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특허 상세정보

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내보내기 페이스북 공유 카카오톡 공유

Active clearance control system for a turbomachine

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-025/14   
미국특허분류(USC) 415/145 ; 415/178 ; 60/726 ; 60/3929
출원번호 US-0060449 (1979-07-25)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 64  인용 특허 : 7
초록
▼

An axial compressor is provided with a cooling air manifold surrounding a portion of the shroud, and means for bleeding air from the compressor to the manifold for selectively flowing it in a modulating manner axially along the outer side of the stator/shroud to cool and shrink it during steady-state operating conditions so as to obtain minimum shroud/rotor clearance conditions. Provision is also made to selectively divert the flow of cooling air from the manifold during transient periods of operation so as to alter the thermal growth or shrink rate of t...

대표
청구항
▼

An improved clearance control system for a turbomachine including a compressor of the type having a plurality of rotor stages surrounded in close radial relationship by a stator structure, wherein the improvement comprises: (a) means for introducing the flow of cooling air along an axial path at the outer surface of said stator structure to inhibit thermal growth thereof, said flow-introducing means including means for bleeding motive fluid from said compressor; and (b) means for selectively diverting the flow of cooling air from said axial path during p...

이 특허에 인용된 특허 (7)

  1. Bobo Melvin (Cincinnati OH). Bleed air manifold. USP1976033945759.
  2. Redinger ; Jr. ; Ira H. ; Sadowsky ; David ; Stripinis ; Philip S.. Clearance control for gas turbine engine. USP1978014069662.
  3. Hallinger Claude Christian (L\Hay-les-Roses FR) Kervistin Robert (Melun FR). Device for regulating turbine blade tip clearance. USP1976083975901.
  4. Redinger ; Jr. Ira H. (Vernon CT) Sadowsky David (South Windsor CT) Stripinis Philip S. (South Windsor CT). External gas turbine engine cooling for clearance control. USP1977044019320.
  5. Schwarz Frederick M. (Glastonbury CT). Seal clearance control system for a gas turbine. USP1980074213296.
  6. Patterson William R. (Cincinnati OH). Thermal actuated valve for clearance control. USP1976063966354.
  7. Patterson ; William R.. Variable shroud for a turbomachine. USP1978114127357.

이 특허를 인용한 특허 피인용횟수: 64

  1. Davison Samuel H. (Loveland OH) Kast Kevin H. (Cincinnati OH) Clark Aidan W. (Blue Ash OH). Active clearance control. USP1990054928240.
  2. Putman Robert L. (Bolton CT) Dinse Merle L. (S. Windsor CT). Active clearance control. USP1987034648241.
  3. Weiner Harvey I. (South Windsor CT) Allard Kenneth L. (Wilbraham MA). Active clearance control. USP1986034576547.
  4. Schimmels, Scott Alan; Fusinato, Daniel John; Glessner, John Carl; Mirkovich, Dan Nicholas; Proctor, Robert. Active clearance control manifold system. USP2016059341074.
  5. Legare, Pierre-Yves; Mah, Stephen. Active tip clearance control arrangement for gas turbine engine. USP2012018092146.
  6. Gekht, Eugene; Lucas, Terrence; Haslam-Jones, Thomas Francis; Mills, Danny; Bouchard, Guy. Active turbine or compressor tip clearance control. USP2017039598974.
  7. Tatebayashi, Yasushi. Air-bleed gas turbine. USP2010097788931.
  8. Stadler, Michael; Braeutigam, Ralf. Aircraft with an engine having a by-pass air inlet opening and a bleed air outlet. USP2018029902500.
  9. Willkop Franz (Munich DEX) Zaehring Gerhard (Woerthsee DEX) Popp Joachim (Dachau DEX) Ruetsch Robert (Karlsfed DEX). Apparatus for optimizing the blade and sealing slots of a compressor of a gas turbine. USP1988014719747.
  10. Albrecht Richard W. (Fairfield OH) Shepherd Andrew (Fairfield OH). Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud. USP1993125273396.
  11. Takahashi, Yasuo; Myoren, Chihiro; Kawamura, Kohta. Axial compressor and gas turbine having axial compressor. USP2017059644642.
  12. Khanin, Alexander Anatolievich; Kostege, Valery. Axial flow gas turbine. USP2015038974174.
  13. Wright William B. (Leicester GB2) Flatman Richard J. (Derby GB2). Blade tip clearance control. USP1987084683716.
  14. Mark Stewart Schroder. Bucket tip clearance control system. USP2002086435823.
  15. Schwarz Fred M. (Glastonbury CT) Crawley ; Jr. Clifton J. (Glastonbury CT) Rausco Anthony (Middletown CT) Lagueux Ken R. (Berlin CT). Clearance control method for gas turbine engine. USP1991045005352.
  16. Davison Samuel H. (Milford OH) McGreehan William F. (Westchester OH). Clearance control system. USP1990014893984.
  17. McGreehan William F. (Westchester OH). Clearance control system. USP1990014893983.
  18. Klingels, Hermann. Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine. USP2014038678742.
  19. Kendrick, Donald W.. Combustion cavity layouts for fuel staging in trapped vortex combustors. USP2014048689562.
  20. Charon, Christophe; Cook, Graëme; Garcia, Grégory; Kapala, Patrick; Lippinois, Eric; Loudet, Claude; Marois, Fabrice; Pham, Lucien; Raulin, Dominique. Compressor air drawing off system. USP2004086782702.
  21. Dierksmeier, Douglas David; Grant, Steven Lester; Muskat, James Christopher. Compressor tip clearance control and gas turbine engine. USP2016109458855.
  22. Mojem, Mats; Scholz, Andreas. Device and method for bleeding compressor air in a turbofan engine. USP20180910077719.
  23. Aschenbruck, Emil; Ebbing, Hildegard; Mohr, Klaus Dieter. Device for cooling a component subject to temperature stress of nonuniform intensity. USP2003056568902.
  24. Montgomery, Michael E.. Diaphragm shell structures for turbine engines. USP2014038662831.
  25. Seitz, Peter A.. Flow structure for a turbocompressor. USP2009107600965.
  26. Beecroft, Peter. Gas bleed arrangement. USP20190110174681.
  27. Laurello, Vincent; Yuri, Masanori. Gas turbine compressor and clearance controlling method therefor. USP2004056732530.
  28. Pinero, Hector M.; Peroulakis, George N.. Gas turbine engine case for clearance control. USP2013058434997.
  29. Dougan, Jr., Donald; Carminati, Daniel; Wang, Cheng-Zhang. Gas turbine engine outer case with contoured bleed boss. USP2016129528391.
  30. Pritchard, Jr., Byron Andrew; Califf, Charles Daniel; Wood, Peter John; Holm, Raymond Gust; van de Wall, Allan George; Pezzi, Peter Alfred. Gas turbine engine variable bleed valve for ice extraction. USP2018059982598.
  31. Urban, Justin R.; Bifulco, Anthony R.. Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events. USP2018029890711.
  32. Anatoly Rakhmailov RU. Gas turbine engine with exhaust compressor having outlet tap control. USP2002066397576.
  33. Khanin, Alexander Anatolievich; Kostege, Valery. Gas turbine of the axial flow type. USP2015038979482.
  34. Ballard, Jr., Henry G.; Beadie, Douglas Frank; Memmer, John David. Method and apparatus for clearance control utilizing fuel heating. USP2018059963994.
  35. Morgan, Rex Allen; Davi, Michael Alan; Gazzillo, Clement; Jordan, Harold Lamar. Method and apparatus for gas turbine engine temperature management. USP2014058714906.
  36. Liebl Josef (Dachau DEX). Method and apparatus for optimizing the vane clearance in a multi-stage axial flow compressor of a gas turbine. USP1989014795307.
  37. Down, Andrew; Nilsson, Ulf. Method and device for cooling a component of a turbine. USP2012098257017.
  38. Kendrick, Donald W.. Method of fuel staging in combustion apparatus. USP2013108549862.
  39. Plunkett, Timothy T.; Hershey, John E.; Osborn, Brock E.; Seitzer, Kenneth E.; Taylor, Keith K.. Method, system, and apparatus for reducing a turbine clearance. USP2012108296037.
  40. Palmer Donald L.. Passive turbine coolant regulator responsive to engine load. USP1999125996331.
  41. LeBlanc, Ryan Edward; Cummings, Kevin J.; Ali, Amr. Reduced height ligaments to minimize non-integral vibrations in rotor blades. USP2016079394792.
  42. Sexton Brendan F. ; Knuijt Hans M. ; Eldrid Sacheverel Q. ; Myers Albert ; Coneybeer Kyle E. ; Johnson David Martin ; Kellock Iain R.. Removable inner turbine shell and bucket tip clearance control. USP2000066079943.
  43. Sexton Brendan F. (Clifton Park NY) Knuijt Hans M. (Niskayuna NY) Eldrid Sacheverel Q. (Saratoga Springs NY) Myers Albert (Amsterdam NY) Coneybeer Kyle E. (Schenectady NY) Johnson David Martin (Balls. Removable inner turbine shell with bucket tip clearance control. USP1997115685693.
  44. Sexton Brendan F. ; Knuijt Hans M. ; Eldrid Sacheverel Q. ; Myers Albert ; Coneybeer Kyle E. ; Johnson David Martin ; Kellock Iain R.. Removable inner turbine shell with bucket tip clearance control. USP2000076082963.
  45. Sexton Brendan F. ; Knuijt Hans M. ; Eldrid Sacheverel Q. ; Myers Albert ; Coneybeer Kyle E. ; Johnson David Martin ; Kellock Iain R.. Removable inner turbine shell with bucket tip clearance control. USP1999065913658.
  46. Sexton Brendan F. ; Knuijt Hans M. ; Eldrid Sacheverel Q. ; Myers Albert ; Coneybeer Kyle E. ; Johnson David Martin ; Kellock Iain R.. Removable inner turbine shell with bucket tip clearance control. USP1999055906473.
  47. Sexton Brendan F. ; Knuijt Hans M. ; Eldrid Sacheverel Q. ; Myers Albert ; Coneybeer Kyle E. ; Johnson David Martin ; Kellock Iain R.. Removable inner turbine shell with bucket tip clearance control. USP1998075779442.
  48. Hagi Naoki,JPX. Seal active clearance control system for gas turbine stationary blade. USP2000116152685.
  49. Rioux, Philip Robert; Saftler, Rishon. Splitter for air bleed manifold. USP20180710018118.
  50. Sakai, Yusuke; Ikeguchi, Takuya; Terauchi, Koji. Structure for extracting compressed air from compressor of gas turbine engine and gas turbine engine with the structure. USP2016039291099.
  51. Klasing, Kevin Samuel; Albrecht, Jr., Richard William; Powell, Brandon Flowers; Marusko, Mark Willard; Venzon, Anthony; Wallace, Thomas Ryan. Suction-based active clearance control system. USP20180710018067.
  52. Haddad Donald E. (Amston CT) Pereiras ; Jr. Emilio (Shelton CT). Synthesized feedback for gas turbine clearance control. USP1991034999991.
  53. Carlucci, Gregory C.; Knight, Glenn Alexander; Rumbo, Jim; Loots, Dennis D; Peckham, Roger; Bacic, Marko; Haberstock, James Kenneth. System and method for turbine blade clearance control. USP20190110184348.
  54. Boris Karpman ; John L. Shade ; Daniel E. Kane. System and method of controlling clearance between turbine engine blades and case based on engine components thermal growth model. USP2002116487491.
  55. Paprotna,Hubert Edward; Foust,Adam Matthew. System for actively controlling compressor clearances. USP2008107434402.
  56. Kervistin Robert (Lee Mee Sur Seine FRX). System for adjusting radial clearance between rotor and stator elements. USP1989074849895.
  57. Klingler, Brett Darrick. Turbine assembly and method for supporting turbine components. USP2015038967951.
  58. Chehab, Abdullatif M.. Turbine blade tip clearance control. USP2010057708518.
  59. Joe, Christopher R.; Ward, Daniel A.. Turbine blade tip clearance control. USP2017059644490.
  60. Joe, Christopher R.; Ward, Daniel A.. Turbine blade tip clearance control. USP2016059347334.
  61. Böck, Alexander. Turbo engine. USP2013128608435.
  62. Franconi, Robert B.; Goodman, Robert B.; MacDonald, Scott R.; Mazzone, Paul. Turbofan jet engine having a turbine case cooling valve. USP2005066910851.
  63. Weiner Harvey I. (South Windsor CT). Valve and manifold for compressor bore heating. USP1987024645416.
  64. Kendrick, Donald W.. Vortex premixer for combustion apparatus. USP2014048689561.

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