with protection shell 23 on the inner wall, the protection rod 22 is far away from one side fixedly connected with connection plate 24 of the protection plate 21, and the protection shell 23 is fixedly connected with the connection plate 24, the power is put into the protection shell 23 and is fixed well, the protection rod 22 fixes the protection shell 23 on the connection plate 24, when the unmanned aerial vehicle flies, the power can be stably fixed inside the protection shell 23 and can not be influenced by vibration, so that the electric energy transmission is unstable, the normal work of the unmanned aerial vehicle is affected, and the protection structure 2 ensures that the unmanned aerial vehicle works, and the power is stably supplied.

Referring to fig. 2, the locking mechanism 3 includes a fixing seat 31, a rotating arm 32 and a pressing buckle 33, the fixing seat 31 and the base 1 are integrally designed, the rotating arm 32 is rotatably connected to two sides of the fixing seat 31, and the rotating arm 32 is rotatably connected to the pressing buckle 33 through a rotating shaft.

Referring to fig. 3, the fixing mechanism 4 includes a fixing shell 41, a fixing plate 42 and a fixing block 43, the fixing plate 42 is installed at the front end of the fixing shell 41, the fixing blocks 43 are installed at two sides of the fixing shell 41 and are integrally connected, the quick release mechanism is in a connection state when the press buckle 33 is matched with the fixing block 43, and meanwhile, the stability of the quick release mechanism is ensured.

Referring to fig. 3, the surface of the fixing shell 41 is provided with a threaded connection hole, and the fixing shell 41 is connected with the arm of the unmanned aerial vehicle through the threaded hole, so that the stability of arm connection is ensured.

Please refer to fig. 2, the cushion pad 5 is made of rubber, and the rubber can make the fixing plate 42 and the fixing base 31 in soft contact, so that the fixing shell 41 is cushioned and damped during the flight of the unmanned aerial vehicle, thereby preventing the unmanned aerial vehicle from affecting the flight of the unmanned aerial vehicle due to severe shaking during the flight.

The working principle is as follows: the power is put into protective housing 23 internal fixation and is good, protective housing 23 is fixed on connecting plate 24 to fender rod 22, at unmanned aerial vehicle flight during operation, the power can be stably fixed inside protective housing 23, can not receive vibrations to influence, lead to electric energy transmission unstable, influence unmanned aerial vehicle's normal work, protective structure 2 ensures unmanned aerial vehicle during operation, the power is stabilized and is supplied power, it is fixed through base 1 and unmanned aerial vehicle, quick detach mechanism is in connected state when pressing and detaining 33 and fixed block 43 cooperation, unmanned aerial vehicle during operation, rubber can make fixed plate 42 and the soft contact of fixing base 31, make unmanned aerial vehicle flight in-process, cushion the shock attenuation to set casing 41, prevent that inside camera or scattering ware from colliding, influence normal work, set casing 41 is connected with unmanned aerial vehicle's horn through the screw hole, the stability of horn connection has been ensured.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a novel unmanned aerial vehicle rapid disassembly structure, includes base (1) and blotter (5), base (1) one side is provided with blotter (5) of symmetry, its characterized in that: protection architecture (2) are installed to base (1) both sides that are close to blotter (5), one side fixedly connected with locking mechanism (3) of base (1) are kept away from in protection architecture (2), one side fixedly connected with fixed placer's of protection architecture (2) fixed establishment (4) are kept away from in locking mechanism (3).

2. The novel rapid dismounting structure of unmanned aerial vehicle as claimed in claim 1, wherein: protection architecture (2) are including protection shield (21), fender rod (22), protective housing (23) and connecting plate (24), one side fixedly connected with protection shield (21) of locking mechanism (3) are kept away from in base (1), protection shield (21) both sides fixedly connected with fender rod (22), fender rod (22) inner wall fixedly connected with protective housing (23), one side fixedly connected with connecting plate (24) of protection shield (21) are kept away from in fender rod (22), and protective housing (23) and connecting plate (24) fixed connection.

3. The novel rapid dismounting structure of unmanned aerial vehicle as claimed in claim 1, wherein: locking mechanism (3) are including fixing base (31), rotor arm (32) and compress tightly knot (33), fixing base (31) and base (1) are a global design, fixing base (31) both sides are rotated and are connected with rotor arm (32), rotor arm (32) are connected through pivot and the rotation of pressing knot (33).

4. The novel rapid dismounting structure of unmanned aerial vehicle as claimed in claim 1, wherein: fixed establishment (4) are including set casing (41), fixed plate (42) and fixed block (43), the front end at set casing (41) is installed to fixed plate (42), both sides and as an organic whole connection at set casing (41) are installed in fixed block (43).

5. The novel rapid dismounting structure of unmanned aerial vehicle as claimed in claim 4, wherein: the surface of the fixed shell (41) is provided with a threaded connecting hole.

6. The novel rapid dismounting structure of unmanned aerial vehicle as claimed in claim 1, wherein: the buffer cushion (5) is made of rubber.