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Differentially geared reversible fan for ducted fan gas turbine engines 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/04
  • F02C-003/06
출원번호 US-0609931 (1975-09-03)
우선권정보 UK-0039694 (1974-09-11)
발명자 / 주소
  • Scott Alexander (Bristol EN) Peck Peter Eric (Bristol EN)
출원인 / 주소
  • Rolls-Royce (1971) Limited (EN 03)
인용정보 피인용 횟수 : 86  인용 특허 : 0

초록

A ducted fan gas turbine engine comprises a pair of turbines in flow series which are contra-rotating and which drive shafts which in turn drive into an epicyclic gear. The output from the epicyclic gear drives a fan which normally provides forward thrust from the engine. The fan can be made to rota

대표청구항

A ducted fan gas turbine engine comprising a fan, two shafts, a turbine drivingly connected to each shaft for driving the shafts in opposite rotational directions, and a gear mechanism, wherein the two shafts are connected with the gear mechanism, the output of the gear mechanism being connected to

이 특허를 인용한 특허 (86)

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