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특허 상세정보

Electrical systems architecture for an aircraft, and related operating methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) H02K-007/00   
미국특허분류(USC) 290/007
출원번호 UP-0944199 (2007-11-21)
등록번호 US-7687927 (2010-04-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Hope Baldauff Hartman, LLC
인용정보 피인용 횟수 : 9  인용 특허 : 41
초록

An electrical architecture for an aircraft is provided. The electrical architecture is particularly suitable for relatively small, compact, and lightweight aircraft. In one embodiment, the electrical architecture includes an electrical generator component coupled to the aircraft engine, and an air compression system coupled to the electrical generator component. The electrical generator component is configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the engine mechanical power, and the air...

대표
청구항

What is claimed is: 1. An electrical architecture for an aircraft having an engine, the electrical architecture comprising: an electrical generator component coupled to the engine, the electrical generator component being configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the mechanical power; and an air compression system comprising a compressor motor subsystem that lacks a motor controller, the air compression system coupled to the electrical generator component and configured to receiv...

이 특허에 인용된 특허 (41)

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