Title:
ロケット後支点支持調整システム
Document Type and Number:
Japanese Patent JP7339366
Kind Code:
B2
Abstract:
A rocket rear fulcrum support adjustment system, comprising two rocket rear fulcrum support adjustment apparatuses fixedly arranged on both sides of a lifting arm (5) along the direction of width of the lifting arm (5), the two being symmetrical about the central axis of the lifting arm (5) in the direction of length; each rocket rear fulcrum support adjustment apparatus comprises a slewing support base (1), a rotation pushing unit (2), a support unit (3), and a pulling unit (4); the rotation pushing unit (2) is arranged between the slewing support base (1) and the lifting arm (5), and is used for pushing the slewing support base (1) to rotate to avoid the rocket lift-off space; the support unit (3) is arranged on the slewing support base (1), and is used for supporting the rear fulcrum of the rocket; and the pulling unit (4) is connected to the slewing support base (1) and the support unit (3); in the process of lifting up the rocket, the support of the support unit (3) gradually transforms into pulling of the rocket by the pulling unit (4). The present system can implement multiple degree of freedom adjustment of the rocket, effectively reducing the difficulty of aligning and adjusting the rocket during reloading, and significantly increasing the efficiency of aligning the rocket with the launch pad after lifting.
Inventors:
Zhang Yu
Zhang Hikojo
Han dynasty
Wei silver interest
Jun Yang
Wu Snow
Zhang Hikojo
Han dynasty
Wei silver interest
Jun Yang
Wu Snow
Application Number:
JP2021572674A
Publication Date:
September 05, 2023
Filing Date:
November 03, 2020
Export Citation:
Assignee:
BEIJING LANDSPACETECH CO., LTD.
International Classes:
B64G5/00; F16M11/10
Domestic Patent References:
| JP5342500A |
Foreign References:
| CN105865265A | ||||
| US6186039 | ||||
| KR101676373B1 | ||||
| RU2477247C1 | ||||
| CN111006546A |
Attorney, Agent or Firm:
Choi Hae-ryong
Takayuki Kawai
Takayuki Kawai