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公开(公告)号:EP2458160A3
公开(公告)日:2016-09-07
申请号:EP11182798.6
申请日:2011-09-26
CPC分类号: F01D15/10 , B64D41/00 , F02C7/275 , F05D2220/3217 , F05D2220/34 , F05D2220/764 , F05D2220/766 , F05D2220/768 , H02P9/00
摘要: A power generating apparatus for use with an aircraft gas turbine engine (10) has a low pressure spool assembly (12) which includes an electrical generator (34). The electrical generator (34) includes a generator stator (48) supported on a stationary structure of the engine and a generator rotor (58) rotatable around the generator stator (48) and mounted to the low pressure spool assembly (12).
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公开(公告)号:EP2458160A2
公开(公告)日:2012-05-30
申请号:EP11182798.6
申请日:2011-09-26
CPC分类号: F01D15/10 , B64D41/00 , F02C7/275 , F05D2220/3217 , F05D2220/34 , F05D2220/764 , F05D2220/766 , F05D2220/768 , H02P9/00
摘要: A power generating apparatus for use with an aircraft gas turbine engine (10) has a low pressure spool assembly (12) which includes an electrical generator (34). The electrical generator (34) includes a generator stator (48) supported on a stationary structure of the engine and a generator rotor (58) rotatable around the generator stator (48) and mounted to the low pressure spool assembly (12).
摘要翻译: 一种与飞机燃气涡轮发动机(10)一起使用的发电装置具有包括发电机(34)的低压线轴组件(12)。 发电机(34)包括支撑在发动机的固定结构上的发电机定子(48)和围绕发电机定子(48)旋转并安装在低压线轴组件(12)上的发电机转子(58)。
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