DE69812051D1 - Turbomaschinenschaufel mit Riefen - Google Patents
Turbomaschinenschaufel mit RiefenInfo
- Publication number
- DE69812051D1 DE69812051D1 DE69812051T DE69812051T DE69812051D1 DE 69812051 D1 DE69812051 D1 DE 69812051D1 DE 69812051 T DE69812051 T DE 69812051T DE 69812051 T DE69812051 T DE 69812051T DE 69812051 D1 DE69812051 D1 DE 69812051D1
- Authority
- DE
- Germany
- Prior art keywords
- grooves
- turbomachine blade
- turbomachine
- blade
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- F01D5/16—Form or construction for counteracting blade vibration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/995,979 US5913661A (en) | 1997-12-22 | 1997-12-22 | Striated hybrid blade |
Publications (1)
Publication Number | Publication Date |
---|---|
DE69812051D1 true DE69812051D1 (de) | 2003-04-17 |
Family
ID=25542384
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69812051T Expired - Lifetime DE69812051D1 (de) | 1997-12-22 | 1998-10-21 | Turbomaschinenschaufel mit Riefen |
Country Status (4)
Country | Link |
---|---|
US (1) | US5913661A (de) |
EP (1) | EP0924380B1 (de) |
JP (1) | JPH11201089A (de) |
DE (1) | DE69812051D1 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6454536B1 (en) * | 2000-02-09 | 2002-09-24 | General Electric Company | Adhesion enhancers to promote bonds of improved strength between elastomers metals in lightweight aircraft fan blades |
US6338609B1 (en) * | 2000-02-18 | 2002-01-15 | General Electric Company | Convex compressor casing |
GB0100695D0 (en) * | 2001-01-11 | 2001-02-21 | Rolls Royce Plc | a turbomachine blade |
GB2391270B (en) * | 2002-07-26 | 2006-03-08 | Rolls Royce Plc | Turbomachine blade |
GB2397257A (en) * | 2003-01-16 | 2004-07-21 | Rolls Royce Plc | Article provided with a vibration damping coating |
DE10301755A1 (de) * | 2003-01-18 | 2004-07-29 | Rolls-Royce Deutschland Ltd & Co Kg | Fanschaufel für ein Gasturbienentriebwerk |
GB0406444D0 (en) * | 2004-03-23 | 2004-04-28 | Rolls Royce Plc | An article having a vibration damping coating and a method of applying a vibration damping coating to an article |
EP1640562A1 (de) * | 2004-09-23 | 2006-03-29 | Siemens Aktiengesellschaft | Verfahren zur Frequenzverstimmung einer Turbinenschaufel sowie Turbinenschaufel |
JP4863162B2 (ja) * | 2006-05-26 | 2012-01-25 | 株式会社Ihi | ターボファンエンジンのファン動翼 |
DE502006003548D1 (de) * | 2006-08-23 | 2009-06-04 | Siemens Ag | Beschichtete Turbinenschaufel |
GB2450936B (en) * | 2007-07-13 | 2010-01-20 | Rolls Royce Plc | Bladed rotor balancing |
FR2921099B1 (fr) * | 2007-09-13 | 2013-12-06 | Snecma | Dispositif d'amortissement pour aube en materiau composite |
FR2943102B1 (fr) * | 2009-03-12 | 2014-05-02 | Snecma | Aube en materiau composite comportant un dispositif d'amortissement. |
US8083489B2 (en) * | 2009-04-16 | 2011-12-27 | United Technologies Corporation | Hybrid structure fan blade |
US20120324901A1 (en) * | 2011-06-23 | 2012-12-27 | United Technologies Corporation | Tandem fan-turbine rotor for a tip turbine engine |
US20130078103A1 (en) * | 2011-09-23 | 2013-03-28 | Christopher S. McKaveney | Hollow fan blade rib geometry |
DE102015203868A1 (de) | 2015-03-04 | 2016-09-08 | Rolls-Royce Deutschland Ltd & Co Kg | Fanschaufel für einen Flugantrieb |
US10677068B2 (en) * | 2018-01-18 | 2020-06-09 | Raytheon Technologies Corporation | Fan blade with filled pocket |
FR3081370B1 (fr) * | 2018-05-22 | 2020-06-05 | Safran Aircraft Engines | Corps d'aube et aube en materiau composite ayant un renfort fibreux compose d'un tissage tridimensionnel et de fibres courtes et leur procede de fabrication |
US10995631B2 (en) * | 2019-04-01 | 2021-05-04 | Pratt & Whitney Canada Corp. | Method of shedding ice and fan blade |
US11220913B2 (en) * | 2019-10-23 | 2022-01-11 | Rolls-Royce Corporation | Gas turbine engine blades with airfoil plugs for selected tuning |
US11572796B2 (en) | 2020-04-17 | 2023-02-07 | Raytheon Technologies Corporation | Multi-material vane for a gas turbine engine |
US11795831B2 (en) | 2020-04-17 | 2023-10-24 | Rtx Corporation | Multi-material vane for a gas turbine engine |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2412615A (en) * | 1943-04-16 | 1946-12-17 | Gen Electric | Bladed machine element |
US2933286A (en) * | 1954-09-15 | 1960-04-19 | Gen Electric | Damping turbine buckets |
US3357850A (en) * | 1963-05-09 | 1967-12-12 | Gen Electric | Vibration damping turbomachinery blade |
GB1040825A (en) * | 1965-04-20 | 1966-09-01 | Rolls Royce | Improvements in rotor blades and/or stator blades for gas turbine engines |
US3796513A (en) * | 1972-06-19 | 1974-03-12 | Westinghouse Electric Corp | High damping blades |
US4118147A (en) * | 1976-12-22 | 1978-10-03 | General Electric Company | Composite reinforcement of metallic airfoils |
US4178667A (en) * | 1978-03-06 | 1979-12-18 | General Motors Corporation | Method of controlling turbomachine blade flutter |
FR2688264A1 (fr) * | 1992-03-04 | 1993-09-10 | Snecma | Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite. |
FR2695163B1 (fr) * | 1992-09-02 | 1994-10-28 | Snecma | Aube creuse pour turbomachine et son procédé de fabrication. |
US5655883A (en) * | 1995-09-25 | 1997-08-12 | General Electric Company | Hybrid blade for a gas turbine |
US5634771A (en) * | 1995-09-25 | 1997-06-03 | General Electric Company | Partially-metallic blade for a gas turbine |
US5947688A (en) * | 1997-12-22 | 1999-09-07 | General Electric Company | Frequency tuned hybrid blade |
-
1997
- 1997-12-22 US US08/995,979 patent/US5913661A/en not_active Expired - Fee Related
-
1998
- 1998-10-21 DE DE69812051T patent/DE69812051D1/de not_active Expired - Lifetime
- 1998-10-21 JP JP10298996A patent/JPH11201089A/ja active Pending
- 1998-10-21 EP EP98308625A patent/EP0924380B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0924380A2 (de) | 1999-06-23 |
US5913661A (en) | 1999-06-22 |
EP0924380A3 (de) | 2000-02-23 |
JPH11201089A (ja) | 1999-07-27 |
EP0924380B1 (de) | 2003-03-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8332 | No legal effect for de |