发明名称 AIRCRAFT LEG DROP TESTER
摘要 <P>PROBLEM TO BE SOLVED: To provide an aircraft leg drop tester for implementing a drop test without a trouble if an aircraft leg is a small leg having a small requirement of a plumb load. Ž<P>SOLUTION: A leg support 20 is combined with a plumb, downwardly couples and fixes the aircraft leg 10, and vertically and movably supports it within a guide window 30. A support lifting means 40 with a coupling/releasing mechanism is provided within the guide window 30 along with the leg support 20. The support lifting means 40 downwardly couples the leg support 20, lifts the leg support 20 within the guide window 30, releases the leg support 20 from a predetermined level within the guide window 30 to drop, and includes an electromagnet 42 as the coupling/releasing mechanism of the leg support 20 for upwardly sucking the leg support 20. Ž<P>COPYRIGHT: (C)2010,JPO&INPIT Ž
申请公布号 JP2010181318(A) 申请公布日期 2010.08.19
申请号 JP20090025845 申请日期 2009.02.06
申请人 SUMITOMO PRECISION PROD CO LTD 发明人 FUJIOKA KENJI
分类号 G01N3/303;B64F5/00 主分类号 G01N3/303
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