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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Internally ventilated noise suppressor with large plug nozzle

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/04    F01N-001/14    F02K-001/08   
미국특허분류(USC) 239/26513 ; 239/26529 ; 239/26531 ; 181/215
출원번호 US-0405962 (1982-03-17)
국제출원번호 PCT/US82/00327 (1982-03-17)
§371/§102 date 19820317 (19820317)
국제공개번호 WO-8303281 (1983-09-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 44  인용 특허 : 5
초록
▼

A jet engine noise suppressor particularly adapted for supersonic aircraft. The nozzle (10) has an internal wall surface (70) around a generally centrally positioned body (50) and an annular area (62) extending between the wall and the body. In this area there are separate gas and air flow ducts (64, 66) having entrance ends (82, 80) and exit ends (76, 78), the entrance ends of the gas ducts extending annularly around the body (50) to receive gas exhaust from the engine and the air ducts have entrance ends annularly outwardly of the gas ducts along the w...

대표
청구항
▼

In a jet engine nozzle adapted to exhaust a propulsive gas jet, said nozzle having wall means longitudinally bounding a generally centrally positioned body, and an annular area extending between said wall means and said body, an improved jet engine noise suppressor in said nozzle comprising: separate first and second ducts having adjacent annular cross secions at entrance ends and exit ends, said ducts extending longitudinally through a portion of said annular area; said first and second ducts being shaped and arranged to invert flow patterns through the...

이 특허에 인용된 특허 (5)

  1. Rabone George R. (Cincinnati OH). Convergent-divergent plug nozzle. USP1977054026472.
  2. Klees ; Garry W.. Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine. USP1978044085583.
  3. Klees Garry W. (Mercer Island WA). Multicycle engine. USP1976023938328.
  4. Klees Garry W. (Mercer Island WA). Simplified method and apparatus for hot-shield jet noise suppression. USP1981094291782.
  5. Pedersen George H. (Indianapolis IN). Variable cycle gas turbine engine. USP1977104054030.

이 특허를 인용한 특허 피인용횟수: 44

  1. Beardsley, Peter K; Knight, Glenn A. Aeroengine thrust reverser. USP2011017866142.
  2. Letay, Benoit; Saget, Benjamin; Lesieur, Franck; Flin, Stephane. Aircraft nacelle that incorporates a thrust reversal device. USP2014048701386.
  3. Baker, Von David. Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle. USP2013068459036.
  4. Ress, Robert A. Aircraft with gas turbine engine having outer bypass elements removed. USP2018019863368.
  5. Presz ; Jr. Walter M. ; Reynolds Gary. Alternating lobed mixer/ejector concept suppressor. USP1999035884472.
  6. John J. Dugan. Apparatus for reducing noise in the jet engine. USP2002086427801.
  7. Brice,David C.; Whitmire,Julia K.; Barton, deceased,Brian E.. Apparatus, method and system for gas turbine engine noise reduction. USP2007017159383.
  8. Makowski, Maciej D.; Vasquez, David A.. Articulated diffuser and door for submerged ram air turbine power and cooling control. USP20181010094336.
  9. Bellanger, Alexandre; Bouillon, Florent; Dubois, Laurent. Beam for a cascade thrust reverser. USP2016059341142.
  10. Dussillols, Laurent; Vuillemin, Alexandre Alfred Gaston. Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft. USP2010107810335.
  11. Batey J. Gary. Core flow expansion chamber device system for reduction of jet turbine engine noise. USP1998065758488.
  12. Huber, Jerome; Bonnet, Jean-Paul; Delville, Joel; Jordan, Peter; Strekowski, Francois. Device for reducing noise generated by an aircraft jet engine with curve ducts. USP2012048157050.
  13. Zysman Steven H. (Middletown CT) Lord Wesley K. (Glastonbury CT) Barber Thomas J. (West Hartford CT). Double lobed mixer with major and minor lobes. USP1997065638675.
  14. Marshall, Richard M.. Dual function cascade integrated variable area fan nozzle and thrust reverser. USP2017099759158.
  15. Newton Arnold C,GBX. Ducted fan gas turbine engine with variable area fan duct nozzle. USP2000066070407.
  16. Moore, Matthew D.; Marques, Edward C.. Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines. USP20181010094334.
  17. Sloan, Mark L.; Marques, Edward C.; Moore, Matthew D.; Bigbee-Hansen, William J.. Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines. USP2010077762057.
  18. Clark, Larry T.. Jet blade ejector nozzle. USP2003126662548.
  19. Torkelson Delbert W. (Claremore OK). Jet engine noise suppression system. USP1990034909346.
  20. Mengle, Vinod G.. Jet engine nozzle exit configurations and associated systems and methods. USP2011067966824.
  21. Mengle, Vinod G.. Jet engine nozzle exit configurations and associated systems and methods. USP2013088511090.
  22. Moore, Matthew D.; Boren, Kelly L.; Shen, Hao; Nelson, Chester P.. Jet noise suppressor. USP2017099758254.
  23. Dehu,Michel Philippe; Lore,Xavier Raymond Yves. Locking system on a cascade thrust reverser. USP2006037007454.
  24. Newell John Keith ; Zwernemann Gregory Richard. Mechanism of noise suppression system for a supersonic aircraft. USP1998095801341.
  25. Papamoschou Dimitri (Mission Viejo CA). Method of eliminating mach waves from supersonic jets. USP1997015590520.
  26. Zysman Steven H. ; Lord Wesley K. ; Barber Thomas J.. Method of noise suppression for a turbine engine. USP1998075775095.
  27. Howe, Mark E.. Method of varying a fan duct nozzle throat area of a gas turbine engine. USP2015028959889.
  28. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Nozzle arrangement and method of making the same. USP201903RE47304.
  29. Dionne, Luc. Passive cooling system for auxiliary power unit installation. USP2017059644538.
  30. Howe, Mark E.. Pivoting fan nozzle nacelle. USP2012038127532.
  31. Sheoran,Yogendra Y.; Payne,Roger I.. System and method for dumping surge flow into eductor primary nozzle for free turbine. USP2006127152410.
  32. Birch, Stanley F.; Secundov, Alexander N.; Lyubimov, Dmitriy A.; Khritov, Konstantin M.; Maslov, Vladimir P.; Mironov, Aleksey K.. Systems and methods for passively directing aircraft engine nozzle flows. USP2011017870722.
  33. Birch, Stanley F.; Secundov, Alexander N.; Lyubimov, Dmitriy A.; Khritov, Konstantin M.; Maslov, Vladimir P.; Mironov, Aleksey K.. Systems and methods for passively directing aircraft engine nozzle flows. USP2012058166768.
  34. Lausten, Merlyn; Bulman, Melvin J.. Thrust augmentation in plug nozzles and expansion-deflection nozzles. USP2010117823376.
  35. Sheoran, Yogendra Y.; Brown, Daniel V.; Edmonds, David H.. Tortuous path quiet exhaust eductor system. USP2003096615576.
  36. Su Michael W. ; Podleski Steve D. ; Gally Thomas A. ; Newsum Sean A.. Turbo fan engine nacelle exhaust system with concave primary nozzle plug. USP2001016178740.
  37. Kohlenberg, Gregory A.. Turbofan engine having inner fixed structure including ducted passages. USP2012108286415.
  38. Moore, Matthew D.; Marques, Edward C.. Turbofan engine with variable exhaust cooling. USP2017029574518.
  39. Weir, Don; Sheoran, Yogendra Yogi; Hollingshead, Doug; Hall, Peter. Turboprop engine systems with noise reducing inlet assemblies. USP2015069057329.
  40. Presz ; Jr. Walter M.. Two-stage mixer ejector suppressor. USP1998065761900.
  41. Duesler Paul W. ; Loffredo Constantino V. ; Prosser ; Jr. Harold T. ; Jones Christopher W.. Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems. USP1998075778659.
  42. Lair, Jean-Pierre. Variable area plug nozzle. USP2005016845607.
  43. Dussillols, Laurent Christophe; Longeville, Olivier Roland; Vuillemin, Alexandre Alfred Gaston. Variable-section flow mixer for a double-flow turbojet for a supersonic airplane. USP2010117827802.
  44. Lair,Jean Pierre. Ventilated confluent exhaust nozzle. USP2006037010905.

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