AIRCRAFT LEG DROP TESTER

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. SOLUTION: A leg support 20 is combined with a plumb, downwardly couples and fixes the aircraft leg 10, and vertica...

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Bibliographische Detailangaben
1. Verfasser:	FUJIOKA KENJI
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	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. 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. COPYRIGHT: (C)2010,JPO&INPIT