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Modified start sequence of a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64F-001/34
  • B64D-027/16
  • F02C-007/27
  • F02C-007/277
출원번호 US-0042363 (2016-02-12)
등록번호 US-10040577 (2018-08-07)
발명자 / 주소
  • Teicholz, Matthew D.
  • Sutliff, Jeffrey W.
  • Greene, Jr., William H.
  • White, Kenneth J.
  • Feulner, Matthew R.
  • Virtue, Jr., John P.
  • Glahn, Jorn A.
  • Hoover, Philip D.
  • Pinedo, Victor M.
  • Solomonides, Jason B.
출원인 / 주소
  • UNITED TECHNOLOGIES CORPORATION
대리인 / 주소
    Cantor Colburn LLP
인용정보 피인용 횟수 : 0  인용 특허 : 62

초록

A system for starting a gas turbine engine of an aircraft is provided. The system includes a pneumatic starter motor, a discrete starter valve switchable between an on-state and an off-state, and a controller operable to perform a starting sequence for the gas turbine engine. The starting sequence i

대표청구항

1. A system for starting a gas turbine engine of an aircraft, the system comprising: a pneumatic starter motor;a discrete starter valve switchable between an on-state and an off-state;a controller operable to perform a starting sequence for the gas turbine engine, the starting sequence comprising al

이 특허에 인용된 특허 (62)

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