首页> 外国专利> PAYLOAD SUSPENSION SYSTEM OF LAUNCH VEHICLE; LAUNCH VEHICLE PROVIDED WITH SUCH SUSPENSION SYSTEM AND PAYLOAD OF LAUNCH VEHICLE

PAYLOAD SUSPENSION SYSTEM OF LAUNCH VEHICLE; LAUNCH VEHICLE PROVIDED WITH SUCH SUSPENSION SYSTEM AND PAYLOAD OF LAUNCH VEHICLE

机译:发射车辆的有效载荷悬挂系统;具有这种悬架系统的发射车辆和发射车辆的有效载荷

摘要

FIELD: space engineering. SUBSTANCE: proposed system is used for satellite, personnel, cargo unit of orbital station. Proposed suspension system includes one or more hydraulic chambers of variable geometry which are arranged between launch vehicle and payload. Provision is made for first and second rigid members secured to chamber and payload on one side and to launch vehicle on other side for transmission of arising loads through structure of said chamber. Hydraulic chamber and said rigid members are circular in shape; each first and second member has at least one external and one internal fin which are separated by said chamber. Various versions of hydraulic chambers, their members and structural beams are described in invention. EFFECT: reduction of mass; avoidance of transmission of peak loads, impact loads or vibrations to payload. 16 cl, 12 dwg
机译:领域:空间工程。物质:提议的系统用于轨道站的卫星,人员,货物单元。提出的悬架系统包括布置在运载火箭和有效载荷之间的一个或多个可变几何形状的液压室。设置了第一和第二刚性构件,该第一和第二刚性构件在一侧被固定到舱室和有效载荷,并且在另一侧被发射车辆以通过所述舱室的结构传输所产生的载荷。液压室和所述刚性构件为圆形。每个第一和第二构件具有至少一个外部翅片和一个内部翅片,它们由所述腔室隔开。在本发明中描述了液压室的各种形式,其构件和结构梁。效果:减轻重量;避免将峰值载荷,冲击载荷或振动传递给有效载荷。 16厘升,12载重吨

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