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특허 상세정보

Electrical aircraft engine start and generating system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02N-011/04    F02N-011/14   
미국특허분류(USC) 322/10 ; 290/38R ; 290/46 ; 318/138
출원번호 US-0169699 (1980-07-17)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 52  인용 특허 : 0
초록

This invention relates to electrical aircraft engine start and generating system for use in an aircraft having an engine driven torque converter coupled to an alternator which provides AC power for conversion to DC and AC power. The system includes a reversible AC to DC converter controllably electrically coupled to the alternator and a controller unit to provide DC power in a generating mode. The reversible AC to DC converter is capable of receiving externally supplied DC power to be converted to AC power to drive the alternator as a motor in a start mo...

대표
청구항

An electrical aircraft engine start and generating system for use in an aircraft having an engine driven drive unit coupled to an alternator which provides AC power for conversion to DC and AC power, said system including in combination: a reversible AC to DC converter means controllably electrically coupled to said alternator and a controller means to provide DC power output in a generating mode, said reversible AC to DC converter means capable of receiving externally supplied DC power to be converted to AC power to drive said alternator as a motor in a...

이 특허를 인용한 특허 피인용횟수: 52

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