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특허 상세정보

Cantilevered tip turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 060/2261; 060/796
출원번호 US-0577595 (2004-12-01)
등록번호 US8033094 (2011-09-27)
국제출원번호 PCT/US2004/039980 (2004-12-01)
§371/§102 date 20070420 (20070420)
국제공개번호 WO06/059978 (2006-06-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds, P.C.
인용정보 피인용 횟수 : 17  인용 특허 : 73
초록

A tip turbine engine (10) according to the present invention includes an engine support structure (12) for cantilevering a load bearing shaft from an engine support plane (P). An engine support structure (12) defines the engine support plane (P), which is perpendicular to an engine centerline (A). The shaft (60) is rotationally fixed, coaxial with the engine centerline (A), and structurally supported by the engine support structure (12) such that a load borne by the shaft (60) is transferred along the engine support plane.

대표
청구항

The invention claimed is: 1. A tip turbine engine assembly comprising:an axial compressor having a plurality of compressor blades;a fan downstream of the axial compressor;an engine support plane defined by an engine support structure;an engine centerline axis essentially perpendicular to said support plane; anda fixed shaft coaxial with said engine centerline axis, the fixed shaft having a forward end aft of the plurality compressor blades, said fixed shaft being non-moveable during operation, wherein said fixed shaft is cantilevered from said engine sup...

이 특허에 인용된 특허 (73)

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  2. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP2017119821917.
  3. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP20180710017270.
  4. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David. Aft engine for an aircraft. USP2018059957055.
  5. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Aircraft having an aft engine. USP2017059637217.
  6. Lamarre, Sylvain; Fontaine, Mike; Julien, Andre; Gaul, Michael; Thomassin, Jean; Mitrovic, Lazar. Compound engine assembly with cantilevered compressor and turbine. USP2018019869240.
  7. Kupiszewski, Thomas; Miller, Brandon Wayne; Vondrell, Randy M.. Electric propulsion system. USP20181010093428.
  8. Miller, Brandon Wayne; Vondrell, Randy M.; Marrinan, Patrick Michael; Gemin, Paul Robert; Moore, Nicholas Taylor. Electric propulsion system for an aircraft. USP20181110137981.
  9. Kupiszewski, Thomas; Miller, Brandon Wayne; Vondrell, Randy M.; Gemin, Paul Robert. Embedded electric machine. USP20180910071811.
  10. Porte, Alain. Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft. USP2013028366039.
  11. Miller, Brandon Wayne; Schmidt, Richard; Niergarth, Daniel Alan. Gas turbine engine frame assembly. USP2018049932858.
  12. Reinhardt, Gregory; Swiderski, Joseph; Pollock, Douglas; Barrette, Real; Mongeau, Stephane. Gas turbine engine module adapter to a carrier. USP2018059982568.
  13. Reinhardt, Gregory; Swiderski, Joseph; Pollock, Douglas; Barrette, Réal; Mongeau, Stéphane. Gas turbine engine module adapter to a carrier. USP2016019228451.
  14. Hamel, Jeffrey Anthony; Murrow, Kurt David. Gas-electric propulsion system for an aircraft. USP20180610000293.
  15. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Non-axis symmetric aft engine. USP2018029884687.
  16. Niergarth, Daniel Alan; Vondrell, Randy M.; Miller, Brandon Wayne; Marrinan, Patrick Michael. Propulsion engine for an aircraft. USP20190410252810.
  17. Vondrell, Randy M.; Polakowski, Matthew Ryan; Murrow, Kurt David; Crabtree, Glenn. Propulsion system for an aircraft. USP2017099764848.