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특허 상세정보

Conjoined reverse core flow engine arrangement

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-029/06    F02K-001/54    F01D-013/00    B64D-027/20    F02K-001/52    F02K-001/60    F02K-001/64   
출원번호 US-0190175 (2014-02-26)
등록번호 US-9845159 (2017-12-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kinney & Lange, P. A.
인용정보 피인용 횟수 : 1  인용 특허 : 48
초록

A system of conjoined gas turbine engines has a first engine with a first propulsor having a first axis and a first engine core having a second axis, and a second engine with a second propulsor having a third axis and a second engine core having a fourth axis. The first axis and third axis are parallel to one another; and the second axis and fourth axis are angled from one another.

대표
청구항

1. A system of conjoined gas turbine engines, the system comprising: a first engine with a first propulsor having a first axis and a first engine core having a second axis;a second engine with a second propulsor having a third axis and a second engine core having a fourth axis;wherein the first axis and third axis are parallel to one another; andwherein the second axis and fourth axis are angled from one another, such that the first engine core diverges from the second engine core in an axially aft direction;wherein the first engine core and the second e...

이 특허에 인용된 특허 (48)

  1. Guida, Nicholas R.. Active winglet. USP2014048684315.
  2. Guida, Nicholas R.. Active winglet. USP2011037900877.
  3. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Aircraft configuration. USP2011098016233.
  4. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.; Lan, Justin. Aircraft configuration. USP2014018628040.
  5. Carlson Robert B. (Tukwila WA) Cosgrove Barbara J. (Kirkland WA) Meredith Paul T. (Renton WA). Aircraft configuration with aft mounted engines. USP1990124976396.
  6. Van der Hoeven Antonius J. (Issaquah WA). Aircraft configuration with aft mounted engines and method. USP1990094953812.
  7. Gall, Pierre-Emmanuel; Cros, Christophe. Aircraft having a reduced environmental impact. USP2012118313055.
  8. Krojer Hubert (Bermatingen DEX). Aircraft propulsion system arrangement. USP1985024500055.
  9. Lawson Dale W. R. (Bonita CA). Aircraft turbine engine thrust reverser. USP1993075230213.
  10. Cazals, Olivier. Aircraft with jet engines arranged at the rear. USP2012038128023.
  11. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Airplane configuration. USP2011037900865.
  12. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Airplane configuration. USP2012018087607.
  13. Chanez, Philippe Gerard; Lecordix, Jean-Loic Herve; Thomas, Stephane Jacques Francois. Airplane having engines partially encased in the fuselage. USP2014048684302.
  14. Cazals, Olivier; Manneville, Alexis. Airplane with rear engines. USP2013118573531.
  15. Llamas Sandín, Raúl Carlos. Arrangement for mounting an engine on the airframe of an aircraft. USP2010067726602.
  16. Guillois, Denis; Blin, Laurent Albert; Chapelain, Löic. Cascade type thrust reverser having a pivoting door. USP2014078783010.
  17. Blythe Alan Avery (St. Albans EN) Milligan Robert Ian (Belfast EK). Combined noise shield and thrust reverser. USP1976023936017.
  18. Agrawal, Rajendra K.; Sirica, Steven J.; Schneider, William F.. Convertible gas turbine propulsion system. USP2013088511058.
  19. Suciu, Gabriel L.; Chandler, Jesse M.. Gas turbine engine having fan rotor driven by turbine exhaust and with a bypass. USP2016059352843.
  20. Taylor Maurice I. (Allestree GB2). Gas turbine engine power plant. USP1987074679394.
  21. Roberge, Gary D.. Gas turbine engine systems and related methods involving multiple gas turbine cores. USP2014058726633.
  22. Roberge, Gary D.. Gas turbine engine systems and related methods involving multiple gas turbine cores. USP2012128336289.
  23. Suciu, Gabriel L.; Staubach, Joseph B.; Dye, Christopher M.. Gas turbine engine with modular cores and propulsion unit. USP2015028955304.
  24. Suciu, Gabriel L.; Lord, Wesley K.; Dye, Christopher M.. Gas turbine engine with separate core and propulsion unit. USP2014078789354.
  25. Wolkovitch Julian (2109 Prestonwood Dr. Arlington TX 76012). Joined wing aircraft. USP1982124365773.
  26. Frediani Aldo,ITX. Large dimension aircraft. USP1999055899409.
  27. Cros, Christophe. Low-noise aircraft, particularly at take-off and landing. USP2011128074924.
  28. Ribarov, Lubomir A.; Gieras, Jacek F.. Magnetically coupled contra-rotating propulsion stages. USP2013068464511.
  29. Finch Thomas (San Antonio TX). Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies. USP1982014311289.
  30. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2015109162755.
  31. Rodger L. Modglin ; Frederick H. Peters. Pivot fairing thrust reverser. USP2002126487845.
  32. Lair, Jean-Pierre. Pivoting door thrust reverser for a turbofan gas turbine engine. USP2012058172175.
  33. Gustafsson, Bernhard. Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine. USP2010077753311.
  34. Brislawn Mark G.. Pylon flap for increasing negative pitching moments. USP1998075779191.
  35. Norris, Jams W.; Epstein, Alan; Roberge, Gary D.; Costa, Mark W.; Berryann, Andrew P.; Kupratis, Daniel B.. Reversed-flow core for a turbofan with a fan drive gear system. USP2012058176725.
  36. Wagenfeld Robert E. (New York NY). System for reducing aircraft noise and hush kit. USP1989064836469.
  37. Lair, Jean-Pierre. Thrust reverser. USP2011118051639.
  38. Aten, Michael Ray; Crawford, Sara Christine. Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion. USP2012028109466.
  39. Marshall, Richard M.; Gukeisen, Robert L.. Tri-body variable area fan nozzle and thrust reverser. USP2012018104261.
  40. Rolt, Andrew M.. Turbofan arrangement. USP2010087770377.
  41. Lillibridge Robert W. ; McGuire Kenneth R. ; Phillips Edward J. ; Matthews Eugene James. Turbofan engine with reduced noise. USP1999085943856.
  42. Williams Samuel B.. Twin engine aircraft. USP1999095957405.
  43. Williams Samuel B.. Twin engine aircraft. USP2001036199795.
  44. Strumbos William P. (85 Middleville Rd. Northport NY 11768). VTOL aircraft. USP1989024804155.
  45. Pero, Edward B.. Variable area fan nozzle thrust reverser. USP2012048151551.
  46. Eiler, Donald C.; Larkin, Michael J.. Variable cycle boost propulsor. USP2005016837038.
  47. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J.. Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method. USP2012108276362.
  48. Ellis Roger R. (Wichita KS) Gertsen W. Marvin (Wichita KS) Conley Norman E. (Wichita KS). Wing with improved leading edge for aircraft. USP1980124240597.