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Nacelle anti-icing system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/04   
미국특허분류(USC) 244/134B ; 244/207 ; 60/39093
출원번호 US-0911881 (1986-09-26)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 65  인용 특허 : 0
초록
▼

A nacelle anti-icing system for a jet engine and a method for preventing icing of the nacelle. The nacelle anti-icing system includes a nose cowling assembly having a nose ring and an inlet duct connected to the nose ring, the nose ring including a plurality of openings formed therein; a nose cowling conduit positioned in the nose ring for communicating a heated gas to the plurality of openings formed in the nose ring and for creating a heated gas boundary layer on the inlet duct, and a mechanism connected to the nose cowling conduit for generating the h...

대표
청구항
▼

A nacelle anti-icing system for a jet engine, comprising: a nose cowling assembly which includes a nose ring and an inlet duct connected to said nose ring and having an inner and outer circumferential surface portion, said nose ring including a plurality of openings formed therein; nose cowling conduit means positioned in said nose ring for communicating a heated gas to said plurality of openings formed in said nose ring and for creating a heated gas boundary layer on said inner circumferential surface of said inlet duct and for communicating said heated...

이 특허를 인용한 특허 피인용횟수: 65

  1. Andre, Robert; Porte, Alain. Air inlet cowl for a jet engine, provided with deicing means. USP2003076585191.
  2. Chelin, Frédéric; Surply, Thierry; Bourdeau, Christophe. Air outlet system for aircraft leading edge. USP2013058434724.
  3. Tran, Hein. Air passage device. USP198907H000648.
  4. Saiz Manuel Munoz,ESX. Aircraft air conditioning energy recovery device. USP2000046045088.
  5. Wainfan Barnaby Sam ; Liu Yu Ping ; Rihn Daniel R. ; Leggett Douglas William ; Georges Martin James ; Philhower Jeffry Scott ; Shultz Douglas Ellwood ; Boccados Charles. Aircraft engine air intake system. USP2000106138950.
  6. Lumbab, Alex C.; Leisten, Bradley Scott. Aircraft engine nacelle bulkheads and methods of assembling the same. USP2017079708072.
  7. Saito, Isao; Ishiguro, Tatsuo; Abe, Shigeki; Tanaka, Hideaki; Takasu, Toru; Atsumi, Motohiro; Nakanishi, Masakazu; Kamogari, Minoru. Aircraft ice protection system and aircraft provided with the same. USP2015038967543.
  8. Zheng, Zhijun; Anderson, James H; Sanicki, Scott David. Aircraft nacelle anti-ice systems and methods. USP2018069994327.
  9. Porte, Alain; Chene, Gilles; Hormiere, Arnaud. Aircraft nacelle including an optimised ice treatment system. USP2013128602360.
  10. Porte, Alain; Chene, Gilles; Hormiere, Arnaud. Aircraft nacelle including hot air discharge means. USP2013058448901.
  11. DuPont, Henry Morgan. Airfoil anti-icing assembly and method. USP2004036702233.
  12. Prather, Randall Maurice; Cunningham, Neil Fraser; Jih, Junhaur; Krammer, Erich Alois; Subramanian, Sesha. Anti-ice splitter nose. USP2017109777632.
  13. Brand, Joseph Horace; Dowhan, Michael John. Anti-icing apparatus and method for aero-engine nose cone. USP2009097581378.
  14. Brand, Joseph Horace; Dowhan, Michael John. Anti-icing apparatus and method for aero-engine nose cone. USP2011098015789.
  15. Calder, David P.; Howarth, Graham. Anti-icing system and method for preventing ice accumulation. USP2015049004407.
  16. Laurant, Franck; Bellet, Francois; Joret, Jean-Philippe. Composite panel having a built-in duct. USP2016089410485.
  17. Knight, Glenn A; Maguire, Alan R; Robinson, Daniel; Bostock, George; Wilson, Mark J. Compressor tip injector. USP20181210145387.
  18. Lockwood, Clive. Engine arrangement. USP2011098011172.
  19. Hogate, Isaac Jon. Engine inlet ice protection system having embedded variable watt density heaters. USP2012128334486.
  20. Hogate, Isaac Jon. Engine inlet ice protection system with power control by zone. USP2011118049147.
  21. Cloft, Thomas G.; Wall, Sarah M.. Flow distribution system for inlet flow control. USP2010057708230.
  22. Olsen,Ronald F.; Breer,Marlin D.. Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods. USP2008027331421.
  23. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014098844294.
  24. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2013018353164.
  25. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014058726632.
  26. Tomeo, Peter V.; Anderson, Carney R.. Gas turbine engine nose cone attachment configuration. USP2017069682450.
  27. Winter, Michael; Jain, Ashok K.. Gas turbine engine system providing simulated boundary layer thickness increase. USP2012078209953.
  28. Pollard, Berwyn Owain; Scott, David Russell. Heat exhanger apparatus including heat transfer surfaces. USP2016029260191.
  29. Porte Alain,FRX. Hot air diffuser for a jet engine air inlet cowl with de-icing circuit. USP2000066079670.
  30. Linton, Alan. Ice protection system. USP2005026848656.
  31. De Souza, Francisco José ; Trapp, Luis Gustavo. Icing protection for aircraft air inlet scoops. USP2011077975966.
  32. Richardson, Giles Anthony; MacManus, David; Sheaf, Christopher Thomas John. Intake liner for a gas turbine engine. USP2015018931252.
  33. Kobayashi Takashi,JPX ; Banno Michihiko,JPX ; Amaoka Kazuaki,JPX. Leading edge structure of aircraft airfoil and method of fabricating the same. USP2000096119978.
  34. Lumbab, Alex C.; Leisten, Bradley Scott. Lipskin for a nacelle and methods of making the same. USP2017059656761.
  35. Rocklin, Mark; Karvountzi, Georgia C.; Hummel, Daniel S.. Method and apparatus for aircraft anti-icing. USP2011118061657.
  36. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L.. Method and apparatus for aircraft inlet ice protection. USP2004026688558.
  37. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel. Method and apparatus for aircraft inlet ice protection. USP2002046371411.
  38. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel. Method and apparatus for aircraft inlet ice protection. USP2002106457676.
  39. Shah, Anil D.; Gupta, Alankar. Method and apparatus for detecting conditions conducive to ice formation. USP2009127628359.
  40. Shah,Anil D.; Gupta,Alankar. Method and apparatus for detecting conditions conducive to ice formation. USP2007027175136.
  41. Friddell,Stephen D.; Prichard,Alan K.. Method and apparatus for liquid containment, such as for aircraft fuel vessels. USP2006087090167.
  42. Crouch Jeffrey D. ; Ng Lian L.. Method and apparatus using localized heating for laminar flow. USP2000026027078.
  43. Kobayashi Takashi,JPX ; Banno Michihiko,JPX ; Amaoka Kazuaki,JPX. Method of making a leading edge structure of aircraft airfoil. USP2001086279228.
  44. Lumbab, Alex C.; Leisten, Bradley Scott. Methods and apparatus for noise attenuation in an engine nacelle. USP2017039604438.
  45. Cook, Donald E.; Feider, Michael P.. Methods and systems for detecting icing conditions. USP2014048711008.
  46. Mercier, Claude; Collopy, Gary. Nacelle anti-ice valve utilized as compressor stability bleed valve during starting. USP2018019879599.
  47. Jain, Ashok K.; Winter, Michael. Nacelle assembly having inlet airfoil for a gas turbine engine. USP2013048408491.
  48. Haas, Martin. Nacelle assembly having inlet bleed. USP2012068192147.
  49. Haas, Martin. Nacelle assembly with turbulators. USP2012058186942.
  50. Cloft, Thomas G.; Jain, Ashok K.. Nacelle compartment plenum for bleed air flow delivery system. USP2014028657567.
  51. Jain, Ashok K.. Nacelle flow assembly. USP2013128596573.
  52. Jain, Ashok K.. Nacelle flow assembly. USP2012108282037.
  53. Jain, Ashok K.. Nacelle flow assembly. USP2015049004399.
  54. Porte, Alain; Lalane, Jacques. Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together. USP2016059352844.
  55. Atassi, Oliver V.. Nacelle with porous surfaces. USP2015038974177.
  56. Moscatelli, Antonio; Mancuso, Gianni. Nacelles for aircraft engines with de-icing systems using a two-phase fluid. USP20180710017260.
  57. Lumbab, Alex C.; Lan, Justin Honshune; Leisten, Bradley Scott. Noise attenuating lipskin assembly and methods of assembling the same. USP2018049938852.
  58. Porte, Alain. Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same. USP2004036698691.
  59. Mackin, Steve; Fisher, Robert Earl. Systems and methods for preventing ice formation on portions of an aircraft. USP20190110189572.
  60. Gregory, Karl; Sheppard, Michael James; Attrill, Scott. Thermal anti-icing system. USP2013048413930.
  61. Tindell Runyon H. ; Davis Warren ; Karanik James J.. Thin inlet lip design for low drag and reduced nacelle size. USP2001016179251.
  62. Surply, Thierry; Bourdeau, Christophe. Turbojet nacelle and method for controlling separation in a turbojet nacelle. USP2014028640986.
  63. Canadas Marc,FRX. Turbojet pod with laminar flow. USP2001016179249.
  64. Calder, David Patrick. Turbomachine nacelle and anti-icing system and method therefor. USP2013028382039.
  65. Jain, Ashok K.; Chaudhry, Zaffir A.. Variable shape inlet section for a nacelle assembly of a gas turbine engine. USP2013038402739.

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