发明名称 Aircraft structure fatigue alleviation
摘要 A fuel transfer apparatus for an aircraft comprises: two or more fuel tanks ( 2,3,4,5,6 ) arranged in an inboard to outboard alignment, at least one being situated in the wing ( 1 ) of the aircraft, means for transferring fuel between the tanks ( 8, 9 ), and a fuel management system ( 10 ) for controlling and monitoring the transfer of fuel between tanks the fuel management system comprises; means for receiving a first input signal that the aircraft has left the ground, means for receiving a second input signal that the aircraft is approaching its destination, means for initiating the transfer of the fuel from a relatively inboard tank location to a relatively outboard tank location in response to the first input signal, and means for initiating the transfer of the fuel from a relatively outboard tank location to a relatively inboard tank location in response to the second input signal.
申请公布号 AU4937400(A) 申请公布日期 2000.12.28
申请号 AU20000049374 申请日期 2000.05.25
申请人 BAE SYSTEMS PLC 发明人 DAVID JOHN TIGHE;ANDREW DAVID WILLIAMS
分类号 B64C17/10;B64D37/00 主分类号 B64C17/10
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