$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Abradable component for a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-011/00
출원번호 US-0682048 (2007-03-05)
등록번호 US8038388 (2011-10-04)
발명자 / 주소
  • Freling, Melvin
  • Lagueux, Ken
  • Strock, Christopher W.
  • Pilecki, Jr., Joseph G.
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Carlson, Gaskey & Olds PC
인용정보 피인용 횟수 : 5  인용 특허 : 45

초록

A gas turbine engine component includes an airfoil having a radial outward end and a radial inward end. A seal member is positioned adjacent to the radial inward end of the airfoil. A tip of the radial inward end of the airfoil is coated with an abradable material. The seal member is coated with an

대표청구항

What is claimed is: 1. A gas turbine engine component, comprising:a compressor stator vane having a radial outward end and a radial inward end;a rotor seal land adjacent to said radial inward end of said compressor stator vane, wherein a tip of said radial inward end of said compressor stator vane i

이 특허에 인용된 특허 (45)

  1. Walden Frederick Clell ; Crawford George Lee ; Dalzell ; Jr. William John, Abradable seal having improved properties and method of producing seal.
  2. Erickson ; Arnold Roderick ; Panzera ; Carlino, Abradable seal material and composition thereof.
  3. Wiebe David J. (Palm Beach Gardens FL), Abradeable labyrinth stator seal.
  4. Draskovich Barry S. ; Frani Norman E. ; Joseph Stephen S. ; Narasimhan Dave, Abrasive tip/abradable shroud system and method for gas turbine compressor clearance control.
  5. Seda, Jorge F.; Dunbar, Lawrence W.; Gliebe, Philip R.; Szucs, Peter N.; Brauer, John C.; Johnson, James E.; Moniz, Thomas; Steinmetz, Gregory T., Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors.
  6. Shuba Brian H. (Mason OH), Apparatus for bleeding air.
  7. Randall Richard Good ; George Everett Foster, Article having durable ceramic coating with localized abradable portion.
  8. Mazeaud Georges (Yerres FRX) Picard Jean L. (Vaux Le Penil FRX), Axial compressor and method of carrying out maintenance on the axial compressor.
  9. Robideau Brian A. (Glastonbury CT) Niiler Juri (Glastonbury CT), Blade tip seal for an axial flow rotary machine.
  10. Lewis,Leo V, Cantilevered stator stage.
  11. Koff Steven G. (Palm Beach Gardens FL) Mazzawy Robert S. (South Glastonbury CT) Nikkanen John P. (West Hartford CT) Nolcheff Nick A. (Palm Beach Gardens FL), Case treatment for compressor blades.
  12. Humhauser, Werner, Casing structure of metal construction.
  13. Eaton Harry E. (Woodstock CT) Novak Richard C. (Glastonbury CT), Co-spray abrasive coating.
  14. Freling Melvin ; Gupta Dinesh K. ; Lagueux Ken ; DeMasi-Marcin Jeanine T., Columnar zirconium oxide abrasive coating for a gas turbine engine seal system.
  15. Rice Ivan G. (P.O. Box 233 Spring TX 77383), Compression intercooled gas turbine combined cycle.
  16. Rice Ivan G. (P.O. Box 233 Spring TX 77383), Compression intercooled high cycle pressure ratio gas generator for combined cycles.
  17. Ciokajlo John J. (Henderson NV) Hauser Ambrose A. (Wyoming OH), Counterrotating turbine support assembly.
  18. Clouse,Brian E.; Cardoso,Louis M., Damper for stator assembly.
  19. Holmes Trent H. (Rocky Hill CT), Floating vane support.
  20. Burge Joseph C., Gas turbine compressor spool with structural and thermal upgrades.
  21. Giffin ; III Rollin G. (Cincinnati OH) Lenahan Dean T. (Cincinnati OH), Gas turbine engine.
  22. Plemmons Larry W. (Fairfield OH) Proctor Robert (West Chester OH) Albers Robert J. (Park Hills KY) Gardner Donald L. (West Chester OH), Gas turbine engine case counterflow thermal control.
  23. Johnson David M. (Mainville OH), Gas turbine engine case thermal control flange.
  24. Nissley David M. ; Harter Harold D. ; Godin Daniel R. ; Foster George E., Gas turbine engine component.
  25. Ciokajlo John J. (Henderson NV) Hauser Ambrose A. (Wyoming OH) Davison Samuel H. (Milford OH), Gas turbine engine rotor support system.
  26. Fried, Reinhard, Gas turbine seal.
  27. Lardellier, Alain, Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor.
  28. Shuba Brian H. (Mason OH), Method for bleeding air.
  29. Srdoch Rudolph R. (Trafford PA), Mounting bracket for bracing peripheral connecting rings for dynamoelectric machines′stator windings.
  30. Sileo Gerard A. (Jupiter FL) Appleby John W. (Palm Beach Gardens FL) Narsavage Stephen T. (Jupiter FL) Alent Francis X. (Port St. Lucie FL) Davis Charles G. (Jupiter FL), Plasma sprayed abradable seals for gas turbine engines.
  31. Bracken,Robert James; Hathaway,Sterling Ray; Fitts,David Orus; Korzun,Ron W.; Duclos,Laurence Scott; Adis,William Edward; Kowalczyk,Mark William; Couture,Bernard Arthur, Removable abradable seal carriers for sealing between rotary and stationary turbine components.
  32. Ackermann William (East Hartford CT), Rotary seal.
  33. Ciokajlo John J. (Henderson NV) Hauser Ambrose A. (Wyoming OH) Davison Samuel H. (Milford OH), Rotatable turbine frame.
  34. Koff Steven G. (Cambridge MA) Nikkanen John P. (West Hartford CT) Mazzawy Robert S. (South Glastonbury CT), Rotor case treatment.
  35. Pilecki, Jr.,Joseph G., Rotor for jet turbine engine having both insulation and abrasive material coatings.
  36. Nissley David M. ; Harter Harold D. ; Godin Daniel R. ; Foster George E., Segmented abradable ceramic coating.
  37. De Cosmo Anthony R. (Wallingford CT) Young John H. (South Windsor CT), Shroud ring for use in a gas turbine engine.
  38. Tran,Tuy; Pickens,John T., Split knife edge seals.
  39. Laurello, Vincent P., Stator structure for a gas turbine engine.
  40. Vine Raymond W. (East Hartford CT) Robbins Donald A. (South Windsor CT) Nordstrom Donald G. (Meriden CT) Goodstein Mark B. (Windsor Locks CT), Thin abradable ceramic air seal.
  41. Frenkel Richard G. (Belmont MA) Huffman James A. (Topsfield MA) Rennert Jonathan A. (Belmont MA) Stasio Dominic (Wakefield MA), Thrust droop compensation method and system.
  42. Barbeau Dennis E. (Liberty Center OH), Turbine engine with shroud cooling means.
  43. Beutin, Bruno; Brault, Michel; Gervais, Pascal; Guigli, Elisabeth; Thore, Monique, Turbomachine rotor assembly with two bladed-discs separated by a spacer.
  44. Koff Steven G. (Miami FL) Koff Bernard L. (Palm Beach Gardens FL) Lyon Bruce V. (Palm Beach Gardens FL) Duer Mark G. (Palm Beach Gardens FL), Vaned passage hub treatment for cantilever stator vanes.
  45. Koff Steven G. ; Koff Bernard L. ; Lyon Bruce V. ; Duer Mark G., Vaned passage hub treatment for cantilever stator vanes and method.

이 특허를 인용한 특허 (5)

  1. Alvanos, Ioannis, Gas turbine engine component having tip vortex creation feature.
  2. Alvanos, Ioannis, Serrated outer surface for vortex initiation within the compressor stage of a gas turbine.
  3. Lyders, David R, Stator assembly with pad interface for a gas turbine engine.
  4. Novikov, Dmitri; Furrer, David Ulrich; Burlatsky, Sergei F, Stiffness controlled abradeable seal system with max phase materials and methods of making same.
  5. Richardson, Carl S.; Szymbor, John A., Vane tip machining fixture assembly.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로