| 摘要 |
PROBLEM TO BE SOLVED: To provide a supporting structure of a seat for an aircraft improved in shock absorbing capacity without adding new development and design change to a conventional seat for the aircraft. SOLUTION: A supporting structure 1 of the seat 60 for the aircraft is constituted of a fixing member fixed to an installation surface 100 by supporting the seat 60, a mount 30 mounted on the seat 60, and a shaft member 40 having both end parts supported by the mount 30 and an intermediate part supported by the fixing member. The shaft member 40 is set to absorb transmitted impact energy by being deformed by the impact energy. COPYRIGHT: (C)2006,JPO&NCIPI
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