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특허 상세정보

Shroud segment and assembly with surface recessed seal bridging adjacent members

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-011/08   
미국특허분류(USC) 415/138; 415/139; 415/173.1; 415/200
출원번호 US-0325779 (2002-12-20)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 24  인용 특허 : 19
초록

A turbine engine shroud segment is provided with a radially outer surface including a pair of spaced apart, opposed first and second edge portion surface depressions, for example spaced circumferentially, having a seal surface shaped to receive, in a surface depression formed between assembled adjacent segments in a shroud assembly, or axially assembled adjacent segments and engine members, a radially outer fluid seal member. The depression portions of a shroud segment are joined with the radially outer surface of the shroud segment through an arcuate tr...

대표
청구항

1. A turbine engine shroud segment comprising a shroud segment body having a radially outer surface extending at least between a pair of first and second spaced apart, opposed outer surface end portions, wherein at least one of the first and second outer edge portions of the radially outer surface in the pair includes a surface depression portion including a depression portion seal surface of a first shape along the depression portion, the depression portion seal surface joined with the shroud body radially outer surface through an arcuate transition sur...

이 특허에 인용된 특허 (19)

  1. Draskovich Barry S.. Ceramic airfoil. USP1999126000906.
  2. Widrig, Scott M.; Morrison, Jay; Albrecht, Harry A.; Shteyman, Yevgeniy; Butner, Steven C.. Ceramic matrix composite turbine vane. USP2003116648597.
  3. Carrier Gilles (Ville Lemoyne CAX) Stoten Michael D. (Oakville CAX) Szwedska Patrick (Mississauga CAX). Ceramic stator vane assembly. USP1988094768924.
  4. Darkins ; Jr. Toby G. ; Shelton Monty L. ; Doughty Roger L. ; Noe Mark E.. Ceramic turbine airfoils with cooled trailing edge blocks. USP2001126325593.
  5. Booher ; Jr. Claude R. (West Chester PA) Rahaim Thomas J. (Claymont DE). Ceramic-to-metal (or ceramic) cushion/seal for use with three piece ceramic stationary vane assembly. USP1976063966353.
  6. Maier Horst R. (Selb DEX) Krauth Axel (Selb DEX) Pohlmann Hans-Juergen (Selb DEX) Nink Horst (Selb DEX) Brobeck Helmut (Hessheim DEX) Cropp Ingo (Frankenthal DEX) Bergmeier Dieter (Heidelberg DEX). Element and method for connecting ceramic and metallic parts. USP1982044325647.
  7. Landis ; Jr. Delmer H. (Loveland OH) Thomas ; Jr. Theodore T. (Loveland OH) Haap Charles J. (Cincinnati OH). Floating seal for a variable area turbine nozzle. USP1980034193738.
  8. Hayton Paul R. (Watford GB2). Gas turbine engines. USP1992075129783.
  9. Matyscak Kamil (Brenden DEX). Guide wave suspension for an axial-flow turbomachine. USP1995025387082.
  10. Lee Ching-Pang. Internally grooved turbine wall. USP2000116142734.
  11. Proctor Robert (West Chester OH) Linger David R. (Cincinnati OH) Di Salle David A. (West Chester OH) Brassfield Steven R. (Cincinnati OH) Plemmons Larry W. (Fairfield OH). Isolated turbine shroud. USP1996105562408.
  12. Predmore, Daniel Ross. Overlapping interference seal and methods for forming the seal. USP2003016503051.
  13. Nichols Herbert E. (Cincinnati OH). Rotor blade shroud segment. USP1991125071313.
  14. Hagle Michael P. (Mason OH). Seal assembly for segmented turbine engine structures. USP1991125074748.
  15. Edward Isaac Cohen. Split face mechanical seal system. USP2002076412784.
  16. Noe, Mark Eugene; Darkins, Jr., Toby George; Doughty, Roger Lee. Tangential flow baffle. USP2003046554563.
  17. Bagepalli Bharat Sampathkumaran ; Corman Gregory Scot ; Dean Anthony John ; DiMascio Paul Stephen ; Mirdamadi Massoud. Turbine assembly containing an inner shroud. USP2000096113349.
  18. Wygle Thomas G. (Loveland OH) Fargher David G. W. (Fairfield OH) Piekarski Arthur J. (Middletown OH). Turbine rotor disk post cooling system. USP1995025388962.
  19. Walker Alan (Wyoming OH) Wakeman Thomas G. (Lawrenceburg IN) Lenahan Dean T. (Cincinnati OH) Plemmons Larry W. (Fairfield OH) Elovic Andrew P. (Rishon Lezion ILX). Turbine shroud clearance control assembly. USP1992075127793.

이 특허를 인용한 특허 피인용횟수: 24

  1. Kerns, Daniel Patrick; Reynolds, Brandon ALlanson. Airfoil fluid curtain to mitigate or prevent flow path leakage. USP20190410253643.
  2. Nakamura, Ikuo; Waki, Kunihiko. Assembling method of stator blade ring segment, stator blade ring segment, coupling member, welding method. USP2012078215904.
  3. McCaffrey, Michael G.; Hudson, Eric A.. Blade clearance control using high-CTE and low-CTE ring members. USP2014078790067.
  4. Jarmon, David C.; Smith, Peter G.. Ceramic matrix composite combustor vane ring assembly. USP2016059335051.
  5. Merrill, Gary B.; Morrison, Jay A.. Compressible ceramic seal. USP2012038132442.
  6. Race, Nathan Stafford; Potter, Brian Denver. Compressor fairing segment. USP2016129528376.
  7. Cairo,Ronald Ralph; Bruce,Kevin Leon; Farrell,Thomas Raymond. Damper seal system and method. USP2007077238002.
  8. Jarmon, David C.; Butler, Shaoluo L.. Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key. USP2014068739547.
  9. Tholen, Susan M.; Lutjen, Paul M.. Gas turbine engines and related systems involving blade outer air seals. USP2012068206092.
  10. Morrison, Jay A.. Grid ceramic matrix composite structure for gas turbine shroud ring segment. USP2012028118546.
  11. Shapiro, Jason David. Method and system for a ceramic matrix composite shroud hanger assembly. USP2018019874104.
  12. Roberts, III, Herbert Chidsey; Bruce, Kevin Leon; Blow, Gerald Kent; Cairo, Ronald Ralph. Methods and apparatus for assembling turbine engines. USP2009077556475.
  13. Shapiro, Jason David; Desander, Donald Brett; Vickers, Edward Charles. Methods and assemblies for attaching airfoils within a flow path. USP20190410253641.
  14. Shapiro, Jason David; Reynolds, Brandon ALlanson; Baldiga, Jonathan David. Methods and features for positioning a flow path inner boundary within a flow path assembly. USP20190410247019.
  15. Franks, Michael John; Shapiro, Jason David; Rulli, Samuel Ross; Doughty, Roger Lee. Mounting apparatus for low-ductility turbine shroud. USP2017089726043.
  16. Strock, Christopher W.; Tholen, Susan M.. Oriented fiber ceramic matrix composite abradable thermal barrier coating. USP2011027887929.
  17. Shi, Jun; Jarmon, David C.; Hoffman, Lee A.; Bombara, David J.; Butler, Shaoluo L.; Prociw, Lev A.; Kojovic, Aleksandar. Reverse flow combustor duct attachment. USP2014108864492.
  18. Dev, Bodhayan; Meyer, Robert Carl; Sarawate, Neelesh Nandkumar; Albert, Jason Edward; Itzel, Gary Michael. Seal assembly to seal corner leaks in gas turbine. USP2018019869194.
  19. Martin, Yves; Di Paola, Franco. Sealing and cooling at the joint between shroud segments. USP2014048684680.
  20. Budnick, Matthew; Chuong, Conway; Scott, Jonathan A.. Seals for a circumferential stop ring in a turbine exhaust case. USP2017099771818.
  21. Sippel, Aaron D.; Freeman, Ted J.; Thomas, David J.; Lamusga, Joseph P.; Shoemaker, Brian J.; Hillier, Steven. Split line flow path seals. USP2017099759079.
  22. Kirtley, Kevin Richard; Morgan, Victor John. Tapered gas turbine segment seals. USP2018019863323.
  23. McCaffrey, Michael G.. Turbine rotor non-metallic blade attachment. USP2014128920127.
  24. Durocher,Eric; Clermont,Martin. Turbine shroud segment feather seal located in radial shroud legs. USP2008057374395.