A release system (1) for releasing satellites from a launch vehicle, comprising: (i) a torsion bar (2) having a first end (2a) fixed to the launch vehicle (3) by means of support means (4) and locked in terms of rotation about a longitudinal axis (X) of the torsion bar (2), and a second end (2b) connected to the launch vehicle (3) by means of hinge means (5) and free to rotate about the longitudinal axis (X); (ii) at least one launch arm (6) extending perpendicularly from the torsion bar (2) and comprising: (a) a torsion bar (7) having a first end (7a) fixed in an integral manner to the torsion bar (2); and (b) a guide (8) having a first end (8a) connected to the second end (7b) of the torsion bar (7), and a second free end (8b); (iii) at least one slider (10) fixed in an integral manner to the satellite (18) to be launched and arranged to engage the guide (8) in a sliding manner; and (iv) a limit stop element (12) designed to act on the torsion bar (7) to interrupt the rotation of the launch arm (6) about the longitudinal axis (X).
一种用于从运载火箭释放卫星的释放系统(1),包括:(i)扭杆(2),具有第一端(2a)和第二端(2b),第一端(2a)通过支承器件(4)固定至运载火箭(3),并且在围绕扭杆(2)的纵向轴线(X)的旋转方面被锁定,第二端(2b)通过铰接器件(5)连接至运载火箭(3),并且围绕纵向轴线(X)自由旋转;(ii)至少一个发射臂(6),从扭杆(2)垂直地延伸,并且包括:(a)扭力杆(7),具有以整体方式固定至扭杆(2)的第一端(7a);以及(b)引导件(8),具有连接至扭力杆(7)的第二端(7b)的第一端(8a)、以及第二自由端(8b);(iii)至少一个滑动件(10),以整体方式固定至待发射的卫星(18),并布置成以滑动方式接合引导件(8);以及(iv)限位止动元件(12),设计成作用在扭力杆(7)上,以中断发射臂(6)围绕纵向轴线(X)旋转。
System for releasing satellites from launch vehicle
用于从运载火箭释放卫星的系统
2023-02-03
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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