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 GB201219916(D0) 申请公布日期 2012.12.19
申请号 GB20120019916 申请日期 2012.11.06
申请人 ROLLS-ROYCE PLC 发明人
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代理机构 代理人
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