发明名称 PAY-LOAD DAMPING MECHANISM
摘要 PROBLEM TO BE SOLVED: To allow supporting a pay-load by attenuating a vibration and a locking applied to the pay-load effectively. SOLUTION: This is a pay-load damping mechanism to attenuate the vibration applied to a pay-load 5 as well as to support the pay-load 5 housed in a rocket for pay-load shooting up, at a pay-load adapter 4 side, and cushioning bodies 12 provided plurally in the peripheral direction in order to attenuate the vibrations in the machine axis 13 direction of the rocket and in the direction perpendicular to the machine axis by supporting the load of the pay-load 5; semiactive dampers 20 provided plurally in the peripheral direction in order to increase the cushioning effect of the vibration; and tortion bars 21 and 22 provided to cross at least two sets or more, on the surface orthogonal to the machine axis 13 of the rocket, in order to prevent the locking of the pay-load 5; are provided.
申请公布号 JP2000289699(A) 申请公布日期 2000.10.17
申请号 JP19990098848 申请日期 1999.04.06
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 KASHIWAZAKI AKIHIRO;KOIKE YUJI;AZUMI ICHIRO;MITA MICHIYA;IWAMOTO HIROSUKE
分类号 B64G1/38;B64G1/64;F16F15/04;(IPC1-7):B64G1/38 主分类号 B64G1/38
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