CN209910506U

CN209910506U - Launching cradle

Info

Publication number: CN209910506U
Application number: CN201920528178.1U
Authority: CN
Inventors: 范琪伟; 何洋扬; 荣英佼; 童鹤; 岳权
Original assignee: Yong Zhuo Defense Technology Co Ltd
Current assignee: Yong Zhuo Defense Technology Co Ltd
Priority date: 2019-04-18
Filing date: 2019-04-18
Publication date: 2020-01-07
Anticipated expiration: 2029-04-18

Abstract

The utility model discloses a launcher, take frame, oriented board, frame, left side board, right side board, dog, oriented seat, oriented rod, recess strip, head, primary shaft, support platform, angle control pole, secondary shaft, angle control groove, oblique side pipe, adjustment pad, square steel pipe and sleeve pipe including base frame, explosion, base frame's inner chamber is provided with the explosion and takes the frame, the left front end of base frame and rear end all set up and have connect angle control pole, angle control pole's top is provided with the support platform, the top threaded connection of support platform has the support. The utility model discloses a base frame, explosion area frame, oriented board, frame, left side board, right side board, dog, oriented seat, oriented rod, recess strip, head, primary shaft, support platform, angle control pole, secondary shaft, angle control groove, oblique side pipe, adjustment pad, square steel pipe and sheathed tube cooperation have solved the unstable problem of rocket blasting ware launcher security.

Description

Launching cradle

Technical Field

The utility model relates to an ammunition fuze technical field specifically is a launching cradle.

Background

The rocket is a carrier for realizing space flight, the rocket has many kinds, the original rocket is an arrow which is attached to the head of a bow and an igniter by an igniter and then is fired when being jetted to enemies, the rocket is only used for releasing smoke and fire in the past year, the modern rocket is jetted backwards at high speed by hot air flow, and the jet propulsion device which moves forwards by utilizing the generated reaction force carries a combustion agent and an oxidant, does not depend on oxygen in air for combustion supporting, can fly in the atmosphere and in outer space, can be used as a rapid and long-distance transport tool and can be used for launching satellites and delivering weapons to the warhead, the rocket projectile launcher is a device for hanging and launching rocket projectiles, and the rocket blaster is a vehicle-mounted rocket blaster, so that the problem of unstable safety of the rocket blaster launcher exists.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a launcher possesses safety and stability's advantage, has solved the unstable problem of rocket blasting ware launcher security.

In order to achieve the above object, the utility model provides a following technical scheme: a launcher comprises a base frame, an explosion belt frame, a directional plate, a frame, a left side plate, a right side plate, a stop block, a directional seat, a directional rod, a groove strip, a seal head, a first shaft, a support table, an angle control rod, a second shaft, an angle control groove, an inclined square tube, an adjusting pad, a square steel tube and a sleeve, wherein the explosion belt frame is arranged in an inner cavity of the base frame, the angle control rod is arranged at the front end and the rear end of the left side of the base frame, the support table is arranged at the top of the angle control rod, the support is in threaded connection with the top of the support, the top of the support is movably connected with the directional plate through the first shaft, the frame is fixedly connected with the bottom of the directional plate, the left side plate and the right side plate are respectively arranged at the rear end and the front end of the bottom of the directional plate, the directional rod is arranged at the, one end of the orientation rod is provided with a seal head, and the top of the orientation plate is provided with a stop block and a base frame.

Preferably, the surface of the angle control rod is connected with the frame through an angle control groove, and the angle control groove is movably connected with the frame through a second shaft.

Preferably, a square steel pipe is fixedly connected between the angle control rods.

Preferably, a sleeve is arranged on the left side of the top of the orientation plate.

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

the utility model discloses a set up base frame, explosion area frame, oriented board, frame, left side board, right side board, dog, oriented seat, oriented rod, recess strip, head, primary shaft, support, supporting seat platform, angle control pole, secondary shaft, angle control groove, oblique side pipe, adjustment pad, square steel pipe and sheathed tube cooperation, played and drawn into a rectilinear state with the explosion area, the effect of explosion area explosion under the fuse effect at last has improved the security, the unstable problem of rocket blasting ware launcher security has been solved.

Drawings

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

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

FIG. 3 is a schematic diagram of the left side plate structure of the present invention;

FIG. 4 is a schematic view of the stopper structure of the present invention;

fig. 5 is a schematic view of the square steel tube structure of the present invention.

In the figure: the device comprises a base frame 1, an explosive zone frame 2, an orientation plate 3, a frame 4, a left side plate 5, a right side plate 6, a stop 7, an orientation seat 8, an orientation rod 9, a groove strip 10, a seal head 11, a first shaft 12, a support 13, a support table 14, an angle control rod 15, a second shaft 16, an angle control groove 17, an oblique square tube 18, an adjusting pad 19, a square steel tube 20 and a sleeve 21.

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. 1-5, a launcher comprises a base frame 1, an explosive zone frame 2, an orientation plate 3, a frame 4, a left side plate 5, a right side plate 6, a stopper 7, an orientation seat 8, an orientation rod 9, a groove strip 10, a head 11, a first shaft 12, a support 13, a support table 14, an angle control rod 15, a second shaft 16, an angle control groove 17, an oblique square pipe 18, an adjustment pad 19, a square steel pipe 20 and a sleeve 21, wherein the explosive zone frame 2 is arranged in an inner cavity of the base frame 1, the angle control rod 15 is arranged at both the front end and the rear end of the left side of the base frame 1, the surface of the angle control rod 15 is connected with the frame 4 through the angle control groove 17, the angle control groove 17 is movably connected with the frame 4 through the second shaft 16, the square steel pipe 20 is fixedly connected between the angle control rods 15, the support table 14 is arranged at the top of the angle control rod 15, the support table 13 is in, the top of the support 13 is movably connected with the orientation plate 3 through a first shaft 12, the left side of the top of the orientation plate 3 is provided with a sleeve 21, the bottom of the orientation plate 3 is fixedly connected with a frame 4, the rear end and the front end of the bottom of the orientation plate 3 are respectively provided with a left side plate 5 and a right side plate 6, the bottom of the frame 4 is provided with an orientation rod 9, the bottom of the orientation plate 3 is provided with an orientation seat 8, one end of the orientation rod 9 is provided with a seal head 11, the top of the orientation plate 3 is provided with a stop 7 and a base frame 1, and the cooperation of the base frame 1, the explosion belt frame 2, the orientation plate 3, the frame 4, the left side plate 5, the right side plate 6, the stop 7, the orientation seat 8, the orientation rod 9, a groove strip 10, the seal head 11, the first shaft 12, the support 13, a support platform 14, an angle control rod 15, a second shaft 16, an angle control groove 17, an inclined square pipe 18, and finally, the effect of explosion under the action of the fuse is achieved, so that the safety is improved, and the problem of unstable safety of the launcher of the rocket blaster is solved.

When the rocket launcher is used, firstly, the explosive zones, namely, the warheads, are orderly arranged in the explosive zone frame 2, then rocket projectiles are loaded into the launcher which consists of the parts such as the directional seat 8, the directional rod 9, the left side plate 5, the right side plate 6, the stop dog 7, the groove strips 10 and the like, the launching angle is adjusted through the angle control rod 15 and the angle control groove 17, the rocket is ignited through the ignition device, the rocket engine stably flies out of the launcher under the guidance of the directional seat 8, the directional rod 9 and the groove strips 10 at a fixed angle and direction, then the explosive zones are pulled to fly forwards by the projectile tail structure, the explosive zones are pulled to be in a linear state, finally, the explosive zones explode under the fuse effect, and the problem of unstable safety of the rocket launcher of the blasting device is solved.

In summary, the following steps: the launcher solves the problem of unstable safety of the rocket launcher through the cooperation of a base frame 1, an explosion belt frame 2, an orientation plate 3, a frame 4, a left side plate 5, a right side plate 6, a stop dog 7, an orientation seat 8, an orientation rod 9, a groove strip 10, a seal head 11, a first shaft 12, a support 13, a support table 14, an angle control rod 15, a second shaft 16, an angle control groove 17, an inclined square pipe 18, an adjusting pad 19, a square steel pipe 20 and a sleeve 21.

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 launcher, includes base frame (1), explosion area frame (2), directional board (3), frame (4), left side board (5), right side board (6), dog (7), directional seat (8), directional pole (9), recess strip (10), head (11), primary shaft (12), support (13), support platform (14), angle control pole (15), secondary shaft (16), angle control groove (17), oblique side pipe (18), adjustment pad (19), square steel pipe (20) and sleeve pipe (21), its characterized in that: an explosion belt frame (2) is arranged in the inner cavity of the base frame (1), angle control rods (15) are respectively arranged at the front end and the rear end of the left side of the base frame (1), a support base (14) is arranged at the top of the angle control rod (15), a support base (13) is connected with the top of the support base (14) in a threaded manner, the top of the support (13) is movably connected with the orientation plate (3) through a first shaft (12), the bottom of the directional plate (3) is fixedly connected with a frame (4), the rear end and the front end of the bottom of the directional plate (3) are respectively provided with a left side plate (5) and a right side plate (6), the bottom of the frame (4) is provided with an orientation rod (9), the bottom of the orientation plate (3) is provided with an orientation seat (8), one end of the orientation rod (9) is provided with a seal head (11), and the top of the orientation plate (3) is provided with a stop block (7) and a base frame (1).

2. A launcher according to claim 1, wherein: the surface of the angle control rod (15) is connected with the frame (4) through an angle control groove (17), and the angle control groove (17) is movably connected with the frame (4) through a second shaft (16).

3. A launcher according to claim 1, wherein: and a square steel pipe (20) is fixedly connected between the angle control rods (15).

4. A launcher according to claim 1, wherein: the left side of the top of the orientation plate (3) is provided with a sleeve (21).