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    • 5. 发明公开
    • ADAPTOR AND PAYLOAD-LAUNCHING ROCKET
    • 适应症在NUTZLASTSTARTRAKETE
    • EP2657136A1
    • 2013-10-30
    • EP11850682.3
    • 2011-12-15
    • Mitsubishi Heavy Industries, Ltd.
    • TOMBE, Toshihiro
    • B64G1/64B64G1/38F16F15/02F16F15/04F16F15/073
    • B64G1/641B64G2001/228F16F15/02F16F15/04F16F15/073F16F2230/0052
    • An object is to provide an adaptor that can attenuate a vibration acting on a payload using a simple structure, and a payload launch vehicle. The adaptor (1) according to the invention controls a vibration of the payload housed in the payload launch vehicle, and is provided between the payload and a rocket portion. The adaptor (1) includes a tube member having a double structure including an outer tube (11) and an inner tube (12); a first elastic member (21) coupled to the outer tube (11) and the inner tube (12) at one end of the tube member; and a second elastic member (22) coupled to the outer tube and the inner tube at the other end of the tube member. The adaptor (1) is linked to the payload on the inner tube side or the outer tube side on one end side of the tube member, and linked to a leading end of the rocket portion on the outer tube side or the inner tube side on the other end side of the tube member.
    • 目的是提供一种适配器,其可以使用简单的结构和有效载荷运载火箭衰减作用在有效载荷上的振动。 根据本发明的适配器(1)控制装载在有效载荷运载火箭中的有效载荷的振动,并且设置在有效载荷和火箭部分之间。 适配器(1)包括具有包括外管(11)和内管(12)的双重结构的管构件; 在所述管构件的一端处联接到所述外管(11)和所述内管(12)的第一弹性构件(21) 以及在所述管构件的另一端处联接到所述外管和所述内管的第二弹性构件(22)。 适配器(1)连接到管构件的一端侧的内管侧或外管侧的有效载荷上,并且与外管侧或内管侧的火箭部的前端连接 管构件的另一端侧。