$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색도움말
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

통합검색

도움말도움말
상세검색 다국어 입력

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 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.

특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Components with micro cooled patterned coating layer and methods of manufacture

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-005/14    F01D-005/18    F01D-005/28    B05D-001/02    B05D-001/32    C23C-004/18    C23C-014/58    C23C-014/04    C23C-024/04    B05D-003/06    B05D-007/00   
출원번호 US-0663989 (2012-10-30)
등록번호 US-9562436 (2017-02-07)
발명자 / 주소
  • Bunker, Ronald Scott
  • Weaver, Scott Andrew
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Agosti, Ann M.
인용정보 피인용 횟수 : 0  인용 특허 : 40
초록
▼

A manufacturing method includes providing a substrate with an outer surface and at least one interior space, selectively deposited a coating on a portion of the substrate to form a selectively deposited coating having one or more grooves formed therein. The method further includes processing at least a portion of the surface of the selectively deposited coating to plastically deform the selectively deposited coating in the vicinity of the top of a respective groove. An additional coating is applied over at least a portion of the surface of the selectivel...

대표
청구항
▼

1. A manufacturing method comprising: providing a substrate with a continuous outer surface and at least one interior space;selectively depositing a coating on at least a portion of the continuous outer surface to define one or more grooves in the coating wherein each groove extends at least partially along the coating;processing at least a portion of a surface of the coating so as to plastically deform the coating at least in a vicinity of the top of a respective groove, such that a gap across the top of the respective groove is reduced; andapplying one...

인용문헌 (40)

  1. Lorenzo Battisti IT, Boundary layer control of aerodynamic airfoils.
  2. Correia Victor H. S. ; Manning Robert F., Cool tip blade.
  3. Horvath Richard L. (Hamilton OH) Harris Robert W. (Fairfield OH), Cooled turbine blade tip closure.
  4. Subramanian, Ramesh; Keyser, Mercedes, Cooling structure and method of manufacturing the same.
  5. Lee Ching P. (Cincinnati OH) Vaughn Eugene T. (Cincinnati OH) Palmer Nicholas C. (Loveland OH), Diffusion-cooled blade tip cap.
  6. Lee, Ching-Pang; Schafrik, Robert Edward; Darolia, Ramgopal, Directly cooled thermal barrier coating system.
  7. Jackson Melvin R. (Niskayuna NY) Skelly David W. (Burnt Hills NY) Rowe Raymond G. (Schenectady NY) LaChapelle Donald G. (Cincinnati OH) Wilson Paul S. (Sharonville OH), Double-wall airfoil.
  8. Tomita Yasuoki (Takasago JPX), Gas turbine rotor blade tip cooling device.
  9. Birkner, Jens; Halberstadt, Knut, Gas-turbine blade and method of manufacturing a gas-turbine blade.
  10. Correia Victor H. S., Impingement cooled airfoil tip.
  11. Schnell,Alexander; Bezencon,Cyrille; Hoebel,Matthias; Khan,Abdus Suttar; Konter,Maxim; Kurz,Wilfried, MCrAlY-coating.
  12. Hasz, Wayne Charles; Venkataramani, Venkat S.; Lee, Ching-Pang, Method for forming a channel on the surface of a metal substrate.
  13. Thomas Frank Fric ; Robert Patrick Campbell, Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture.
  14. Bunker Ronald Scott ; Bailey Jeremy Clyde ; Lee Ching-Pang ; Abuaf Nesim, Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture.
  15. Jackson Melvin Robert (2208 Niskayuna Dr. Niskayuna NY 12309) Skelly David William (8 Hollywood Dr. Burnt Hills NY 12027) Rowe Raymond Grant (2263 Berkley Ave. Schenectady NY 12309) LaChapelle Donald, Method for making a double-wall airfoil.
  16. Richard J. Grylls ; Yuk-Chiu Lau, Method for modifying stoichiometric NiAl coatings applied to turbine airfoils by thermal processes.
  17. Memmen,Robert L.; Neal,James W., Method for turbine element repairing.
  18. Bunker,Ronald Scott; Hardwicke,Canan Uslu; Lee,Ching Pang, Method of forming concavities in the surface of a metal component, and related processes and articles.
  19. Browning Janel Koca ; Jackson Melvin Robert, Method of forming hollow channels within a component.
  20. Zhao Ji-Cheng ; Jackson Melvin Robert ; Dupree Paul Leonard ; Dobbs James Ross, Method of forming hollow channels within a component.
  21. McKinley Barry Lee, Method of forming internal passages within articles and articles formed by same.
  22. Schnell,Alexander; Bezencon,Cyrille; Hoebel,Matthias; Khan,Abdus Suttar; Konter,Maxim; Kurz,Wilfried, Method of growing a MCrAlY-coating and an article coated with the MCrAlY-coating.
  23. Ronald S. Bunker, Method of modifying cooled turbine components.
  24. Bezencon, Cyrille; Fehrmann, Bernd; Hoebel, Matthias; Konter, Maxim; Kurz, Wilfried; Wagnière, Jean-Daniel, Method of producing a hot gas component of a turbomachine including an embedded channel.
  25. Lee, Ching-Pang; Darolia, Ramgopal, Network cooled coated wall.
  26. Darolia, Ramgopal; Lee, Ching-Pang; Schafrik, Robert Edward, Process for forming micro cooling channels inside a thermal barrier coating system without masking material.
  27. Hans-Joachim Roesler DE; Alexander Beeck DE; Peter Ernst CH; Reinhard Fried CH, Process for producing a thermally loaded casting.
  28. Maxim Konter CH; Wilfried Kurz CH, Process for producing or repairing cooling channels in monocrystalline components of gas turbines.
  29. Fernihough John,CHX ; Beeck Alexander,DEX ; Bogli Andreas,CHX, Process of plugging cooling holes of a gas turbine component.
  30. Jeffrey Arnold Fehrenbach ; John Howard Starkweather ; Michael Beverley, Shaped cooling hole for an airfoil.
  31. Joslin,Frederick R., Suspended abrasive waterjet hole drilling system and method.
  32. Lee Ching-Pang, Tapered tip turbine blade.
  33. Mayer Jeffrey C. ; Liotta Gary C. ; Starkweather John H. ; Gominho Antonio C., Tapered tip-rib turbine blade.
  34. Yan Chai ; Gary M. Lomasney ; Keith Douglas Sheffler, Thermal barrier coating having improved durability and method of providing the coating.
  35. Liang, George, Transpiration cooled turbine airfoil.
  36. Campbell, Christian X.; Morrison, Jay A., Turbine airfoil with a compliant outer wall.
  37. Lee Ching-Pang (Cincinnati OH), Turbine blade squealer tip peripheral end wall with cooling passage arrangement.
  38. Devore, Matthew A.; Luczak, Blake J., Turbine component with axially spaced radially flowing microcircuit cooling channels.
  39. Emmerson Calvin W. (Mooresville IN), Turbine cooling.
  40. Lee Ching-Pang, Twin rib turbine blade.

IPC 상위 출원인