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Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-001/04
출원번호 US-0276522 (2008-11-24)
등록번호 US8011877 (2011-08-23)
발명자 / 주소
  • Schilling, Jan Christopher
  • Kray, Nicholas Joseph
출원인 / 주소
  • General Electric Company
대리인 / 주소
    William Scott, Andes
인용정보 피인용 횟수 : 3  인용 특허 : 36

초록

A gas turbine engine assembly having one or more blade rows with blades extending radially inwardly from a rotatable drum, one or more composite fiber material rings disposed circumferentially around the rotatable drum, and the composite fiber material rings including circumferentially extending hig

대표청구항

What is claimed is: 1. A gas turbine engine assembly comprising:one or more blade rows having blades extending radially inwardly from a rotatable drum,one or more composite fiber material rings disposed circumferentially around a radially outer surface of the rotatable drum and located radially outw

이 특허에 인용된 특허 (36)

  1. Seda, Jorge F., Aircraft engine with inter-turbine engine frame.
  2. 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.
  3. Orlando, Robert Joseph; Moniz, Thomas Ory; Baughman, John Lewis, Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans.
  4. Schreiber, Karl, Axial-flow compressor for a gas turbine engine.
  5. Kochendorfer Richard (Silberwaldstrasse 1 7000 Stuttgart 75 DEX), Bandage for radially stressing the segments of a compressor rotor for a turbine.
  6. Ress ; Jr. Robert A. (Carmel IN), Composite compressor rotor with removable airfoils.
  7. Xie,Ming; Mitchell,Stephen C.; LaChapelle,Donald G.; Braley,Michael Scott; Roberts,Gary D.; Hopkins,Dale, Composite containment case for turbine engines.
  8. Xie,Ming; Mitchell,Stephen C.; LaChapelle,Donald George; Blanton,Lee A.; Price,Richard T.; Crall,David W.; Worthoff,Frank, Composite fan containment case for turbine engines.
  9. Matheny,Alfred Paul, Composite tip shroud ring.
  10. Seda, Jorge F.; Dunbar, Lawrence W.; Szucs, Peter N.; Brauer, John C.; Johnson, James E., Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor.
  11. Orlando,Robert Joseph; Moniz,Thomas Ory, Counter-rotating gas turbine engine and method of assembling same.
  12. Moniz,Thomas O.; Singh,Anant P.; Allen,Daniel M.; Bond,Donald R., Counter-rotating turbine engine and method of assembling same.
  13. Seda,Jorge Francisco; Moniz,Thomas Ory; Butler,Lawrence, Counter-rotating turbine engine and method of assembling same.
  14. Moniz, Thomas Ory; Orlando, Robert Joseph, Counterrotatable booster compressor assembly for a gas turbine engine.
  15. Prentice, Ian Francis; Crall, David William; Busbey, Bruce Clark; Glynn, Christopher Charles; Bond, Donald Ray, Counterrotatable booster compressor assembly for a gas turbine engine.
  16. Wojtyczka, Czeslaw; Amin, Samy, Fan case design with metal foam between Kevlar.
  17. Twigg, Edwin S, Fiber reinforced metal rotor.
  18. Dambrine Bruno Jacques Gerard,FRX, Fibre-reinforced rotor stage for a turbomachine.
  19. Moniz,Thomas Ory; Orlando,Robert Joseph, Gas turbine engine assembly and methods of assembling same.
  20. Orlando, Robert Joseph; Moniz, Thomas Ory; Schilling, Jan Christopher, Gas turbine engine assembly and methods of assembling same.
  21. Ress ; Jr. Robert Anthony (Carmel IN), Gas turbine rotor with remote support rings.
  22. Farmer James L., High strength composite reinforced turbomachinery disk.
  23. Romani Giuseppe,CAX, Integrated fan / low pressure compressor rotor for gas turbine engine.
  24. Stoffer Lewis J. (Cincinnati OH), Light weight fan assembly.
  25. Krueger Wolfgang (Reichertshausen DEX) Wei William (Munich DEX), Method for manufacturing a blade ring for drum-shaped rotors of turbomachinery.
  26. Wei William (Munich DEX) Krger Wolfgang (Reichertshausen DEX), Method for manufacturing fiber-reinforced components for propulsion plants.
  27. Jakobsen Karl Severin (Somers CT) McLaughlin David Benjamin (South Windsor CT), Method of making filament reinforced composite rings from plural flat filamentary spiral layers.
  28. Schreiber,Karl, Protective ring for the fan protective casing of a gas turbine engine.
  29. Hull Peter R. (Ipswich MA), Reinforced rotor disk assembly.
  30. Ress ; Jr. Robert Anthony, Selectively reinforced member and method of manufacture.
  31. Henry, John Leslie; Orlando, Robert Joseph; Moniz, Thomas Ory, Turbofan engine assembly and method of assembling same.
  32. Orlando, Robert Joseph; Moniz, Thomas Ory, Turbofan engine assembly and method of assembling same.
  33. Aumont,Caroline; Chatel,Sandrine; Dambrine,Bruno Jacques Gerard; Escure,Didier Rene Andre; Fromentin,Jean Francois; Guedou,Jean yves; Molliex,Ludovic Edmond Camille; Rousselin,Stephane, Turbomachine rotor including at least one disk reinforced by a composite ring.
  34. Taylor John B. (Cincinnati OH), Unducted, counterrotating gearless front fan engine.
  35. Giffin ; III Rollin G. (Cincinnati OH), Variable specific thrust turbofan engine.
  36. Baughman, John Lewis; Orlando, Robert Joseph; Moniz, Thomas Ory, Variable torque split aircraft gas turbine engine counter rotating low pressure turbines.

이 특허를 인용한 특허 (3)

  1. Kray, Joseph Nicholas; Gemeinhardt, Gregory Carl; Jadhav, Prakash Kashiram; Klei, Douglas Edward; Nandula, Phani; Subramanian, Suresh, Composite compressor blade and method of assembling.
  2. Kray, Nicholas Joseph; McAfee, Christopher Lee; Shim, Dong-Jin, Composite rotor and vane assemblies with integral airfoils.
  3. Kray, Nicholas Joseph; Schilling, Jan Christopher; Jain, Nitesh; Roy, Abhijit, Method and system for separable blade platform retention clip.
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