- 专利标题: Hybrid gas turbine engine starter-generator
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申请号: US10920814申请日: 2004-08-17
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公开(公告)号: US20060038405A1公开(公告)日: 2006-02-23
- 发明人: Mingzhou Xu , Michael Duddeck , Wayne Pearson , William Scherzinger , David Stout
- 申请人: Mingzhou Xu , Michael Duddeck , Wayne Pearson , William Scherzinger , David Stout
- 主分类号: F02N11/04
- IPC分类号: F02N11/04 ; H02K23/52 ; H02P9/04
摘要:
A rotating electrical machine, such as an aircraft starter-generator, that may be operated in either a DC motor mode or an AC generator mode. The machine includes a conventionally wound main stator that is selectively configurable as a multi-pole AC stator and a multi-pole DC stator. The machine also includes rotor windings that are configured to be selectively coupled to either an exciter or a plurality of commutator segments, and DC brushes that are selectively moveable into, and out of, electrical contact with the commutator segments, to thereby electrically couple and decouple a DC power source to and from, respectively, the rotor windings.
公开/授权文献
- US07078826B2 Hybrid gas turbine engine starter-generator 公开/授权日:2006-07-18
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