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Blade containment structure 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-021/00
출원번호 US-0488563 (1983-04-25)
발명자 / 주소
  • Tomich Michael J. (Lynnfield MA)
출원인 / 주소
  • General Electric Company (Lynn MA 02)
인용정보 피인용 횟수 : 34  인용 특허 : 5

초록

A blade containment structure employs a two-layer honeycomb region radially outward of a fan blade rub strip. The two layers are separated by a septum and each layer contributes independently to strength and stiffness of the structure. A Kevlar blanket radially outward of the honeycomb region retain

대표청구항

A blade containment structure for surrounding blades of a gas turbine engine comprising: an annular honeycomb structure positionable radially outwardly of the entire axially extent of blade tips of said blades and including: a radially inner honeycomb region bounded by a septum and an inner wall spa

이 특허에 인용된 특허 (5)

  1. Monhardt Richard J. (Glastonbury CT) Orr Alfred B. (West Suffield CT) Premont Emile J. (South Hadley MA) Wright Joseph B. (Somers CT), Containment structure.
  2. Stanton William A. (Thorneywood GB2) Hazlewood Jonathan (Darley Abbey GB2) Kerridge Norman A. (Little Eaton GB2), Gas turbine engine casing.
  3. Lardellier Alain M. J. (Melun FRX), Removable support for the sealing lining of the casing of jet engine blowers.
  4. Joubert Raymond J. M. (Savigny sur Orge FRX) Soligny Marcel R. (Chevilly-Larue FRX), Retaining device for the compressor casing of a turbine engine.
  5. Porcelli Gerard (Yerres FRX), Safety device for a rotating element of a turbine engine.

이 특허를 인용한 특허 (34)

  1. McMillan, Alison J; Beckford, Peter R, Aerofoil containment structure.
  2. Xie, Ming, Articles comprising composite structures having mounting flanges.
  3. Hersheng Lin ; Shen-yeh Chen, Ballistic shield for dual engine single output shaft propulsion system.
  4. Voleti, Sreenivasa R.; Lussier, Darin S.; Naik, Rajiv A., Case with ballistic liner.
  5. Xie, Ming; Braley, Michael Scott, Composite fan containment case and methods of fabricating the same.
  6. Modafferi Mario,CAX ; Gomuc Reha,CAX, Containment system for containing blade burst.
  7. Evans, Dale E., Fan assembly.
  8. Wojtyczka, Czeslaw; Amin, Samy, Fan case design with metal foam between Kevlar.
  9. Wojtyczka, Czeslaw; Marshall, Andrew, Fan case for turbofan engine.
  10. Wojtyczka, Czeslaw; Marshall, Andrew, Fan case with rub elements.
  11. Evans, Dale Edward, Fan casing for a gas turbine engine.
  12. Kappes, Matthew J., Fan containment case.
  13. Costa, Mark W.; Robertson, Jr., Thomas J.; Lussier, Darin S., Fan containment case with thermally conforming liner.
  14. Allen Jeffrey S. ; Breeze-Stringfellow Andrew ; Manharth Gary B., Fan containment structure having contoured shroud for optimized tip clearance.
  15. Hoyland, Matthew Ashley Charles; Evans, Dale Edward, Fan containment system.
  16. Stewart Ian F. (Derby GB2), Fan duct casing.
  17. Costa, Mark W.; Tracy, James E.; Valentine, David E.; Ward, Raymond C.; Lewis, Dana H., Fan rub strip in situ machining system and method.
  18. Evans, Dale E., Fan track liner assembly.
  19. Goodwin Jeremy P,GB2, Gas Turbine engine casing construction.
  20. Clark, Daniel N. S., Gas turbine engine blade containment arrangement.
  21. Sathianathan, Sivasubramaniam K; Booth, Stephen J; Martindale, Ian G, Gas turbine engine blade containment assembly.
  22. Sivasubramaniam K Sathianathan GB; Ian G Martindale GB; Michael R Lawson GB, Gas turbine engine blade containment assembly.
  23. Evans, Charles R.; Ward, Douglas D., Jet aircraft fan case containment design.
  24. Worthoff,Frank; Glynn,Christopher Charles; Crall,David William; Bedel,David Lawrence, Method and apparatus for fabricating gas turbine engines.
  25. Crall, David William; Worthoff, Frank; Mollmann, Daniel Edward; Kray, Nicholas Joseph; Farson, Max, Methods and apparatus for fabricating a fan assembly for use with turbine engines.
  26. Xie, Ming, Methods for reducing stress on composite structures.
  27. Marlin, Francois Marie Paul; Verseux, Philippe, Panel for supporting abradable material in a turbomachine.
  28. Costa Mark W. ; Foose Andrew S. ; Korn Nathan D. ; Kowza Jan B. ; Lopardi Wendy P. ; Welch Douglas A., Penetration resistant fan casing for a turbine engine.
  29. Konigs, Karl-Heinz; Sonois, Gerome; Martins, Philippe, Piece of abradable material for the manufacture of a segment of an abradable ring seal for a turbomachine, and process for the manufacture of such a piece.
  30. Konigs, Karl-Heinz; Sonois, Gerome; Martins, Philippe, Segment of an abradable ring seal for a turbomachine, and process for the manufacture of such a piece.
  31. Ivakitch, Richard; Wojtyczka, Czeslaw; Eleftheriou, Andreas, Steel soft wall fan case.
  32. Svensson,Jan; Dahl,Eva; Russberg,David; Sjoqvist,Roger; Nilsson,Jan; Johansson,Sten, Turbine and a component.
  33. Perrot, Vincent Paul Gabriel; Cochon, Sébastien, Turbine engine casing and rotor wheel.
  34. Schilling Jan C., Turbomachine fan casing with dual-wall blade containment structure.
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