发明名称 REGLERANORDNING FOR DRIVKRAFTEN HOS FLYGPLAN
摘要 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.
申请公布号 SE8702113(L) 申请公布日期 1988.03.01
申请号 SE19870002113 申请日期 1987.05.21
申请人 GEN ELECTRIC 发明人 WALKER N NMN;DAY S G;COLLOPY P D;BENNETT G W
分类号 B64D31/12;B64C11/30;B64C11/50;F02C9/58;F02K3/072;(IPC1-7):B64C13/00 主分类号 B64D31/12
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