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특허 상세정보

Compound engine assembly with direct drive of generator

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-015/10    F02C-006/00    H02K-007/18    H02P-009/04    B64D-041/00    F01C-001/22    F02C-003/10    F01C-011/00    B64D-013/06   
출원번호 US-0750207 (2015-06-25)
등록번호 US-9771165 (2017-09-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Norton Rose Fulbright Canada
인용정보 피인용 횟수 : 2  인용 특허 : 33
초록

A compound engine assembly for use as an aircraft auxiliary power unit, having an engine core including internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft directly engaged to the engine shaft such as to be rotatable at a same speed, a compressor having an outlet in communication with the engine core inlet, and a turbine section having an inlet in communication with the engine core outlet and configured to compound power with the engine core. The turbine section may include a first stage turbine ...

대표
청구항

1. A compound engine assembly for use as an auxiliary power unit for an aircraft, the compound engine assembly comprising: an engine core including at least one internal combustion engine each in driving engagement with an engine shaft;a generator having a generator shaft in driving engagement with the engine shaft to provide electrical power for the aircraft, the generator and engine shafts being directly engaged to one another such as to be rotatable at a same speed;a compressor having an outlet in fluid communication with an inlet of the engine core; ...

이 특허에 인용된 특허 (33)

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