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특허 상세정보

Electrical generator an aero-engine including such a generator, and an aircraft including such a generator

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/06   
미국특허분류(USC) 244/058; 60/039163
출원번호 US-0564926 (2000-05-04)
우선권정보 GB-0010393 (1999-05-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Baker & McKenzie
인용정보 피인용 횟수 : 86  인용 특허 : 9
초록

An aero-engine is provided with an integrated switched reluctance generator permanently connected to the low speed spool of the engine such that "windmilling" of the engine enables the generator to be turned if the engine suffers a flame out. The generator is driven by a step up gearbox so as to provide reasonable electrical output, say 25 kW, during flameout whilst keeping the generator weight down.

대표
청구항

1. An electrical generator for use with a gas turbine engine having a low speed spool, wherein the generator is driven from the low speed spool, in which the generator is a switched reluctance generator permanently coupled to the low speed spool via a step up gear box.

이 특허를 인용한 특허 피인용횟수: 86

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