发明名称 Last chance aircraft back-up hydraulic system
摘要 A last chance aircraft back-up hydraulic system in which fuel from the fuel tanks of the aircraft is injected into the return line of a leaking hydraulic system by use of a pump activated by a guarded switch by the aircraft's pilot. The fuel serves as hydraulic fluid to operate the pumps of the system as it is injected upstream from the fluid being lost to extend the operating time of the system and prevent failure so the aircraft can be landed at a site.
申请公布号 US2003094540(A1) 申请公布日期 2003.05.22
申请号 US20010990639 申请日期 2001.11.21
申请人 THE BOEING COMPANY 发明人 SHAPPELL PAUL E.;JANIESCH RICHARD H.
分类号 B64C13/42;F15B20/00;F15B21/06;(IPC1-7):B64B1/36;B64C15/00 主分类号 B64C13/42
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