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Turbine engine arrangements

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/055
출원번호 US-0036360 (2005-01-18)
우선권정보 GB-0401189.6(2004-01-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Oliff & Berridge, PLC
인용정보 피인용 횟수 : 22  인용 특허 : 36
초록
▼

A fan turbine engine arrangement is provided in which a core engine is aligned such that an input of a nacelle is aligned with the upwash of a wing to which the arrangement is secured. The engine drives a fan such that bypass flows produced by the fan are guided by a duct to present a downward component for uplift. The core engine presents its output flow through a nozzle which is aligned with the fundamental axis Y--Y of the engine. In such circumstances, the bypass flows cross the core engine flow from the nozzle unless that engine is adjustable during...

대표
청구항
▼

The invention claimed is: 1. A turbine engine arrangement comprising: a nacelle defining an inlet duct and a final mixing nozzle; a turbine engine disposed in a flow path between the inlet duct and the final mixing nozzle, the arrangement secured to an aircraft wing, wherein the engine includes a fan and a core engine that rotate about a principal rotation axis of the engine, wherein the principal rotation axis is aligned with an upflow of air to the wing to avoid a turning of an inlet flow in the inlet to pass through the engine, and wherein the final...

이 특허에 인용된 특허 (36)

  1. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing engine and engine nacelle combination. USP1984054449680.
  2. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing engine and engine nacelle combination. USP1984054449683.
  3. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing, engine and engine nacelle combination. USP1984054449681.
  4. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing, engine and engine nacelle combination. USP1984054449682.
  5. Seelen Laurence (Cincinnati OH) Joseph Thomas P. (West Chester OH) Spofford Hahn M. (West Chester OH) Orkiszewski Charles S. (Cincinnati OH). Aircraft engine forward mount. USP1994015277382.
  6. Brantley, James W.. Aircraft gas turbine engine backbone deflection control. USP1994065319922.
  7. Marche Herve,FRX. Aircraft motor pod including a pivotable pod cowling. USP1998055755403.
  8. Cole Ronald A. (Barnet GB2). Attachment of masses to aircraft and spacecraft. USP1982034318516.
  9. Reysa Gary D. ; Swenson Lynn A. ; Hutchison Robert A. ; Fung Kenny L.. Auxiliary power and thrust unit. USP2001066247668.
  10. Kelber Charles C. (2081 Snowden Ave. Long Beach CA 90815). Combination lift thrust device. USP1987054666104.
  11. Denning Ralph M. (Bristol GB2). Compound helicopter and powerplant therefor. USP1987094691877.
  12. Hapke Donald W. (Issaquah WA). Deployable inlet for aeroplane center boost engine. USP1984064456204.
  13. Saiz Manuel Munuoz,ESXITX 28017. Device for lift and to reduce resistance to aircraft advance. USP2000106138946.
  14. Goldstein Sidney E. (Kirkland WA) Pera Ronald J. (Seattle WA). Devices and method for rocket booster vectoring to provide stability augmentation during a booster launch phase. USP1988014721271.
  15. Ivers Douglas E.. Efficient multi-directional active vibration absorber assembly. USP2000016009985.
  16. James Varnell L. (Enumclaw WA). Engine mounting assembly. USP1976043952973.
  17. Kress Robert W. (Saugerties NY). Four engine VTOL aircraft. USP1992075131605.
  18. Dunn, James P.. Fuel cell powered electric aircraft. USP2003056568633.
  19. Wynosky Thomas A. (Madison CT). Gas turbine engine nacelle. USP1988024722357.
  20. Johnson ; Joseph M.. Gas turbine exhaust nozzle for controlled temperature flow across adjoining airfoils. USP1978014066214.
  21. Farris Edsel S. (Burton WA). Jet flow deflector for aircraft. USP1976023940092.
  22. Duesler Paul W.. Mounting arrangement for a gas turbine engine. USP1998075775638.
  23. Rodgers Leonard J.,GB2 ; Newton Arnold C.,GB2 ; Berry James P.,GB2 ; Farrar Peter G. G.,GB2 ; Udall Kenneth F.,GB2. Mounting for coupling a turbofan gas turbine engine to an aircraft structure. USP1998055746391.
  24. Stockman Norbert O. (Batavia OH) Yates David E. (Cincinnati OH) Crum Timothy S. (Fairfield OH). Nacelle inlet for an aircraft gas turbine engine. USP1991105058617.
  25. Parkinson, Colin C. A.; Kinnerly, Anthony G.. Power plant attachment arrangements for aircraft wings. USP1985124560122.
  26. Bradfield Ganey W. (Fort Worth TX) Cragin ; Jr. Glynn P. (Irving TX). Propulsion system for a V/STOL airplane. USP1981114301980.
  27. Bevilaqua, Paul. Propulsion system for a vertical and short takeoff and landing aircraft. USP2004056729575.
  28. Smith Michael A. (Tacoma WA). Strut supported inlet. USP1984074458863.
  29. Powell Donald T.. Strut-wing interface having dual upper links. USP2000086095456.
  30. White John L. (Bellevue WA). System for mounting a jet engine. USP1986084603821.
  31. Musgrove Robert G. (Arlington TX). Tandem fan series flow VSTOL propulsion system. USP1984104474345.
  32. Zimmermann Vincent H. (Olivette MO) DEGarcia ; Jr. Horacio J. (Maryland Heights MO) Pierson Harlan K. (Hazelwood MO). Trifan powered VSTOL aircraft. USP1976083972490.
  33. Valverde Rene L. (4405 Toledo St. Coral Gables FL 33146). Turbocraft. USP1991085039031.
  34. Kress Robert W. (4308 Ulster Landing Rd. Saugerties NY 12477) Stump Joseph W. (42 Derby Pl. Smithtown NY 11787). Unmanned aerial aircraft having a single engine with dual jet exhausts. USP1994125372337.
  35. Giffin ; III Rollin G. (Cincinnati OH). Variable specific thrust turbofan engine. USP1993115261227.
  36. Lardellier Alain M. J. (Melun FRX). Wing mounting nacelle for a very high by-pass ratio turbojet aero-engine. USP1990074940196.

이 특허를 인용한 특허 피인용횟수: 22

  1. Dawson, Stacie M.; Wiley, Richard. Core reflex nozzle for turbofan engine. USP2011088002520.
  2. Dindar, Mustafa; Burton, Scott Andrew; Blodgett, Keith Edward James; Cedar, Richard David. Exhaust nozzle with non-coplanar and/or non-axisymmetric shape. USP2017119810178.
  3. McCall, John. Fan exhaust nozzle for turbofan engine. USP2013108561384.
  4. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2010097797944.
  5. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014098844294.
  6. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2013018353164.
  7. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014058726632.
  8. Winter, Michael; Jain, Ashok K.. Gas turbine engine providing simulated boundary layer thickness increase. USP2011017870721.
  9. Winter, Michael; Jain, Ashok K.. Gas turbine engine system providing simulated boundary layer thickness increase. USP2012078209953.
  10. Suchezky, Mark E.; Simpkins, Lisa M.. Jet engine exhaust nozzle and associated system and method of use. USP2014068746613.
  11. Jain, Ashok K.; Winter, Michael. Nacelle assembly having inlet airfoil for a gas turbine engine. USP2013048408491.
  12. Haas, Martin. Nacelle assembly having inlet bleed. USP2012068192147.
  13. Haas, Martin. Nacelle assembly with turbulators. USP2012058186942.
  14. Jain, Ashok K.. Nacelle flow assembly. USP2013128596573.
  15. Jain, Ashok K.. Nacelle flow assembly. USP2012108282037.
  16. Jain, Ashok K.. Nacelle flow assembly. USP2015049004399.
  17. Marley, Scott. Non-handed thrust reverser for installation on handed aircraft gas turbine propulsion engines. USP2013058439305.
  18. Jain, Ashok K.; Winter, Michael. Variable contour nacelle assembly for a gas turbine engine. USP2016019228534.
  19. Jain, Ashok K.; Winter, Michael. Variable contraction ratio nacelle assembly for a gas turbine engine. USP2014058727267.
  20. Jain, Ashok K.. Variable geometry nacelle assembly for a gas turbine engine. USP2012068205430.
  21. Jain, Ashok K.; Chaudhry, Zaffir A.. Variable shape inlet section for a nacelle assembly of a gas turbine engine. USP2013038402739.
  22. Dindar, Mustafa; Burton, Scott Andrew; Blodgett, Keith Edward James; Cedar, Richard David. Variable slope exhaust nozzle. USP2015119181899.

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