CN211391738U - Unmanned aerial vehicle aircraft signal transmitter - Google Patents

Abstract

The utility model discloses an unmanned aerial vehicle aircraft signal transmitter, including main part and slider, the control handle groove has been seted up to the top both sides of main part, and the bottom that the main part is close to the control handle groove is provided with the control rod, and the top of control rod is connected with the connecting rod. This unmanned aerial vehicle aircraft signal transmitter, the control handle drives the connecting rod and rotates, make the connecting rod produce relative movement with the control rod, the control rod drives the inside that the slide bar shifted out the draw-in groove, make the slide bar get into the inside of slide tray, the spring drives connecting rod and control handle rebound, make the control handle shift out the inside in control handle groove, the control handle uses the completion back, press the control handle, make the control rod drive the one side that the slide bar moved the draw-in groove, spring compression, later rotate the control handle, make the control handle produce relative rotation with the control rod, make the control rod drive the inside that the slide bar got into the draw-in groove, be convenient for with the inside in control handle indentation control handle groove, be convenient for accomodate.

Description

Unmanned aerial vehicle aircraft signal transmitter

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle aircraft signal transmitter.

Background

The aircraft is also called a rotor aircraft and a rotor helicopter, is a multi-rotor aircraft, and when the aircraft is used, a user needs to control the unmanned aerial vehicle through a signal transmitter. Although the types and the number of the existing aircraft signal transmitters are very large, the existing aircraft signal transmitters still have certain problems, and certain inconvenience is brought to the use of the aircraft signal transmitters.

The existing aircraft signal transmitter is mainly used for controlling the aircraft through the control handle, but the control handle is highly fixed, so that the control handle is inconvenient to store and use, and therefore the technology capable of improving the structure of the aircraft signal transmitter is urgently needed to perfect the device.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle aircraft signal transmitter to solve present aircraft signal transmitter that above-mentioned background art provided and when using, control the aircraft mostly through the handle, but the handle highly fixed, inconvenient accomodating the handle, the problem of inconvenient use.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle aircraft signal transmitter comprises a main body and a sliding block, wherein control handle grooves are formed in two sides of the top of the main body, control levers are arranged at the bottoms of the main body, close to the control handle grooves, and the tops of the control levers are connected with connecting rods; the top of the connecting rod is fixedly provided with an operating handle, one side of the connecting rod, which is close to the operating rod, is provided with a connecting groove, two sides of the connecting rod, which are close to the connecting groove, are provided with sliding grooves, one side of the connecting rod, which is close to the top of the sliding grooves, is provided with a clamping groove, and a spring is fixed between the top of the operating rod and the; one side that the control rod is close to the draw-in groove is fixed with the slide bar, and the top that the main part is close to the control rod is provided with the dust guard, and the spout has been seted up to the both sides that the main part is close to the dust guard, and the slider is fixed in one side that the dust guard is close to the spout, and the bottom of slider is seted up flutedly, and one side that the main part is close to the.

Preferably, the connecting rod is elastically connected with the operating rod through a spring, and the outer diameter of the operating rod is matched with the inner diameter of the connecting groove.

Preferably, the sliding rod is a cylinder, the outer diameter of the sliding rod is matched with the height of the clamping groove, and the sliding rod and the clamping groove form a clamping structure.

Preferably, the sliding groove and the sliding block are T-shaped, the inner size of the sliding groove is matched with the outer size of the sliding block, and the sliding groove and the sliding block form a sliding structure.

Preferably, the cross section of the bump is an arc-shaped elastic sheet, and the external dimension of the bump is matched with the internal dimension of the groove.

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

beneficial effect 1 this unmanned aerial vehicle aircraft signal transmitter, the control handle drives the connecting rod and rotates, make the connecting rod produce relative movement with the control rod, the control rod drives the inside that the slide bar shifted out the draw-in groove, make the slide bar get into the inside of slide tray, the spring drives connecting rod and control handle rebound, make the control handle shift out the inside in control handle groove, the control handle uses the back of accomplishing, press the control handle, make the control rod drive the one side that the slide bar moved the draw-in groove, the spring compression, later rotate the control handle, make control handle and control rod produce relative rotation, make the control rod drive the inside that the slide bar got into the draw-in groove, be convenient for with the inside in control handle indentation control handle groove, be convenient for accomodate the.

Beneficial effect 2 this unmanned aerial vehicle aircraft signal transmitter, the dust guard drives the slider and removes in the inside of spout, makes the slider support the lug, makes lug compression deformation, and when the dust guard is closed completely, the lug just aligns with the recess, and the lug resumes the shape and supports the recess, avoids the dust guard to remove easily, is convenient for fix the dust guard, is convenient for prevent dust to the operating panel of main part through the dust guard.

Beneficial effect 3 this unmanned aerial vehicle aircraft signal transmitter, when removing the dust guard, the dust guard moves the slider and slides in the inside of spout, through the sliding structure that spout and slider constitute, is convenient for lead the removal of dust guard, avoids the removal of dust guard to produce the skew.

Drawings

Fig. 1 is a schematic top view of the present invention;

FIG. 2 is a schematic side view of the present invention;

FIG. 3 is a schematic view of a partial enlarged structure at A in FIG. 2 according to the present invention;

fig. 4 is a schematic view of the connection structure of the operating rod of the present invention.

In the figure: 1. a main body; 2. a lever groove; 3. a joystick; 4. a connecting rod; 5. a control handle; 6. connecting grooves; 7. a sliding groove; 8. a card slot; 9. a spring; 10. a slide bar; 11. a dust-proof plate; 12. a chute; 13. a slider; 14. a groove; 15. and (4) a bump.

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.

Referring to fig. 1-4, an unmanned aerial vehicle signal transmitter includes a main body 1, a lever groove 2, a lever 3, a connecting rod 4, a lever 5, a connecting groove 6, a sliding groove 7, a slot 8, a spring 9, a sliding rod 10, a dust guard 11, a sliding groove 12, a sliding block 13, a groove 14, and a protrusion 15.

Handle groove 2 has been seted up to the top both sides of main part 1, main part 1 is provided with control rod 3 near the bottom in handle groove 2, the top of control rod 3 is connected with connecting rod 4, connecting rod 4 passes through spring 9 and constitutes elastic connection with control rod 3, and the external diameter of control rod 3 is identical with the internal diameter of spread groove 6, when rotating control handle 5, control handle 5 drives connecting rod 4 and rotates, make connecting rod 4 and control rod 3 produce relative movement, control rod 3 drives the inside that slide bar 10 shifted out draw-in groove 8, make slide bar 10 get into the inside of slide groove 7, spring 9 drives connecting rod 4 and control handle 5 and upwards removes, make control handle 5 shift out the inside in handle groove 2, drive control rod 3 through control handle 5 and remove, control the unmanned aerial vehicle aircraft.

The top of connecting rod 4 is fixed with handle 5, and connecting rod 4 has seted up spread groove 6 near one side of control lever 3, and connecting rod 4 has seted up sliding tray 7 near the both sides of spread groove 6, and connecting rod 4 has seted up draw-in groove 8 near top one side of sliding tray 7, is fixed with spring 9 between 3 tops of control lever and the 6 tops of spread groove.

A sliding rod 10 is fixed on one side of the operating rod 3 close to the clamping groove 8, the sliding rod 10 is a cylinder, the outer diameter of the sliding rod 10 is matched with the height of the clamping groove 8, the sliding rod 10 and the clamping groove 8 form a clamping structure, after the operating handle 5 is used, the operating handle 5 is pressed, the operating rod 3 drives the sliding rod 10 to move to one side of the clamping groove 8, the spring 9 is compressed, then the operating handle 5 is rotated, the operating handle 5 and the operating rod 3 rotate relatively, the operating rod 3 drives the sliding rod 10 to enter the clamping groove 8, the operating handle 5 is conveniently retracted into the operating handle groove 2, the operating handle 5 is fixed inside the operating handle groove 2, a dustproof plate 11 is arranged on the top of the main body 1 close to the operating rod 3, sliding grooves 12 are formed on two sides of the main body 1 close to the dustproof plate 11, the sliding grooves 12 and the sliding blocks 13 are in a T shape, and the inner size of the, and the chute 12 and the slide block 13 form a sliding structure, when moving the dust guard 11, the dust guard 11 drives the slide block 13 to slide in the chute 12, the sliding structure formed by the chute 12 and the slide block 13 is convenient to guide the movement of the dust guard 11, and the movement of the dust guard 11 is prevented from being deviated, the slide block 13 is fixed on one side of the dust guard 11 close to the chute 12, the bottom of the slide block 13 is provided with a groove 14, one side of the main body 1 close to the groove 14 is fixed with a bump 15, the cross section of the bump 15 is an arc-shaped elastic sheet, and the external dimension of the bump 15 is matched with the internal dimension of the groove 14, when the dust guard 11 is closed and covers the control handle groove 2, the dust guard 11 drives the slide block 13 to move in the chute 12, so that the slide block 13 abuts against the bump 15, the bump 15 is compressed and deformed, when the dust guard 11 is completely closed, the bump 15 is exactly, the dust guard 11 is prevented from being easily moved, and the dust guard 11 is conveniently fixed.

When the signal transmitter of the unmanned aerial vehicle is used, firstly, when the signal transmitter is used, the dust guard 11 is moved to expose the control handle 5, the control handle 5 is rotated to drive the connecting rod 4 to rotate, so that the connecting rod 4 and the control rod 3 generate relative movement, the control rod 3 drives the sliding rod 10 to move out of the inside of the clamping groove 8, so that the sliding rod 10 enters the inside of the sliding groove 7, the spring 9 drives the connecting rod 4 and the control handle 5 to move upwards, so that the control handle 5 moves out of the inside of the control handle groove 2, the control rod 3 is driven by the control handle 5 to move, the unmanned aerial vehicle is controlled, after the use is finished, the control handle 5 is pressed, so that the control rod 3 drives the sliding rod 10 to move to one side of the clamping groove 8, the spring 9 is compressed, then the control handle 5 is rotated to enable the control handle 5 and the control rod 3 to generate relative rotation, so, the operation handle 5 is retracted into the operation handle groove 2, the operation handle 5 is fixed in the operation handle groove 2, then the dust guard 11 drives the sliding block 13 to move in the sliding groove 12, the sliding block 13 is abutted against the convex block 15, the convex block 15 is compressed and deformed, when the dust guard 11 is completely closed, the convex block 15 is exactly aligned with the groove 14, the convex block 15 is restored to be in the shape to abut against the groove 14, the dust guard 11 is prevented from easily moving, the dust guard 11 is convenient to fix, and the operation panel of the main body 1 is prevented from dust through the dust guard 11.

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 invention.

Claims (5)

1. An unmanned aerial vehicle aircraft signal transmitter, includes main part (1) and slider (13), its characterized in that: control handle grooves (2) are formed in two sides of the top of the main body (1), a control rod (3) is arranged at the bottom, close to the control handle grooves (2), of the main body (1), and the top of the control rod (3) is connected with a connecting rod (4);

a control handle (5) is fixed at the top of the connecting rod (4), a connecting groove (6) is formed in one side, close to the control lever (3), of the connecting rod (4), sliding grooves (7) are formed in two sides, close to the connecting groove (6), of the connecting rod (4), a clamping groove (8) is formed in one side, close to the top of the sliding grooves (7), of the connecting rod (4), and a spring (9) is fixed between the top of the control lever (3) and the top of the connecting groove (6);

one side of the operating rod (3) close to the clamping groove (8) is fixed with a sliding rod (10), the top of the main body (1) close to the operating rod (3) is provided with a dustproof plate (11), the two sides of the main body (1) close to the dustproof plate (11) are provided with sliding grooves (12), the sliding block (13) is fixed on one side of the dustproof plate (11) close to the sliding grooves (12), the bottom of the sliding block (13) is provided with a groove (14), and one side of the main body (1) close to the groove (14) is fixed with a convex block (15).

2. A drone aircraft signal transmitter in accordance with claim 1, characterized in that: the connecting rod (4) is elastically connected with the operating rod (3) through a spring (9), and the outer diameter of the operating rod (3) is matched with the inner diameter of the connecting groove (6).

3. A drone aircraft signal transmitter in accordance with claim 1, characterized in that: the sliding rod (10) is a cylinder, the outer diameter of the sliding rod (10) is matched with the height of the clamping groove (8), and the sliding rod (10) and the clamping groove (8) form a clamping structure.

4. A drone aircraft signal transmitter in accordance with claim 1, characterized in that: the sliding chute (12) and the sliding block (13) are T-shaped, the inner size of the sliding chute (12) is matched with the outer size of the sliding block (13), and the sliding chute (12) and the sliding block (13) form a sliding structure.

5. A drone aircraft signal transmitter in accordance with claim 1, characterized in that: the section of the convex block (15) is an arc-shaped elastic sheet, and the external dimension of the convex block (15) is matched with the internal dimension of the groove (14).

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