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특허 상세정보

Mission adaptive inlet

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64B-001/24    B64C-001/38    B64D-015/00    F02B-027/00   
미국특허분류(USC) 24/405.3B ; 24/413.0 ; 24/413.4R ; 13/701.51
출원번호 US-0898162 (1997-07-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Harness Dickey & Pierce P.L.C.
인용정보 피인용 횟수 : 49  인용 특허 : 21
초록

A mission adaptive inlet (42) for an aircraft (40) has a rigid lip panel (56) pivotally attached to an inlet (42) of the aircraft (40). An actuation mechanism is coupled to the rigid lip panel (56) and causes the rigid lip panel (56) to pivot from a first position to a second position. A reinforced elastomer system (48) is connected the rigid lip panel and the inlet (42).

대표
청구항

[ What is claimed is:] [1.] A mission adaptive inlet for providing air to a jet engine of an aircraft comprising:a rigid lip panel pivotally attached to an inlet of the aircraft;an actuation mechanism coupled to the rigid lip panel and causing the rigid lip panel to pivot from a first position to a second position; anda reinforced elastomer system connected to the rigid lip panel and the inlet, the reinforced elastomer section including an elastomeric skin capable of elastic elongation and having a plurality of rods sliding freely inside the elastomer sk...

이 특허에 인용된 특허 (21)

  1. Geiger Michael Watson ; Gruensfelder Cynthia Ann ; Jacobs Jack Howard. Active reinforced elastomer system. USP1999085931422.
  2. Maclean Brian J. (Daniel WY) Carpenter Bernard F. (Littleton CO) Misra Mohan S. (Golden CO). Adaptive control surface using antagonistic shape memory alloy tendons. USP1997095662294.
  3. Gruensfelder Cynthia Ann ; Geiger Micael Watson ; Jacobs Jack Howard ; Wille Robert Henry. Apparatus for eliminating gaps in an aircraft. USP1999115979828.
  4. Tindell Runyon H. (Old Bethpage NY). Blown boundary layer control system for a jet aircraft. USP1995095447283.
  5. Haas Jan T. (Hamburg DEX) Hadwin Robin-Leslie (Buxtehude DEX). Controllable diffuser for an air intake of an aircraft. USP1987024641678.
  6. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  7. Ellis James R. ; Diller Joseph B.. Expandable aircraft section. USP1998095803405.
  8. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry. Expandable fuel cell. USP1999075927651.
  9. Cameron Dean Emory. Fairing for an expandable bay. USP1999095947417.
  10. Smith David R. (West Haven CT) Amelio Armand F. (New Milford CT). Low observable engine air inlet system. USP1997125697394.
  11. Covey James H. (Snohomish WA). Method for plating one side of a woven fabric sheet. USP1990014892626.
  12. Beier Theodor Harry ; Haake John Martin ; Wille Robert Henry ; Jacobs Jack Howard. Reinforced elastomer panel with embedded strain and pressure sensors. USP1999045896191.
  13. Livingston David E. (Huntsville AL) Kornell Thomas J. (Federal Way WA). Single-piece, flexible inlet ramp. USP1991075033693.
  14. Syberg Jan (Kent WA). Supersonic inlet having variable area sideplate openings. USP1983024372505.
  15. Hamstra Jeffrey William ; Sylvester Thomas Gerard. System and method for diverting boundary layer air. USP1998075779189.
  16. Wille Robert Henry. Tail for an aircraft. USP1999095947422.
  17. Jabs Alfred (Groebenzell DEX). Turboramjet engine. USP1992035094071.
  18. Ball William Henderson (Mercer Island WA) Ishimitsu Kichio Keith (Mercer Island WA). Variable camber inlet for supersonic aircraft. USP1977034012013.
  19. Readnour Jack L. (Ft. Mitchell KY) Wright Jack D. (Mason OH). Variable contour annular air inlet for an aircraft engine nacelle. USP1991035000399.
  20. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.
  21. duPont Anthony A. (7946 Ivanhoe Ave. La Jolla CA 92037). Variable geometry duct seal. USP1993075226455.

이 특허를 인용한 특허 피인용횟수: 49

  1. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. AFT engine nacelle shape for an aircraft. USP2017119815560.
  2. Shammoh, Ali A. A. J.. Adjustable angle inlet for turbojet engines. USP2013108544793.
  3. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP2017119821917.
  4. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP20180710017270.
  5. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David. Aft engine for an aircraft. USP2018059957055.
  6. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Aircraft having an aft engine. USP2017059637217.
  7. Sakurai, Seiya; Fox, Stephen J.; Grimlund, Kristin E.. Apparatus and methods for varying inlet lip geometry of a jet engine inlet. USP2005066910327.
  8. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V.. Apparatus for variation of a wall skin. USP2003076588709.
  9. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Braking assembly and system. USP2003126655504.
  10. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Concealed air vents. USP2003066571820.
  11. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Container holder that utilizes moldline structures. USP2003046547117.
  12. John Cleveland Waldrop, III ES. Elastic ground plane. USP2002016337294.
  13. Behrens, William W.; Tucker, Andrew R.. Extended plug cold plate. USP2014058720828.
  14. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2010097797944.
  15. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014098844294.
  16. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2013018353164.
  17. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014058726632.
  18. Prasad, Dilip; Feng, Jinzhang; Sabnis, Jayant S.. Gas turbine engine inlet with noise reduction features. USP2010067739865.
  19. Prasad, Dilip; Feng, Jinzhang; Sabnis, Jayant S.. Gas turbine engine inlet with noise reduction features. USP2012108286654.
  20. Smith, Angus Roy; Arzoglou, Dimitris. Gas turbine engine nacelle having a symmetric flowpath. USP2016059328662.
  21. Smith, Angus Roy; Arzoglou, Dimitris. Gas turbine engine nacelle having a symmetric flowpath and design method thereof. USP2015038985507.
  22. Winter, Michael; Jain, Ashok K.. Gas turbine engine providing simulated boundary layer thickness increase. USP2011017870721.
  23. Winter, Michael; Jain, Ashok K.. Gas turbine engine system providing simulated boundary layer thickness increase. USP2012078209953.
  24. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2009087575195.
  25. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2005046877695.
  26. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2012028108980.
  27. Binks, Alan; James, Norman John; Layland, Michael John. Inlet section of an aircraft engine nacelle. USP2016089403599.
  28. Binks, Alan; James, Norman John; Layland, Michael John. Inlet section of an aircraft engine nacelle. USP2012098267642.
  29. Binks, Alan; James, Norman John; Layland, Michael John. Inlet section of an aircraft engine nacelle. USP2012068197191.
  30. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP2018059957889.
  31. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP2018049951690.
  32. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Low noise aeroengine inlet system. USP20180810054050.
  33. Cox, Brian N.; Davis, Janet B.; dos Santos e Lucato, Sergio Luis; Marshall, David B.; McCabe, Brock S.; Sudre, Olivier H.. Morphable ceramic composite skins and structures for hypersonic flight. USP2009047516918.
  34. Jain, Ashok K.; Winter, Michael. Nacelle assembly having inlet airfoil for a gas turbine engine. USP2013048408491.
  35. Haas, Martin. Nacelle assembly having inlet bleed. USP2012068192147.
  36. Haas, Martin. Nacelle assembly with turbulators. USP2012058186942.
  37. Jain, Ashok K.. Nacelle flow assembly. USP2013128596573.
  38. Jain, Ashok K.. Nacelle flow assembly. USP2012108282037.
  39. Jain, Ashok K.. Nacelle flow assembly. USP2015049004399.
  40. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Non-axis symmetric aft engine. USP2018029884687.
  41. Madsen, Casey Lyn. Shape memory alloy rods for actuation of continuous surfaces. USP2015119174723.
  42. Quackenbush, Todd R.; McKillip, Jr., Robert M.; Danilov, Pavel V.. Supersonic engine inlet diffuser with deployable vortex generators. USP2016089429071.
  43. Weir, James William; Springett, Frank Benjamin; Ensley, Eric Trevor. System and method for sealing a wellbore. USP2013108544538.
  44. Jain, Ashok K.; Winter, Michael. Variable contour nacelle assembly for a gas turbine engine. USP2016019228534.
  45. Jain, Ashok K.; Winter, Michael. Variable contraction ratio nacelle assembly for a gas turbine engine. USP2014058727267.
  46. Lamb, Jr., Donald William. Variable geometry helicopter engine inlet. USP2017059656760.
  47. Labrecque, Michel; Couture-Gagnon, Vincent; Ullyott, Richard. Variable geometry inlet system. USP20190310221764.
  48. Jain, Ashok K.. Variable geometry nacelle assembly for a gas turbine engine. USP2012068205430.
  49. Jain, Ashok K.; Chaudhry, Zaffir A.. Variable shape inlet section for a nacelle assembly of a gas turbine engine. USP2013038402739.