CN-224230845-U - Rocket positioning and launching system

CN224230845UCN 224230845 UCN224230845 UCN 224230845UCN-224230845-U

Abstract

The utility model provides a rocket positioning and launching system, which relates to the technical field of rocket transshipment positioning, so as to optimize the rocket positioning and launching system to a certain extent and improve positioning accuracy and positioning efficiency. The rocket positioning launching system comprises a launching vehicle, an rocket body, a first centering device and a second centering device, wherein a bearing space is formed in the launching vehicle and used for bearing the rocket body, the first centering device is located at one end of the bearing space, which faces to the headstock of the launching vehicle, and can emit straight light beams extending along the length direction of the bearing space, the second centering device is arranged at the tail of the rocket body, and the second centering device can emit straight light beams extending along the vertical direction.

Inventors

WANG XINJIANG
TIAN SHUO
Zong Wenshuo
WANG RAN
CHI JIACHENG
CAO LONG
LING SEN
WANG MING
FENG JUNLONG
GU JIAYOU
LI ZHENYU
YANG JINGYU
YAN BO

Assignees

中国人民解放军63601部队

Dates

Publication Date: 20260512
Application Date: 20250530

Claims (9)

1. The rocket positioning and launching system is characterized by comprising a launch vehicle, an rocket body, a first centering device and a second centering device; The launching vehicle is provided with a bearing space, the bearing space is used for bearing the arrow body, the first centering device is positioned at one end of the bearing space, which faces the head of the launching vehicle, and the first centering device can emit straight light beams which extend along the length direction of the bearing space; The second centering device is arranged at the tail part of the arrow body and can emit straight light beams extending along the vertical direction.
2. A rocket positioning and launching system according to claim 1, further comprising a docking device comprising a positioning mechanism and an alignment mechanism, said alignment mechanism being disposed on a side wall of said rocket body tail, said positioning mechanism being coupled to said launcher and disposed in correspondence of said alignment mechanism; The positioning mechanism is formed with a guide portion, the alignment mechanism is formed with a fitting portion, the guide portion extends in the vertical direction, and the fitting portion can be inserted into the guide portion and move in the guide portion.
3. A rocket positioning launch system according to claim 2 wherein said positioning mechanism comprises a positioning seat and a positioning plate; The positioning seat is connected with the launching vehicle, the positioning plate is arranged on the positioning seat along the vertical direction, the guide part is formed on the positioning plate, and one end of the guide part penetrates through the edge of the positioning plate to form an opening, so that the matching part can enter the guide part.
4. A rocket positioning launching system according to claim 2, wherein the number of alignment mechanisms is two, and the two alignment mechanisms are oppositely disposed on the side wall of the tail of the rocket body along the radial direction of the rocket body; the positioning mechanisms are arranged in one-to-one correspondence with the alignment mechanisms.
5. A rocket positioning and launching system according to claim 3, wherein said positioning seat comprises a seat body, a slide block and a first locking member, said seat body is connected with said launcher, and said seat body is formed with a slide track along the width direction of said launcher; the first locking piece penetrates through the sliding block and enters the slideway, so that the sliding block can slide along the slideway; the locating plate is connected with the sliding block.
6. A rocket positioning launch system according to claim 3 wherein said positioning mechanism further comprises a second locking member, said second locking member being connected to said launch vehicle through said positioning seat.
7. A rocket positioning launch system according to claim 2 wherein said alignment mechanism comprises a mount and an alignment post; the mounting seat is connected with the arrow body, the alignment column is connected with the mounting seat, and the axis of the alignment column extends along the radial direction of the arrow body.
8. A rocket positioning launch system according to claim 7 wherein said alignment posts comprise rolling portions of the posts, said posts being connected to said mounting blocks, said rolling portions being sleeved outside said posts and rotatable relative to said posts.
9. A rocket positioning launch system according to claim 2 wherein said first centering device comprises a first connection base and a first launcher and said second centering device comprises a second connection base and a second launcher; the first connecting seat is connected with the launching vehicle, the first emitter is arranged on the first connecting seat, and the first emitter can emit light beams extending along the length direction of the launching vehicle; The second connecting seat is connected with the arrow body, the second emitter is installed on the second connecting seat, and the second emitter can emit light beams which are emitted to the emitting vehicle along the vertical direction.

Description

Rocket positioning and launching system Technical Field The utility model relates to the technical field of rocket transferring and positioning, in particular to a rocket positioning and launching system. Background After the solid rocket is tested in a factory building in a technical area, the rocket body is required to be hoisted to a main beam of a launching vehicle for fixing so as to ensure the stability of the rocket body in the transportation process, and the work is called rocket loading and loading. And the rocket is transferred and loaded and the rocket body needs to be positioned rapidly, when the solid rocket is hoisted to the launching vehicle, the positioning device and the cooperative command mode are adopted to guide the rocket body and the launching vehicle locking device to position. At present, a positioning rod is mostly installed at the tail of a rocket, a positioning seat is installed at a corresponding position of the tail of a launching vehicle, the positioning rod is restrained by the positioning seat to guide rocket positioning, but the existing positioning rod is inserted and positioned by vertical lifting, so that the positioning rod is inconvenient to observe in the alignment process, and the problems of poor positioning precision, low positioning precision, complex operation, long time consumption and the like are caused. Therefore, there is an urgent need to provide a rocket positioning launching system and a positioning method, so as to solve the problems in the prior art to a certain extent. Disclosure of utility model The utility model aims to provide a rocket positioning and launching system and a rocket positioning method, so that the rocket positioning and launching system is optimized to a certain extent, and the positioning accuracy and the positioning efficiency are improved. The rocket positioning launching system comprises a launching vehicle, an rocket body, a first centering device and a second centering device, wherein a bearing space is formed in the launching vehicle and used for bearing the rocket body, the first centering device is located at one end of the bearing space, which faces the head of the launching vehicle, and can emit straight light beams extending along the length direction of the bearing space, the second centering device is arranged at the tail of the rocket body, and the second centering device can emit straight light beams extending along the vertical direction. The rocket positioning and launching system further comprises a docking device, wherein the docking device comprises a positioning mechanism and an alignment mechanism, the alignment mechanism is arranged on the side wall of the tail of the rocket body, the positioning mechanism is connected with the launching vehicle and is arranged corresponding to the alignment mechanism, the positioning mechanism is provided with a guide part, the alignment mechanism is provided with a matching part, the guide part extends along the vertical direction, and the matching part can be inserted into the guide part and move in the guide part. The positioning mechanism comprises a positioning seat and a positioning plate, wherein the positioning seat is connected with the launching vehicle, the positioning plate is arranged on the positioning seat along the vertical direction, the guide part is formed on the positioning plate, one end of the guide part penetrates through the edge of the positioning plate to form an opening, and the matching part can enter the guide part. Specifically, the number of the alignment mechanisms is two, and the two alignment mechanisms are oppositely arranged on the side wall of the tail part of the arrow body along the radial direction of the arrow body; the positioning mechanisms are arranged in one-to-one correspondence with the alignment mechanisms. Further, the positioning seat comprises a seat body, a sliding block and a first locking piece, wherein the seat body is connected with the launching vehicle, a slide way is formed in the seat body along the width direction of the launching vehicle, the first locking piece penetrates through the sliding block to enter the slide way so that the sliding block can slide along the slide way, and the positioning plate is connected with the sliding block. Further, the positioning mechanism further comprises a second locking piece, and the second locking piece penetrates through the positioning seat to be connected with the launching vehicle. The alignment mechanism comprises a mounting seat and an alignment column, wherein the mounting seat is connected with the arrow body, the alignment column is connected with the mounting seat, and the axis of the alignment column extends along the radial direction of the arrow body. Specifically, the alignment column comprises a rolling part of a column body, the column body is connected with the mounting seat, and the rolling part is sleeved outside the column body and can rotate relative to th