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Dual structure turbine blade 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/28
출원번호 US-0269505 (1988-11-10)
발명자 / 주소
  • Wilson Lloyd W. (Scottsdale AZ)
출원인 / 주소
  • Allied-Signal Inc. (Morris Township, Morris County NJ 02)
인용정보 피인용 횟수 : 27  인용 특허 : 11

초록

A single crystal turbine blade has a portion of its attachment section layered with a fine grained, poly-crystalline alloy. The blade is prepared by casting a single crystal body with an undersized attachment section, and then layering the attachment section with the poly-crystalline superalloy to f

대표청구항

A composite turbine blade structure, comprising: a single crystal body having an airfoil section and an attachment section; and a layer of a polycrystalline alloy bonded onto at least a portion of said attachment section.

이 특허에 인용된 특허 (11)

  1. Meetham Geoffrey W. (Allestree GB2) Marjoram John R. (Coxbench GB2), Cambered blade or vane for a gas turbine engine.
  2. Giamei Anthony F. (Middletown CT) Kear Bernard H. (Madison CT), Composite single crystal article.
  3. Schrewelius ; deceased Nils G. (late of Hallstahammar SEX by Maud Schrewelius ; legal representative), Heat-resistant machine component.
  4. Fiedler Louis J. (Trumbull CT) Naik Subhash K. (Milford CT), High strength nickel base single crystal alloys.
  5. Harris Kenneth (Spring Lake MI) Erickson Gary L. (Muskegon MI), Low density single crystal super alloy.
  6. Gell Maurice L. (Newington CT) Giamei Anthony F. (Middletown CT), Mechanically worked single crystal article.
  7. Smashey Russell W. (Loveland OH) Stoffer Lewis J. (Cincinnati OH), Method for producing an article with a fluid passage.
  8. Gazzard Simon Thomas (New Milton EN) Hill Harold Taylor (Lymington EN), Method for reinforcing pistons.
  9. Rairden ; III John R. (Schenectady NY), Method of producing high quality plasma spray deposits of complex geometry.
  10. Kroebig Helmut L. (Rolling Hills CA), Plasma deposited rider rings for hot displacer.
  11. Jackson Melvin R. (Schenectady NY) Rairden ; III John R. (Schenectady NY), Plasma spray-cast components.

이 특허를 인용한 특허 (27)

  1. Propheter-Hinckley, Tracy A.; McCaffrey, Michael G., Airfoil attachment.
  2. Guglielmin, George; Lanzino, Joe; Macchia, Enzo; Barnett, Barry; Eleftheriou, Andreas; McDonough, Thomas, Airfoil blade.
  3. William Patrick Allen ; Walter E. Olson, Article having corrosion resistant coating.
  4. William Patrick Allen ; Walter E. Olson, Article having corrosion resistant coating.
  5. William Patrick Allen ; Walter E. Olson ; Dilip M. Shah ; Alan David Cetel, Article having corrosion resistant coating.
  6. Luthra, Krishan Lal; Corman, Gregory Scot; Ramamurthi, Badri Narayan, Ceramic matrix composite articles and methods for forming same.
  7. Whittaker Gary Scott, Coal gasification burner shield coating.
  8. Steinhardt, Erich; Smarsly, Wilfried; Werner, André, Ductile compensation layer for brittle components.
  9. Macchia, Enzo; Barnett, Barry; Eleftheriou, Andreas; McDonough, Tom; Guglielmin, George; Lanzino, Joe, Gas turbine blade and method of protecting same.
  10. Shah, Dilip M.; Cetel, Alan D.; Stoner, Alan W.; Allen, William P., High modulus metallic component for high vibratory operation.
  11. Shah,Dilip M.; Cetel,Alan D.; Stoner,Alan W.; Allen,William P., High modulus metallic component for high vibratory operation.
  12. Davies, Daniel O., Integral turbine blade and platform.
  13. Strangman, Thomas E., Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk.
  14. Etter, Thomas; Mücke, Roland, Method for manufacturing components made of single crystal (SX) or directionally solidified (DS) nickelbase superalloys.
  15. Barnett, Barry; Cheung, Kin-Leung; McDonough, Thomas; Eleftheriou, Andreas; Macchia, Enzo, Method of applying a nanocrystalline coating to a gas turbine engine component.
  16. Burke Michael A. ; Freyer Paula D. ; Hebbar Mohan A. ; Seth Brij B. ; Swartzbeck Gary W. ; Zagar Thomas Walter, Method of bonding cast superalloys.
  17. Arnold James E., Method of repairing a turbine engine airfoil part.
  18. Mittendorf, Don; Gatto, Christopher David; Lara, Leticia; Kemp, Megan; Szuromi, Andy, Methods for fabricating gas turbine engine components using a stepped transient liquid phase joining process.
  19. Steibel, James Dale, Methods for forming ceramic matrix composite articles.
  20. Cheung, Kin-Leung; Macchia, Enzo; Bamett, Barry, Nano-metal coated vane component for gas turbine engines and method of manufacturing same.
  21. Fitzgerald Thomas John ; Zagar Thomas Walter, Process for forming combustion turbine components by transient liquid phase bonding.
  22. Stuart Lee DE; Peter Broadhead GB; Tim Hopp DE, Retaining arrangement for rotor blades of axial-flow turbomachinery.
  23. Goldman Edward Harvey ; Darolia Ramgopal ; Wortman David John, Superalloy component with dispersion-containing protective coating.
  24. James,Allister W., Turbine blade assembly and method of manufacture.
  25. Burke Michael A. ; Freyer Paula D. ; Hebbar Mohan A. ; Seth Brij B. ; Swartzbeck Gary W. ; Zagar Thomas Walter, Turbine blades made from multiple single crystal cast superalloy segments.
  26. Burke, Michael A.; Freyer, Paula D.; Hebbar, Mohan A.; Seth, Brij B.; Swartzbeck, Gary W.; Zagar, Thomas Walter, Turbine components comprising thin skins bonded to superalloy substrates.
  27. Brummitt-Brown, Angus Robert; Lord, Adrian Clifford; MacDonald, Niall, Turbine diaphragm construction.
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