CN217649646U

CN217649646U - Miniature guided missile emitter suitable for unmanned aerial vehicle transmission

Info

Publication number: CN217649646U
Application number: CN202222121271.5U
Authority: CN
Inventors: 闫兆; 樊江川
Original assignee: Beijing Weitong Xinke Measurement And Control Technology Co ltd
Current assignee: Beijing Weitong Xinke Measurement And Control Technology Co ltd
Priority date: 2022-08-12
Filing date: 2022-08-12
Publication date: 2022-10-25
Anticipated expiration: 2032-08-12

Abstract

The utility model discloses a miniature missile emitter suitable for unmanned aerial vehicle transmission, including the crossbearer, two erect the frame and set up the launch canister in the crossbearer both sides, the inboard of launch canister is equipped with T type slide bar, set up on the both sides wall of crossbearer with T type slide bar assorted spout, T type slide bar injects in the spout, the end of spout is equipped with the guide bar, the slip cover is equipped with the roof on the other end, be connected through the spring between the terminal inner wall of roof and spout, the jack that is used for depositing the guide bar body is offered to the end of T type slide bar, the thread groove has been seted up on the other end of T type slide bar, locking screw hole has been seted up to crossbearer both sides tip, T type slide bar passes through locking behind set screw threaded connection screw hole and the thread groove in the spout. The utility model discloses a T type slide bar extrusion spring makes T type slide bar receive reverse effort to utilize set screw to lock the other end of T type slide bar in the spout, increase the fastness of the installation of launching tube, avoid the launching tube to drop.

Description

Miniature missile launcher suitable for unmanned aerial vehicle transmission

Technical Field

The utility model relates to a guided missile emitter technical field especially relates to a miniature guided missile emitter suitable for unmanned aerial vehicle transmission.

Background

Along with the continuous development of unmanned aerial vehicle technique, especially the continuous maturity of unmanned aerial vehicle technique, unmanned aerial vehicle carries ammunition and fights, becomes a mode of fighting that is more and more popular at present in recent years. The micro missile is particularly suitable for the small unmanned aerial vehicle combat mode due to light weight, small size and high hitting precision. In the past, large airplanes or large unmanned planes are all matched with corresponding weapon launching devices, and the launching devices are complex in structure, large in occupied space and heavy in weight. Small-size unmanned aerial vehicle is because its load weight and volume are limited, need a simple structure, small, light in weight's emitter, for example, the patent number is "202123171903.0", the patent name is "a current patent that is applicable to the miniature guided missile transmission dress of unmanned aerial vehicle transmission", but this type of emitter still has the shortcoming, for example, the launching tube is only through the bolt fastening on the link, such fixed mode leads to becoming flexible by some external factors influence very easily, very easily cause the incident, consequently, need a launching tube to connect firm emitter, avoid the launching tube to drop and cause the incident.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a miniature guided missile emitter suitable for unmanned aerial vehicle transmission solves foretell problem.

In order to solve the technical problem, the utility model adopts the following technical scheme:

the utility model relates to a miniature missile emitter suitable for unmanned aerial vehicle transmission, including crossbearer and two perpendicular framves, the bottom of erecting the frame is connected on the crossbearer, the top of erecting the frame is connected on unmanned aerial vehicle, the both sides of crossbearer are equipped with the launching tube, be equipped with the guided missile that can launch in the launching tube, the inboard of launching tube is equipped with T type slide bar, seted up on the both sides wall of crossbearer with T type slide bar assorted spout, T type slide bar injects in the spout, the end of spout is equipped with the guide bar, the one end of guide bar is fixed the inside of spout, the slip cap is equipped with the roof on the other end, the roof with be connected through the spring between the terminal inner wall of spout, the end of T type slide bar is offered and is used for depositing the jack of guide bar body, set up the thread groove on the other end of T type slide bar, the locking screw hole has been seted up to crossbearer both sides tip, the T type slide bar passes through locking behind set screw threaded connection screw hole and the thread groove in the spout.

Furthermore, the transverse frame and the vertical frame are integrally formed.

Further, the mounting hole has been seted up at the top of erecting the frame, erect the frame and pass through the bolt mounting hole threaded connection is in on the unmanned aerial vehicle.

Furthermore, a side supporting plate is connected between the two vertical frames.

Furthermore, a reinforcing triangular iron is arranged at the joint of the transverse frame and the vertical frame.

Compared with the prior art, the utility model discloses a beneficial technological effect:

the utility model discloses a T type slide bar extrusion spring makes T type slide bar receive reverse effort to utilize set screw to lock the other end of T type slide bar in the spout, increase the fastness of the installation of launching tube, avoid the launching tube to drop.

Drawings

The present invention will be further explained with reference to the accompanying drawings.

Fig. 1 is a front view of the micro missile launcher of the utility model suitable for launching unmanned aerial vehicles;

FIG. 2 is a side view of the micro missile launcher for launching by unmanned aerial vehicles of the present invention;

FIG. 3 is a cross-sectional side view;

description of reference numerals: 1. a transverse frame; 2. erecting; 3. a launch canister; 4. a T-shaped slide bar; 5. a chute; 6. a guide bar; 7. a top plate; 8. a spring; 9. a jack; 10. a thread groove; 11. locking the threaded hole; 12. mounting holes; 13. and a support plate.

Detailed Description

In order to make the technical problem, technical solution and beneficial effects to be solved by the present invention more clearly understood, the following description is made in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention. It should be noted that the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise. The meaning of "a number" is one or more unless specifically limited otherwise.

In the description of the present invention, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", and the like indicate orientations or positional relationships based on orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.

As shown in figures 1-3, a miniature missile launcher suitable for unmanned aerial vehicle transmission, includes crossbearer 1 and two perpendicular framves 2, the bottom of perpendicular frame 2 is connected on the crossbearer 1, crossbearer 1 and perpendicular frame 2 are integrated into one piece, the junction of crossbearer 1 and perpendicular frame 2 is equipped with the enhancement angle iron.

A side supporting plate 13 is connected between the two vertical frames 2 to strengthen the firmness.

The top of erecting frame 2 has seted up mounting hole 12, erect frame 2 and pass through the bolt mounting hole 12 threaded connection be in on the unmanned aerial vehicle.

Launching tubes 3 are arranged on two sides of the transverse frame 1, and missiles capable of being launched are arranged in the launching tubes 3.

The launching barrel is characterized in that a T-shaped sliding rod 4 is arranged on the inner side of the launching barrel 3, sliding grooves 5 matched with the T-shaped sliding rod 4 are formed in two side walls of the cross frame 1, the T-shaped sliding rod 4 is inserted into the sliding grooves 5, guide rods 6 are arranged at the tail ends of the sliding grooves 5, one ends of the guide rods 6 are fixed inside the sliding grooves 5, a top plate 7 is sleeved at the other ends of the guide rods 6 in a sliding mode, the top plate 7 is connected with the inner walls of the tail ends of the sliding grooves 5 through springs 8, inserting holes 9 used for storing rod bodies of the guide rods 6 are formed in the tail ends of the T-shaped sliding rods 4, threaded grooves 10 are formed in the other ends of the T-shaped sliding rods 4, locking threaded holes 11 are formed in the end portions of two sides of the cross frame 1, and the T-shaped sliding rods 4 are locked in the sliding grooves 5 after being connected with the threaded holes 11 and the threaded grooves 10 through positioning screws.

When the launching tube 3 is installed, the T-shaped sliding rod 4 is inserted into the sliding groove 5, the tail end of the T-shaped sliding rod 4 is fixed on the top plate 7, then the T-shaped sliding rod 4 is pressed forcibly, the spring 8 is compressed to the maximum degree, at the moment, the thread groove 10 and the locking threaded hole 11 are located in the same axis, then the T-shaped sliding rod 4 is fixed in the sliding groove 5 through the positioning screw, meanwhile, the top plate 7 is abutted against the T-shaped sliding rod 4, the acting force of the T-shaped sliding rod 4 on the positioning screw is increased, and firmness is enhanced.

The above-mentioned embodiments are only described in the preferred embodiments of the present invention, but not limited to the scope of the present invention, and various modifications and improvements made by the technical solutions of the present invention by those skilled in the art should fall within the protection scope defined by the claims of the present invention without departing from the design spirit of the present invention.

Claims

1. The utility model provides a miniature missile emitter suitable for unmanned aerial vehicle transmission, includes crossbearer (1) and two erects frame (2), the bottom of erecting frame (2) is connected on crossbearer (1), the top of erecting frame (2) is connected on unmanned aerial vehicle, the both sides of crossbearer (1) are equipped with launch canister (3), be equipped with the guided missile that can launch in launch canister (3), its characterized in that: the inboard of launching tube (3) is equipped with T type slide bar (4), seted up on the both sides wall of crossbearer (1) with T type slide bar (4) assorted spout (5), T type slide bar (4) inject in spout (5), the end of spout (5) is equipped with guide bar (6), the one end of guide bar (6) is fixed the inside of spout (5), the slip cover is equipped with roof (7) on the other end, roof (7) with be connected through spring (8) between the terminal inner wall of spout (5), the end of T type slide bar (4) is seted up and is used for depositing jack (9) of guide bar (6) pole body, thread groove (10) have been seted up on the other end of T type slide bar (4), locking screw hole (11) have been seted up to crossbearer (1) both sides tip, locking behind T type slide bar (4) through set screw threaded connection screw hole (11) and thread groove (10) is in spout (5).

2. The micro missile launcher suitable for launching by a drone of claim 1, wherein: the transverse frame (1) and the vertical frame (2) are integrally formed.

3. The micro missile launching device suitable for unmanned aerial vehicle launching as claimed in claim 1, wherein: the top of the vertical frame (2) is provided with a mounting hole (12), and the vertical frame (2) penetrates through the mounting hole (12) in a threaded manner to be connected to the unmanned aerial vehicle.

4. The micro missile launcher suitable for launching by a drone of claim 1, wherein: a side supporting plate (13) is connected between the two vertical frames (2).

5. The micro missile launching device suitable for unmanned aerial vehicle launching as claimed in claim 1, wherein: and reinforcing triangular irons are arranged at the joint of the transverse frame (1) and the vertical frame (2).