发明名称 FUEL PUMPING SYSTEM FOR A GAS TURBINE ENGINE
摘要 <p>A fuel supply system for a gas turbine engine has a first pump for delivering fuel to a first use on a gas turbine engine, and a second pump for delivering fuel to a second use on the gas turbine engine. A valve allows flow from the first pump to be delivered to the first use, but also routes some flow from the first pump to supplement fuel flow from the second pump until a pressure downstream of the second pump increases. The valve then allows flow from the second pump to flow to the first use to supplement the flow from the first pump.</p>
申请公布号 CA2736449(A1) 申请公布日期 2011.11.25
申请号 CA20112736449 申请日期 2011.04.06
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 DYER, GERALD P.;GIBBONS, KEVIN
分类号 F02C7/236;F02C7/232 主分类号 F02C7/236
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