CN219215396U

CN219215396U - Wing convenient to unmanned aerial vehicle installs

Info

Publication number: CN219215396U
Application number: CN202223449847.7U
Authority: CN
Inventors: 石武
Original assignee: Chongqing Camel Aviation Technology Co ltd
Current assignee: Chongqing Camel Aviation Technology Co ltd
Priority date: 2022-12-23
Filing date: 2022-12-23
Publication date: 2023-06-20
Anticipated expiration: 2032-12-23

Abstract

The utility model discloses a wing convenient for installation of an unmanned aerial vehicle, which comprises a fixed box, wherein a sliding rod is fixedly connected between the top and the bottom of an inner cavity of the fixed box, a sliding sleeve and a spring are sequentially sleeved on the surface of the sliding rod from top to bottom, a wing body is arranged on the right side of the fixed box, the left side of the wing body penetrates through the inner cavity of the fixed box, a mounting groove is formed in the left side of the wing body, a positioning groove is formed in the top of the inner cavity of the mounting groove, a fixed rod is fixedly connected to the right side of the sliding sleeve, and the right side of the fixed rod penetrates through the inner cavity of the mounting groove. According to the wing convenient to install, the unmanned aerial vehicle has the advantages of being stable and stable in fixation, preventing loosening, and being worthy of popularization.

Description

Wing convenient to unmanned aerial vehicle installs

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a wing convenient for installation of an unmanned aerial vehicle.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle adopting wireless remote control, is mainly used for aerial photography, agriculture, plant protection, miniature self-timer, express delivery transportation and the like, and in order to facilitate storage and carrying of the unmanned aerial vehicle, wings of the unmanned aerial vehicle are fixed by bolts;

the utility model comprises the following steps: "unmanned aerial vehicle wing of easy to assemble", patent number: "CN208915420U", this patent inserts the upper plate inside the sliding tray, realize the location of wing body through locating hole and reference column, compress tightly the wing body through the upper plate, realize the fixed of upper plate vertical direction through the sliding tray, realize the fixed of upper plate horizontal direction through locking mechanism, the wing body is fixed firm, and the dismouting of being convenient for, but this patent has the problem that is fixed inadequately firm, the wing adopts upper plate and fixing base centre gripping to fix, and only carry out spacing fixedly through locking post and locking spring to the upper plate, unmanned chance produces great vibration in the use, lead to locking spring to take place the shrink because of the vibration and lead to the unable fixed upper plate of locking post easily, make the wing take place not hard up and drop, be unfavorable for people's use.

Disclosure of Invention

The utility model aims to provide a wing convenient to install of an unmanned aerial vehicle, which has the advantages of being stable in fixation and preventing loosening, and solves the problem that the existing wing convenient to install of the unmanned aerial vehicle is easy to loosen after being installed.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle wing convenient to install, includes fixed box, fixedly connected with slide bar between the top and the bottom of fixed box inner chamber, the surface of slide bar is equipped with sliding sleeve and spring from last cover down in proper order, the right side of fixed box is provided with the wing body, the left side of wing body runs through the inner chamber to fixed box, the mounting groove has been seted up in the left side of wing body, the constant head tank has been seted up at the top of mounting groove inner chamber, the right side fixedly connected with dead lever of sliding sleeve, the right side of dead lever runs through the inner chamber to the mounting groove, the inner chamber of constant head tank is provided with the locating piece, the bottom and the dead lever fixedly connected with of locating piece, the top swing joint of fixed box inner chamber rear side has the rotary rod, the surface cover of rotary rod is equipped with the cam, the front side of rotary rod runs through fixed box and fixedly connected with knob, the bottom fixedly connected with control shell of fixed box, the right side of control shell is provided with the hand wheel, the left side fixedly connected with screw rod of hand lever, the left side of screw rod runs through control shell and swing joint has the adjustment shell, adjustment shell and fixed connection top box and fixed connection.

Preferably, the left side fixedly connected with mounting panel of fixed box, the mounting hole has all been seted up at the top and the bottom of mounting panel left side, the left side fixedly connected with protection pad of mounting panel.

Preferably, a first opening matched with the wing body is formed in the right side of the fixed box, and the surface of the rotating rod is movably connected with the fixed box through a bearing.

Preferably, the bottom of adjusting the shell fixedly connected with slider, the spout that uses with the slider cooperation is seted up to the bottom of control shell inner chamber.

Preferably, a threaded hole matched with the screw rod is formed in the right side of the control shell, and a second opening matched with the ejector rod is formed in the bottom of the fixed box.

Preferably, the front side of fixed box is provided with the access panel, and the top and the bottom of access panel front side all are provided with the bolt, and the rear side of bolt runs through the access panel and with fixed box threaded connection.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the wing convenient to install, the unmanned aerial vehicle has the advantages of being stable and stable in fixation, preventing loosening, and being worthy of popularization.

2. According to the wing fixing box, the sliding rod and the sliding sleeve are arranged, the fixing rod can be conveniently used, the positioning block is arranged, the wing body can be matched with the positioning groove to limit and fix, the knob is arranged, a user can conveniently rotate the rotating rod, the cam is arranged, the fixing rod and the positioning block can be matched with the rotating rod to control the use positions of the fixing rod and the positioning block, the screw rod is arranged, the adjusting shell can be controlled to use the positions, the ejector rod is arranged, the wing body can be matched with the adjusting shell to increase the installation stability, and the installation plate and the installation hole are arranged, so that the fixing box can be conveniently installed and fixed.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a front view of the structure of the present utility model;

fig. 3 is a side partial cross-sectional view of the mounting box of the present utility model.

In the figure: 1. a fixed box; 2. a slide bar; 3. a sliding sleeve; 4. a spring; 5. a wing body; 6. a mounting groove; 7. a positioning groove; 8. a fixed rod; 9. a positioning block; 10. a rotating rod; 11. a cam; 12. a knob; 13. a control housing; 14. a hand wheel; 15. a screw; 16. an adjustment housing; 17. a push rod; 18. a mounting plate; 19. a mounting hole; 20. a slide block; 21. and a sliding groove.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-3, an unmanned aerial vehicle wing convenient to install comprises a fixed box 1, a sliding rod 2 is fixedly connected between the top and the bottom of an inner cavity of the fixed box 1, a sliding sleeve 3 and a spring 4 are sleeved on the surface of the sliding rod 2 from top to bottom in sequence, a wing body 5 is arranged on the right side of the fixed box 1, a positioning groove 7 is arranged on the top of the inner cavity of the mounting groove 6, a fixed rod 8 is fixedly connected on the right side of the sliding sleeve 3, the right side of the fixed rod 8 penetrates into the inner cavity of the mounting groove 6, a positioning block 9 is arranged in the inner cavity of the positioning groove 7, the bottom of the positioning block 9 is fixedly connected with the fixed rod 8, a rotary rod 10 is movably connected on the top of the inner cavity of the fixed box 1, a cam 11 is sleeved on the surface of the rotary rod 10, the front side of the rotary rod 10 penetrates through the fixed box 1 and is fixedly connected with a knob 12, the bottom of the fixed box 1 is fixedly connected with a control shell 13, the right side of the control shell 13 is provided with a hand wheel 14, the left side of the hand wheel 14 is fixedly connected with a screw 15, the left side of the screw 15 penetrates through the control shell 13 and is movably connected with an adjusting shell 16, the inner cavity of the adjusting shell 16 is provided with a push rod 17, the top of the push rod 17 penetrates through the fixed box 1 and is fixedly connected with a fixed rod 8, the left side of the fixed box 1 is fixedly connected with a mounting plate 18, the top and the bottom of the left side of the mounting plate 18 are provided with mounting holes 19, the left side of the mounting plate 18 is fixedly connected with a protection pad, the right side of the fixed box 1 is provided with a first opening matched with the wing body 5, the surface of the rotating rod 10 is movably connected with the fixed box 1 through a bearing, the bottom of the adjusting shell 16 is fixedly connected with a sliding block 20, the bottom of the inner cavity of the control shell 13 is provided with a sliding groove 21 matched with the sliding block 20, the screw hole that uses with the cooperation of screw rod 15 has been seted up on the right side of control shell 13, the second opening that uses with the cooperation of ejector pin 17 has been seted up to the bottom of fixed box 1, the front side of fixed box 1 is provided with the access panel, the top and the bottom of access panel front side all are provided with the bolt, the rear side of bolt runs through the access panel and with fixed box 1 threaded connection, through setting up slide bar 2 and sliding sleeve 3, can make things convenient for the use of dead lever 8, through setting up locating piece 9, can carry out spacing fixed to wing body 5 with the constant head tank 7 cooperation, through setting up knob 12, can the person of facilitating the use rotates rotary rod 10, through setting up cam 11, can control the service position of dead lever 8 and locating piece 9 with rotary rod 10 cooperation, through setting up screw rod 15, can control the service position of adjusting shell 16, through setting up ejector pin 17, can increase the steadiness of wing body 5 installation with adjusting shell 16 cooperation, through setting up mounting panel 18 and mounting hole 19, can make things convenient for the installation of fixed box 1, through setting up mounting groove 6, the constant head tank 7,

dead lever

8, 9, cam 12, knob 12, control shell 13, the unmanned aerial vehicle has been realized, the problem is solved, the unmanned aerial vehicle is realized, the unmanned aerial vehicle has been realized, and is easy to take off, the problem is realized, and is easy to be fixed, and is easy to be realized.

When the wing body fixing box is used, the knob 12 is rotated, the knob 12 and the rotary rod 10 are matched to drive the cam 11 to rotate, the cam 11 rotates to extrude the fixing rod 8, the fixing rod 8 moves to drive the sliding sleeve 3 to extrude the spring 4, the wing body 5 is inserted into the inner cavity of the fixing box 1, meanwhile, the fixing rod 8 and the positioning block 9 enter the inner cavity of the mounting groove 6, the spring 4 is reset after the knob 12 is loosened, the positioning block 9 enters the inner cavity of the positioning groove 7, then the hand wheel 14 is rotated, the hand wheel 14 and the screw 15 are matched to drive the adjusting shell 16 to move, the adjusting shell 16 moves to extrude the ejector rod 17, the ejector rod 17 is propped against the fixing rod 8, the fixing rod 8 and the positioning block 9 are prevented from being displaced, and the wing body 5 is prevented from loosening in the use process.

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

Claims

1. The utility model provides an unmanned aerial vehicle wing convenient to installation, includes fixed box (1), its characterized in that: a sliding rod (2) is fixedly connected between the top and the bottom of the inner cavity of the fixed box (1), a sliding sleeve (3) and a spring (4) are sequentially sleeved on the surface of the sliding rod (2) from top to bottom, a wing body (5) is arranged on the right side of the fixed box (1), a mounting groove (6) is formed in the left side of the wing body (5) and penetrates into the inner cavity of the fixed box (1), a positioning groove (7) is formed in the top of the inner cavity of the mounting groove (6), a fixing rod (8) is fixedly connected on the right side of the sliding sleeve (3), the right side of the fixing rod (8) penetrates into the inner cavity of the mounting groove (6), the inner cavity of the positioning groove (7) is provided with a positioning block (9), the bottom of the positioning block (9) is fixedly connected with a fixed rod (8), the top of the rear side of the inner cavity of the fixed box (1) is movably connected with a rotary rod (10), the surface of the rotary rod (10) is sleeved with a cam (11), the front side of the rotary rod (10) penetrates through the fixed box (1) and is fixedly connected with a knob (12), the bottom of the fixed box (1) is fixedly connected with a control shell (13), the right side of the control shell (13) is provided with a hand wheel (14), the left side of the hand wheel (14) is fixedly connected with a screw rod (15), the left side of screw rod (15) runs through control shell (13) and swing joint has regulation shell (16), the inner chamber of regulation shell (16) is provided with ejector pin (17), the top of ejector pin (17) runs through fixed box (1) and with dead lever (8) fixed connection.

2. The wing of claim 1, wherein the wing is configured for ease of installation by a unmanned aerial vehicle, wherein: the left side fixedly connected with mounting panel (18) of fixed box (1), mounting hole (19) have all been seted up at the top and the bottom of mounting panel (18) left side, the left side fixedly connected with protection pad of mounting panel (18).

3. The wing of claim 1, wherein the wing is configured for ease of installation by a unmanned aerial vehicle, wherein: the right side of the fixed box (1) is provided with a first opening matched with the wing body (5), and the surface of the rotating rod (10) is movably connected with the fixed box (1) through a bearing.

4. The wing of claim 1, wherein the wing is configured for ease of installation by a unmanned aerial vehicle, wherein: the bottom of the adjusting shell (16) is fixedly connected with a sliding block (20), and a sliding groove (21) matched with the sliding block (20) for use is formed in the bottom of the inner cavity of the control shell (13).

5. The wing of claim 1, wherein the wing is configured for ease of installation by a unmanned aerial vehicle, wherein: the right side of the control shell (13) is provided with a threaded hole matched with the screw rod (15), and the bottom of the fixed box (1) is provided with a second opening matched with the ejector rod (17).

6. The wing of claim 1, wherein the wing is configured for ease of installation by a unmanned aerial vehicle, wherein: the front side of fixed box (1) is provided with the access panel, and the top and the bottom of access panel front side all are provided with the bolt, and the rear side of bolt runs through the access panel and with fixed box (1) threaded connection.