CN215884090U

CN215884090U - Quick detach mechanism based on unmanned aerial vehicle spare part

Info

Publication number: CN215884090U
Application number: CN202121841593.6U
Authority: CN
Inventors: 卢旭升
Original assignee: Avic Innovation Tianjin Technology Development Co ltd
Current assignee: Avic Innovation Tianjin Technology Development Co ltd
Priority date: 2021-08-06
Filing date: 2021-08-06
Publication date: 2022-02-22
Anticipated expiration: 2031-08-06

Abstract

The utility model discloses a quick-release mechanism based on unmanned aerial vehicle parts, which comprises a base cross rod, wherein a connecting cylinder is fixedly connected in the middle of the base cross rod, a vertical rod is arranged above the base cross rod, a fixing groove is formed in the top of the vertical rod, a fixing hole is formed in the surface of the vertical rod, which is close to the fixing groove, a quick-release mechanism is arranged at the top of the vertical rod, the quick-release mechanism comprises a placing cylinder, a clamping groove is formed in the placing cylinder, fixing plates are fixedly connected to two sides of the placing cylinder, fixing columns are fixedly connected to the inner parts of the fixing plates at the two sides, rotating shafts are fixedly connected to the tail ends of the fixing columns, a plurality of placing grooves are formed in the front and at the back of the placing cylinder, which is close to the bottom, buckles are arranged on the rotating shafts at the two sides, pushing blocks are fixedly connected to the bottoms of the buckles, and fixing buckles are fixedly connected to the tail ends of the pushing blocks. According to the utility model, the rapid disassembly of the unmanned aerial vehicle base can be realized through the design of the buckle, the rotating shaft, the fixing buckle and the fixing hole.

Description

Quick detach mechanism based on unmanned aerial vehicle spare part

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a quick release mechanism based on unmanned aerial vehicle parts.

Background

An unmanned aerial vehicle is a powered, unmanned aerial vehicle. The aircraft is generally composed of an aircraft body, a power device, a flight control and management device, a launching and recovery device and the like, can fly remotely or automatically, and can be used for one time and also can be recovered for multiple times. The electronic weapon is one of high and new technology weaponry at present, is widely applied to a plurality of military operations such as battlefield investigation, electronic countermeasure, post-war damage assessment, ground attack and the like, and is essential equipment for informatization war. In the civil field, it has been widely used in the fields of aerial remote sensing, aerial surveying and mapping, aerial photography, and the like.

But unmanned aerial vehicle can appear various circumstances when using for the part appears damaging, just need change its part in order to continue to use unmanned aerial vehicle, can not realize dismantling the change fast when nevertheless current unmanned aerial vehicle base part is changed.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the defects in the prior art, and provides a quick release mechanism based on unmanned aerial vehicle parts.

In order to achieve the purpose, the utility model adopts the following technical scheme: quick detach mechanism based on unmanned aerial vehicle spare part, including the base horizontal pole, fixedly connected with connecting cylinder in the middle of the base horizontal pole, base horizontal pole top is equipped with the montant, the montant top is equipped with the fixed slot, the montant surface is close to fixed slot department and is equipped with the fixed orifices, the montant top is equipped with quick detach mechanism.

As a further description of the above technical solution:

the quick detach mechanism is including placing a section of thick bamboo, place an inside draw-in groove that is equipped with of section of thick bamboo, place the equal fixedly connected with fixed plate in a both sides, the inside fixedly connected with fixed column of fixed plate in both sides, the terminal fixedly connected with pivot of fixed column, it is equipped with a plurality of standing grooves to place a section of thick bamboo near the bottom position front and back, be equipped with the buckle in the pivot of both sides, buckle bottom fixedly connected with promotes the piece, promote the fixed knot of the terminal fixedly connected with of piece.

As a further description of the above technical solution:

the base cross rod is fixedly connected with the vertical rod through the connecting cylinder, and the base cross rod is vertically connected with the vertical rod.

As a further description of the above technical solution:

the size of placing a section of thick bamboo is greater than the size of montant, the draw-in groove can mutually support with the fixed slot.

As a further description of the above technical solution:

the fixing buckle can be matched and fixed with the fixing hole, and the placing grooves are respectively arranged on two side walls of the placing barrel.

As a further description of the above technical solution:

the fixing buckle can be just inserted into the fixing hole when the vertical rod is inserted into the placing barrel.

As a further description of the above technical solution:

the buckle can not generate interference when the rotating shaft rotates, and the rotating shaft is kept fixed when the buckle rotates.

As a further description of the above technical solution:

the top of the placing cylinder is fixedly connected with a connecting block, and the left side surface of the placing cylinder is fixedly provided with a plurality of connecting plates.

The utility model has the following beneficial effects:

1. compared with the prior art, this quick detach mechanism based on unmanned aerial vehicle spare part promotes the piece through removing and makes the buckle rotate the quick dismantlement maintenance of being convenient for that fixed knot and fixed orifices separation can realize unmanned aerial vehicle base.

2. Compared with the prior art, this quick detach mechanism based on unmanned aerial vehicle spare part through the design of connecting cylinder and buckle, quick replacement comes into operation once more when can quick replacement base horizontal pole makes unmanned aerial vehicle part trouble.

Drawings

Fig. 1 is a schematic view of a three-dimensional mounting structure of a quick release mechanism based on components of an unmanned aerial vehicle according to the present invention;

fig. 2 is a schematic view of a three-dimensional structure of a base of a quick release mechanism based on components of an unmanned aerial vehicle according to the present invention;

fig. 3 is a schematic view of a three-dimensional bottom structure of a quick release mechanism based on components of an unmanned aerial vehicle according to the present invention;

fig. 4 is a schematic perspective surface structure diagram of a quick release mechanism based on components of an unmanned aerial vehicle according to the present invention.

Illustration of the drawings:

1. a base rail; 2. a vertical rod; 3. fixing grooves; 4. a fixing hole; 5. a connecting cylinder; 6. placing the cylinder; 7. a connecting plate; 8. connecting blocks; 9. a pushing block; 10. a rotating shaft; 11. a fixing buckle; 12. a card slot; 13. A fixing plate; 14. fixing a column; 15. a placement groove; 16. and (5) buckling.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Example (b):

referring to fig. 1-4, the utility model provides a quick release mechanism based on components of an unmanned aerial vehicle, which comprises: including base horizontal pole 1, fixedly connected with connecting cylinder 5 in the middle of the base

horizontal pole

1, 1 top of base horizontal pole is equipped with montant 2, base horizontal pole 1 is through connecting

cylinder

5 and 2 fixed connection of montant, base horizontal pole 1 is perpendicular with montant 2 and is connected and is used for supporting the unmanned aerial vehicle body, 2 tops of montant are equipped with fixed slot 3, fixed slot 3 is used for fixed montant 2 position of fixed montant 2 simultaneously with standing groove 15 cooperation is fixed to be placed, 2 surfaces of montant are close to 3 departments of fixed slot and are equipped with fixed orifices 4, fixed orifices 4 can realize the quick dismantlement of part base with fixed knot 11 cooperation is fixed, 2 tops of montant are equipped with quick detach mechanism, be convenient for dismantle fast of part.

The quick-release mechanism comprises a placing barrel 6, the placing barrel 6 is connected with a vertical rod 2 in a matched mode to keep the vertical rod 2 fixed, a clamping groove 12 is formed in the placing barrel 6 and is mutually matched and fixed with a fixing groove 3, a connecting block 8 is fixedly connected to the top of the placing barrel 6 and is used for being fixedly connected with an unmanned aerial vehicle, a plurality of connecting plates 7 are fixed on the left side surface of the placing barrel 6 and are convenient to fix with the unmanned aerial vehicle, fixing plates 13 are fixedly connected to two sides of the placing barrel 6 and are convenient to fix the stability of the mechanism with a buckle 16, fixing columns 14 are fixedly connected to the inner portions of the fixing plates 13 on the two sides, a rotating shaft 10 is fixedly connected to the tail ends of the fixing columns 14 and is convenient to fix the buckle 16, a plurality of placing grooves 15 are formed in the front and back of the position, the vertical rod 2 is convenient to insert into the placing barrel 6, the buckle 16 is arranged on the rotating shafts 10 on the two sides, and the buckle 16 rotates on the rotating shaft 10 to facilitate the fixed buckle 11 to be combined with and separated from the fixing hole 4, the bottom of the buckle 16 is fixedly connected with a pushing block 9, the buckle 16 is convenient to control to rotate, the tail end of the pushing block 9 is fixedly connected with a fixing buckle 11, and the vertical rod 2 and the placing cylinder 6 are convenient to fixedly connect.

The working principle is as follows: during the installation, will place a section of thick bamboo 6 and fix with unmanned through connecting block 8 and connecting plate 7, insert a section of thick bamboo 6 with montant 2 in, fixed slot 3 is fixed with the cooperation of draw-in groove 12, and control promotes 9 control buckles 16 of piece and rotates in pivot 10 for promote the terminal fixed knot 11 of 9 and insert and realize montant 2 and place a fixed connection on 6 in the fixed orifices 4 on 2 surfaces of montant. When the base is disassembled, the control pushing block 9 enables the buckle 16 to rotate, the fixing buckle 11 is separated from the fixing hole 4, and then the vertical rod 2 is drawn out from the placing barrel 6 to complete the disassembly.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.

Claims

1. Quick detach mechanism based on unmanned aerial vehicle spare part, including base horizontal pole (1), its characterized in that: fixedly connected with connecting cylinder (5) in the middle of base horizontal pole (1), base horizontal pole (1) top is equipped with montant (2), montant (2) top is equipped with fixed slot (3), montant (2) surface is close to fixed slot (3) department and is equipped with fixed orifices (4), montant (2) top is equipped with quick detach mechanism.

2. The quick release mechanism based on unmanned aerial vehicle spare part of claim 1, characterized in that: the quick detach mechanism is including placing a section of thick bamboo (6), place inside draw-in groove (12) that is equipped with of a section of thick bamboo (6), place the equal fixedly connected with fixed plate (13) in a section of thick bamboo (6) both sides, the inside fixedly connected with fixed column (14) of both sides fixed plate (13), fixed column (14) terminal fixedly connected with pivot (10), it is equipped with a plurality of standing grooves (15) to place a section of thick bamboo (6) around being close to the bottom position, be equipped with buckle (16) on pivot (10) of both sides, buckle (16) bottom fixedly connected with promotes piece (9), promote the fixed knot (11) of the terminal fixedly connected with of piece (9).

3. The quick release mechanism based on unmanned aerial vehicle spare part of claim 1, characterized in that: the base cross rod (1) is fixedly connected with the vertical rod (2) through the connecting cylinder (5), and the base cross rod (1) is vertically connected with the vertical rod (2).

4. The quick release mechanism based on unmanned aerial vehicle spare part of claim 2, characterized in that: the size of placing a section of thick bamboo (6) is greater than the size of montant (2), draw-in groove (12) can mutually support with fixed slot (3).

5. The quick release mechanism based on unmanned aerial vehicle spare part of claim 2, characterized in that: the fixing buckle (11) can be matched and fixed with the fixing hole (4), and the placing grooves (15) are respectively arranged on two side walls of the placing cylinder (6).

6. The quick release mechanism based on unmanned aerial vehicle spare part of claim 2, characterized in that: when the vertical rod (2) is inserted into the placing barrel (6), the fixing buckle (11) can be just inserted into the fixing hole (4).

7. The quick release mechanism based on unmanned aerial vehicle spare part of claim 2, characterized in that: the buckle (16) can not generate interference when the rotating shaft (10) rotates, and the rotating shaft (10) keeps fixed when the buckle (16) rotates.

8. The quick release mechanism based on unmanned aerial vehicle spare part of claim 2, characterized in that: the top of the placing cylinder (6) is fixedly connected with a connecting block (8), and the left side surface of the placing cylinder (6) is fixedly provided with a plurality of connecting plates (7).