发明名称 HELICOPTER
摘要 PROBLEM TO BE SOLVED: To realize the safety flight by operating a flight control system by a hydraulic fluid filled in an accumulator over the whole flight control range, and confirming the secure operation of the flight control system. SOLUTION: An accumulator 1 is used as a hydraulic source in the pre-flight check. The accumulator 1 as the hydraulic source for pre-flight check is connected to a switching device 013 through an accumulator line 2. When an ordinary flight control system is operated, the discharged oil from a hydraulic pump 08 driven by an engine is fed to a hydraulic equipment 011 as the hydraulic fluid through a hydraulic feed pipe 012, the switching device 013 and the hydraulic feed pipe 012 to operate most of flight control devices such as a main flight control device by the flight control operation over the whole flight control range.
申请公布号 JP2000079898(A) 申请公布日期 2000.03.21
申请号 JP19990184012 申请日期 1999.06.29
申请人 MITSUBISHI HEAVY IND LTD 发明人 SUZUKI HIROSHI;YONEZAWA FUTOSHI
分类号 B64C27/64;B64C13/40;B64D33/00;(IPC1-7):B64C27/64 主分类号 B64C27/64
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