DE69927920D1 - Zwischenschaufelplattform - Google Patents
ZwischenschaufelplattformInfo
- Publication number
- DE69927920D1 DE69927920D1 DE69927920T DE69927920T DE69927920D1 DE 69927920 D1 DE69927920 D1 DE 69927920D1 DE 69927920 T DE69927920 T DE 69927920T DE 69927920 T DE69927920 T DE 69927920T DE 69927920 D1 DE69927920 D1 DE 69927920D1
- Authority
- DE
- Germany
- Prior art keywords
- blade platform
- blade
- platform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
- F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Laminated Bodies (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9828484 | 1998-12-24 | ||
GBGB9828484.7A GB9828484D0 (en) | 1998-12-24 | 1998-12-24 | Improvements in or relating to bladed structures for fluid flow propulsion engines |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69927920D1 true DE69927920D1 (de) | 2005-12-01 |
DE69927920T2 DE69927920T2 (de) | 2006-04-20 |
Family
ID=10844923
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69927920T Expired - Lifetime DE69927920T2 (de) | 1998-12-24 | 1999-12-09 | Zwischenschaufelplattform |
Country Status (4)
Country | Link |
---|---|
US (1) | US6312224B1 (de) |
EP (1) | EP1013886B1 (de) |
DE (1) | DE69927920T2 (de) |
GB (1) | GB9828484D0 (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6217283B1 (en) * | 1999-04-20 | 2001-04-17 | General Electric Company | Composite fan platform |
GB9915637D0 (en) * | 1999-07-06 | 1999-09-01 | Rolls Royce Plc | A rotor seal |
FR2825748B1 (fr) | 2001-06-07 | 2003-11-07 | Snecma Moteurs | Agencement de rotor de turbomachine a deux disques aubages separes par une entretoise |
FR2858351B1 (fr) * | 2003-07-31 | 2006-01-13 | Snecma Moteurs | Plate-forme inter-aubes a flechissement lateral, pour un support d'aubes de turboreacteur |
GB0427083D0 (en) * | 2004-12-10 | 2005-01-12 | Rolls Royce Plc | Platform mounted components |
US7025356B1 (en) | 2004-12-20 | 2006-04-11 | Pratt & Whitney Canada Corp. | Air-oil seal |
US7942639B2 (en) * | 2006-03-31 | 2011-05-17 | General Electric Company | Hybrid bucket dovetail pocket design for mechanical retainment |
GB0611031D0 (en) | 2006-06-06 | 2006-07-12 | Rolls Royce Plc | An aerofoil stage and a seal for use therein |
GB0614640D0 (en) * | 2006-07-22 | 2006-08-30 | Rolls Royce Plc | An annulus filler seal |
GB0804260D0 (en) * | 2008-03-07 | 2008-04-16 | Rolls Royce Plc | Annulus filler |
US8070448B2 (en) * | 2008-10-30 | 2011-12-06 | Honeywell International Inc. | Spacers and turbines |
GB0914060D0 (en) * | 2009-08-12 | 2009-09-16 | Rolls Royce Plc | A rotor assembly for a gas turbine |
GB0919657D0 (en) | 2009-11-11 | 2009-12-23 | Rolls Royce Plc | Annulus filler for a gas turbine engine |
US8794925B2 (en) * | 2010-08-24 | 2014-08-05 | United Technologies Corporation | Root region of a blade for a gas turbine engine |
GB201020857D0 (en) * | 2010-12-09 | 2011-01-26 | Rolls Royce Plc | Annulus filler |
GB201106278D0 (en) | 2011-04-14 | 2011-05-25 | Rolls Royce Plc | Annulus filler system |
US9334743B2 (en) * | 2011-05-26 | 2016-05-10 | United Technologies Corporation | Ceramic matrix composite airfoil for a gas turbine engine |
GB201119655D0 (en) | 2011-11-15 | 2011-12-28 | Rolls Royce Plc | Annulus filler |
FR2988427B1 (fr) * | 2012-03-20 | 2017-07-21 | Snecma | Plate-forme inter-aubes |
RU2525376C1 (ru) * | 2013-03-28 | 2014-08-10 | Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" | Рабочее колесо осевого компрессора газотурбинного двигателя |
CA2913046A1 (en) | 2013-05-23 | 2014-11-27 | General Electric Company | Composite compressor blade and method of assembling |
GB201314540D0 (en) * | 2013-08-14 | 2013-09-25 | Rolls Royce Plc | Annulus filler |
US10024234B2 (en) | 2014-09-08 | 2018-07-17 | Rolls-Royce Deutschland Ltd & Co Kg | Panels of a fan of a gas turbine |
DE102014217884A1 (de) * | 2014-09-08 | 2016-03-24 | Rolls-Royce Deutschland Ltd & Co Kg | Füllelemente eines Fans einer Gasturbine |
US10156151B2 (en) * | 2014-10-23 | 2018-12-18 | Rolls-Royce North American Technologies Inc. | Composite annulus filler |
US10995846B2 (en) * | 2016-09-23 | 2021-05-04 | Bell Helicopter Textron Inc. | Fan with labyrinth seal for prevention of water damage to a gearbox |
FR3080322B1 (fr) * | 2018-04-20 | 2020-03-27 | Safran Aircraft Engines | Aube comprenant une structure en materiau composite et procede de fabrication associe |
US10557361B1 (en) * | 2018-10-16 | 2020-02-11 | United Technologies Corporation | Platform for an airfoil of a gas turbine engine |
FR3107923B1 (fr) * | 2020-03-03 | 2022-02-04 | Safran Aircraft Engines | Procede de fabrication d’une plateforme composite pour une soufflante de turbomachine d’aeronef |
US12012857B2 (en) | 2022-10-14 | 2024-06-18 | Rtx Corporation | Platform for an airfoil of a gas turbine engine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1170592A (en) * | 1966-11-29 | 1969-11-12 | Rolls Royce | Aerofoil-Shaped Blades and Blade Assemblies, for use in a Fluid Flow Machine |
GB1190293A (en) * | 1968-03-20 | 1970-04-29 | Rolls Royce | Method of Making a Bladed Rotor |
US3749518A (en) | 1972-03-15 | 1973-07-31 | United Aircraft Corp | Composite blade root configuration |
US3756745A (en) * | 1972-03-15 | 1973-09-04 | United Aircraft Corp | Composite blade root configuration |
US4045149A (en) | 1976-02-03 | 1977-08-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Platform for a swing root turbomachinery blade |
US4343593A (en) * | 1980-01-25 | 1982-08-10 | The United States Of America As Represented By The Secretary Of The Air Force | Composite blade for turbofan engine fan |
US4589176A (en) * | 1983-11-25 | 1986-05-20 | Rockwell International Corporation | Fiber-composite turbine blade and method for its construction |
GB2171151B (en) | 1985-02-20 | 1988-05-18 | Rolls Royce | Rotors for gas turbine engines |
US5344686A (en) * | 1989-12-20 | 1994-09-06 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh | Tension strained fiber structure component |
FR2685732B1 (fr) | 1991-12-31 | 1994-02-25 | Snecma | Aube de turbomachine en materiau composite. |
US5232346A (en) * | 1992-08-11 | 1993-08-03 | General Electric Company | Rotor assembly and platform spacer therefor |
FR2699499B1 (fr) * | 1992-12-23 | 1995-03-10 | Eurocopter France | Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication avec étape d'injection. |
US5403153A (en) * | 1993-10-29 | 1995-04-04 | The United States Of America As Represented By The Secretary Of The Air Force | Hollow composite turbine blade |
US5573377A (en) * | 1995-04-21 | 1996-11-12 | General Electric Company | Assembly of a composite blade root and a rotor |
-
1998
- 1998-12-24 GB GBGB9828484.7A patent/GB9828484D0/en not_active Ceased
-
1999
- 1999-12-09 DE DE69927920T patent/DE69927920T2/de not_active Expired - Lifetime
- 1999-12-09 EP EP99309924A patent/EP1013886B1/de not_active Expired - Lifetime
- 1999-12-14 US US09/459,866 patent/US6312224B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE69927920T2 (de) | 2006-04-20 |
EP1013886B1 (de) | 2005-10-26 |
EP1013886A2 (de) | 2000-06-28 |
EP1013886A3 (de) | 2004-01-07 |
US6312224B1 (en) | 2001-11-06 |
GB9828484D0 (en) | 1999-02-17 |
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ID28624A (id) | Turunan 2-fenilpiran-4-on | |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |