发明名称 Aircraft Auxiliary Fuel Tank System and Method
摘要 One or more main aircraft fuel tanks are provided with one or more fuel gauges arranged to provide a measure of the amount of fuel in said one or more main fuel tanks. One or more auxiliary fuel tanks are also provided. The aircraft uses fuel during a first phase of fuel consumption, upon commencement of which phase the auxiliary fuel tanks hold fuel. After the first phase said one or more auxiliary fuel tanks are empty and a second phase commences. During the first phase, an indication of the amount of fuel carried by the aircraft is provided by means of summing (i) the amount of fuel in the main fuel tanks as measured by said one or more fuel gauges and (ii) the amount of fuel remaining in said one or more auxiliary fuel tanks as calculated using a measure relating to the fuel consumption rate. During the second phase of fuel consumption, an indication of the amount of fuel carried by the aircraft is provided on the basis of the amount of fuel measured by said one or more fuel gauges.
申请公布号 US2008272237(A1) 申请公布日期 2008.11.06
申请号 US20060158061 申请日期 2006.12.01
申请人 AIRBUS UK LIMITED 发明人 TICHBORNE FRANKLIN GEORGE;LEY KIM MICHAEL
分类号 B64D37/02;G01F23/00 主分类号 B64D37/02
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