发明名称 AIRCRAFT THRUST CONTROL
摘要 <p>AIRCRAFT THRUST CONTROL An integrated control system for coaxial counterrotating aircraft propulsors driven by a common gas turbine engine. The system establishes an engine pressure ratio by control of fuel flow and uses the established pressure ratio to set propulsor speed. Propulsor speed is set by adjustment of blade pitch.</p>
申请公布号 CA1273211(A) 申请公布日期 1990.08.28
申请号 CA19870535879 申请日期 1987.04.29
申请人 GENERAL ELECTRIC COMPANY 发明人 BENNETT, GEORGE W.;WALKER, NEIL
分类号 F02C9/58;F02K3/072;(IPC1-7):B64C11/48 主分类号 F02C9/58
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