发明名称 An electrical generation arrangement for an aircraft
摘要 This invention relates to a multi-spool gas turbine engine, comprising: a first generator for providing electrical power to an electrical system, the generator being driveably connected to a first spool; a second generator for providing electrical power to the electrical system, the generator being driveably connected to a second spool; a disconnection device for disconnecting the second generator from the second spool; and, a controller configured to selectively operate the disconnection device under predetermined powered engine conditions.
申请公布号 EP2728141(A2) 申请公布日期 2014.05.07
申请号 EP20130005183 申请日期 2013.11.02
申请人 ROLLS-ROYCE PLC 发明人 EDWARDS, HUW LLEWELYN;SLATER, ROBERT WILLIAM
分类号 F02C3/113;F02C7/32 主分类号 F02C3/113
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