$\require{mediawiki-texvc}$

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.

Variable vane segment 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/12
  • F01D-009/04
  • F01D-009/02
  • F01D-025/08
  • F01D-025/12
출원번호 US-0706033 (2015-05-07)
등록번호 US-10066549 (2018-09-04)
발명자 / 주소
  • Slavens, Thomas N.
  • Snyder, Brooks E.
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Carlson, Gaskey & Olds, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 64

초록

A variable vane pack includes an inner platform, an outer platform, radially outward of the inner platform, a plurality of vanes connecting the inner platform to the outer platform, wherein the outer platform comprises a platform body and an impingement plate, the impingement plate having a radially

대표청구항

1. A variable vane pack comprising: an inner platform;an outer platform, radially outward of said inner platform;a plurality of vanes connecting said inner platform to said outer platform; andwherein the outer platform comprises a platform body and an impingement baffle, the impingement baffle havin

이 특허에 인용된 특허 (64)

  1. Khanin, Alexander Anatolievich; Kostege, Valery, Axial flow gas turbine.
  2. Romanov, Dmitriy A., Blade outer air seal with multi impingement plate assembly.
  3. Chang, Shyy-Woei, CPU cooler.
  4. Pidcock, Anthony; Close, Desmond; Spooner, Michael P, Combustion apparatus.
  5. Kirsopp, Philip J.; Dornback, Aaron J.; Hoke, James B., Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panel.
  6. Kenworthy Milton J. (Cincinnati OH), Combustor liner.
  7. Chila, Ronald James, Combustor liner cooling system.
  8. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with convergent cooling channel.
  9. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with decreased liner cooling.
  10. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with improved film cooling.
  11. Bunker,Ronald Scott, Combustor liner with inverted turbulators.
  12. Cunha, Frank J.; Erbas-Sen, Nurhak, Combustor liner with reduced cooling dilution openings.
  13. Bunker, Ronald Scott, Combustor liner with ring turbulators and related method.
  14. Enzaki Yoshiki (Kobe JPX) Kitahara Kazuki (Kobe JPX) Terasaka Satoru (Kakogawa JPX) Mori Kenji (Akashi JPX) Kimura Takeshi (Kobe JPX), Combustor of gas turbine.
  15. Guimbard, Jean-Michel Bernard; Pabion, Philippe Jean-Pierre; Soupizon, Jean-Luc, Cooled blade for a turbomachine.
  16. Krueckels, Joerg; Pathak, Milan, Cooled constructional element for a gas turbine.
  17. Pope, J. Edward; Rhodes, Jeffery Forest; Snyder, Douglas J., Cooled gas turbine engine component.
  18. Liang, George, Cooled turbine stator vane.
  19. Joe, Christopher R.; Thole, Karen A., Cooling arrangement for a turbine engine component.
  20. Albrecht,Harry A.; Shteyman,Yevgeniy, Cooling fluid preheating system for an airfoil in a turbine engine.
  21. Bunker Ronald Scott, Cooling for double-wall structures.
  22. Tarada Fathi,CHX, Cooling in gas turbines.
  23. Ahmad, Fathi; Hoell, Harald; Kolk, Karsten; Nimptsch, Harald; Setz, Werner, Cooling of a gas turbine component designed as a rotor disk or turbine blade.
  24. Campbell, Christian X; Eng, Darryl; Lee, Ching-Pang; Patat, Harry, Cooling system for three hook ring segment.
  25. Reichert, Arnd; Lieser, Dirk, Device and method for controlling a cooling air flow of a gas turbine.
  26. Lee Ching-Pang, Dimpled impingement baffle.
  27. Trindade,Ricardo; Pham,Dan Que; Lebel,Larry, Double impingement vane platform cooling.
  28. Bunker, Ronald Scott, Double wall combustor liner segment with enhanced cooling.
  29. Chila, Ronald James; McMahan, Kevin Weston, Effusion cooled one-piece can combustor.
  30. Mayer,Robert R.; Stoner,Charles D., Extended impingement cooling device and method.
  31. Burd, Steven W.; Siskind, Kenneth S.; Graves, Charles B., Gas turbine combustor.
  32. Corr, Robert; Sykes, Peter; Struck, Bruno; Thomas, Kenneth G.; Braeutigam, Richard; Gauce, Danny; Krichever, Alexander; Phi, Vu; Caron, Timothy, Gas turbine combustor with mounting for Helmholtz resonators.
  33. Surace, Raymond; Milliken, Andrew D., Gas turbine engine component cooling scheme.
  34. Wettstein, Hans; Wirsum, Manfred; Schulz, Steffen, Gas turbine plant with exhaust gas recirculation and also method for operating such a plant.
  35. Lam, Kam-Kei, Gas turbine swirler including a vortex generator device and fuel injection openings arranged between adjacent vanes.
  36. Anguisola McFeat, Jose; Kreiselmaier, Erich; Nagler, Christoph; Riazantsev, Sergei, Gas turbine vane with improved cooling.
  37. Gerendas, Miklos, Gas-turbine combustion chamber with a cooling-air supply device.
  38. Auxier Thomas A. (Palm Beach Gardens FL) Rannie James B. (Tequesta FL) Field Robert E. (Tequesta FL), Hot gas duct liner.
  39. Bunker,Ronald Scott; Lee,Ching Pang, Hot gas path component with mesh and impingement cooling.
  40. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Lee,Ching Pang, Hot gas path component with mesh and turbulated cooling.
  41. Durocher, Eric; Grivas, Nicolas, Interturbine vane with multiple air chambers.
  42. Bhangu Jagnandan Kumar (Ockbrook EN), Laminated materials.
  43. Bunker, Ronald Scott, Linear surface concavity enhancement.
  44. Pane ; Francis C. ; Sepulveda ; Domingo, Louver construction for liner of gas turbine engine combustor.
  45. Vogt Robert L. (Marblehead MA), Method of breach cooling.
  46. Lee, Ching-Pang; Morrison, Jay A., Method of fabricating a nearwall nozzle impingement cooled component for an internal combustion engine.
  47. Dede, Ercan Mehmet, Power modules, cooling devices and methods thereof.
  48. Dierberger James A. (Hebron CT) Ackermann William (East Hartford CT) Fine Arthur D. (West Hartford CT), Prestressed combustor liner for gas turbine engine.
  49. Malecki, Stacy T.; Propheter-Hinckley, Tracy A.; Learned, Amanda Jean; Gregg, Shawn J., Recessed metering standoffs for airfoil baffle.
  50. Morrison, Jay A.; Lee, Ching-Pang; Crawford, Michael E., Regeneratively cooled transition duct with transversely buffered impingement nozzles.
  51. Reider Samuel B. (Indianapolis IN), Shingled laminated porous material.
  52. Rogers, Bradley S, Sorbent activation plate.
  53. Noe, Mark Eugene; Darkins, Jr., Toby George; Doughty, Roger Lee, Tangential flow baffle.
  54. Schrantz Jeffrey P. (Apple Valley MN) Squire David R. (Phoenix AZ), Thin wall combustor with backside impingement cooling.
  55. Cunha Francisco J. (Schenectady NY) DeAngelis David A. (Voorheesville NY) Brown Theresa A. (Clifton Park NY) Chopra Sanjay (Albany NY) Correia Victor H. S. (New Labanon NY) Predmore Daniel R. (Clifto, Turbine stator vane segments having combined air and steam cooling circuits.
  56. Liang, George, Turbine vane endwall with float wall heat shield.
  57. Perrot, Vincent Paul Gabriel; Pesteil, Agnes Claire Marie, Turbomachine with variable-pitch vortex generator.
  58. Lee, Ching-Pang; Morrison, Jay A., Two stage serial impingement cooling for isogrid structures.
  59. Smith ; Jr. Paul A. (Palm Beach Gardens FL) Kramer George J. (Jupiter FL), Uniform cooling film replenishment thermal liner assembly.
  60. Dodd ; Alec George, Vane for a gas turbine engine having means for impingement cooling thereof.
  61. Burdick, Andrew D.; Praisner, Thomas J.; Aggarwala, Andrew S.; Hudson, Eric A.; McCaffrey, Michael G., Variable vane and seal arrangement.
  62. Meginnis George B. (Indianapolis IN) Spees John A. (Indianapolis IN), Waffle pattern porous material.
  63. Hadder,James L., Waffled impingement effusion method.
  64. Ekkad, Srinath Varadarajan; Esposito, Eric Ian; Kim, Yong Weon, Zero-cross-flow impingement via an array of differing length, extended ports.
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