发明名称 |
METHOD AND ARRANGEMENT FOR AIRCRAFT FUEL DISPERSION |
摘要 |
Method and arrangement for dispersing fuel 62 within a fuel containment system 60 of an aircraft 30 including utilizing a fuel containment system on an aircraft that is located at least partially within a wing 34 of the aircraft and defines a reservoir portion 42 and a remote portion 44 . Fuel is pumped during at least aircraft flight operation from the reservoir portion to the remote portion at a pumped rate 80 , while simultaneously fuel that is contained in the remote portion of the fuel containment system is permitted to drain to the reservoir portion at a drainage rate 82 . The drainage rate is less than the pumped rate. A fuel mass 64 is accumulated in the remote portion of the fuel containment system because of a difference between the pumped rate and the drainage rate and as a result, a counteractive moment 49 is induced in the aircraft that is opposingly directed to a lift moment 46 caused by wing-lift 45 during aircraft flight.
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申请公布号 |
US2005139727(A1) |
申请公布日期 |
2005.06.30 |
申请号 |
US20040708818 |
申请日期 |
2004.03.26 |
申请人 |
GULFSTREAM AEROSPACE CORPORATION |
发明人 |
WOZNIAK GREGG;LAMB DAVID;LE DUNG |
分类号 |
B64C17/10;B64D37/00;(IPC1-7):B64D37/00 |
主分类号 |
B64C17/10 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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