FR2376958B1 - - Google Patents
Info
- Publication number
- FR2376958B1 FR2376958B1 FR7800347A FR7800347A FR2376958B1 FR 2376958 B1 FR2376958 B1 FR 2376958B1 FR 7800347 A FR7800347 A FR 7800347A FR 7800347 A FR7800347 A FR 7800347A FR 2376958 B1 FR2376958 B1 FR 2376958B1
- Authority
- FR
- France
- 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
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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB862/77A GB1549152A (en) | 1977-01-11 | 1977-01-11 | Rotor stage for a gas trubine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2376958A1 FR2376958A1 (fr) | 1978-08-04 |
| FR2376958B1 true FR2376958B1 (US08124317-20120228-C00060.png) | 1984-06-08 |
Family
ID=9711790
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7800347A Granted FR2376958A1 (fr) | 1977-01-11 | 1978-01-06 | Etage mobile de compresseur |
Country Status (6)
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4326835A (en) * | 1979-10-29 | 1982-04-27 | General Motors Corporation | Blade platform seal for ceramic/metal rotor assembly |
| US4326836A (en) * | 1979-12-13 | 1982-04-27 | United Technologies Corporation | Shroud for a rotor blade |
| FR2517779B1 (fr) * | 1981-12-03 | 1986-06-13 | Snecma | Dispositif d'amortissement des aubes d'une soufflante de turbomachine |
| FR2527260A1 (fr) * | 1982-05-18 | 1983-11-25 | Snecma | Dispositif d'amortissement escamotable pour aubes d'une turbomachine |
| US4505642A (en) * | 1983-10-24 | 1985-03-19 | United Technologies Corporation | Rotor blade interplatform seal |
| US4580946A (en) * | 1984-11-26 | 1986-04-08 | General Electric Company | Fan blade platform seal |
| US4743166A (en) * | 1984-12-20 | 1988-05-10 | General Electric Company | Blade root seal |
| JPS62125052U (US08124317-20120228-C00060.png) * | 1986-01-31 | 1987-08-08 | ||
| US4743164A (en) * | 1986-12-29 | 1988-05-10 | United Technologies Corporation | Interblade seal for turbomachine rotor |
| US4872812A (en) * | 1987-08-05 | 1989-10-10 | General Electric Company | Turbine blade plateform sealing and vibration damping apparatus |
| GB8819133D0 (en) * | 1988-08-11 | 1988-09-14 | Rolls Royce Plc | Bladed rotor assembly & sealing wire therefor |
| US4986737A (en) * | 1988-12-29 | 1991-01-22 | General Electric Company | Damped gas turbine engine airfoil row |
| US5281097A (en) * | 1992-11-20 | 1994-01-25 | General Electric Company | Thermal control damper for turbine rotors |
| US5313786A (en) * | 1992-11-24 | 1994-05-24 | United Technologies Corporation | Gas turbine blade damper |
| US5228835A (en) * | 1992-11-24 | 1993-07-20 | United Technologies Corporation | Gas turbine blade seal |
| US5573375A (en) * | 1994-12-14 | 1996-11-12 | United Technologies Corporation | Turbine engine rotor blade platform sealing and vibration damping device |
| FR2746456B1 (fr) * | 1996-03-21 | 1998-04-30 | Snecma | Dispositif de retenue du pied des aubes d'une soufflante |
| GB2311826B (en) * | 1996-04-02 | 2000-05-10 | Europ Gas Turbines Ltd | Turbomachines |
| US5820338A (en) * | 1997-04-24 | 1998-10-13 | United Technologies Corporation | Fan blade interplatform seal |
| US7121800B2 (en) * | 2004-09-13 | 2006-10-17 | United Technologies Corporation | Turbine blade nested seal damper assembly |
| DE102006041322A1 (de) * | 2006-09-01 | 2008-04-24 | Rolls-Royce Deutschland Ltd & Co Kg | Dämpfungs- und Dichtungssystem für Turbinenschaufeln |
| FR2915510B1 (fr) * | 2007-04-27 | 2009-11-06 | Snecma Sa | Amortisseur pour aubes de turbomachines |
| ES2381842T3 (es) * | 2007-10-25 | 2012-06-01 | Siemens Aktiengesellschaft | Conjunto ensamblado de álabes de turbina y junta de estanqueidad. |
| DE102009011964A1 (de) * | 2009-03-05 | 2010-09-09 | Mtu Aero Engines Gmbh | Rotor für eine Strömungsmaschine |
| FR2945074B1 (fr) | 2009-04-29 | 2011-06-03 | Snecma | Cale d'aube de soufflante renforcee |
| FR2962481B1 (fr) * | 2010-07-12 | 2012-08-31 | Snecma Propulsion Solide | Amortisseur de vibrations a bras de levier pour aube d'un rotor de moteur a turbine a gaz |
| US9022727B2 (en) * | 2010-11-15 | 2015-05-05 | Mtu Aero Engines Gmbh | Rotor for a turbo machine |
| FR2970033B1 (fr) * | 2011-01-04 | 2015-10-16 | Turbomeca | Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en oeuvre |
| GB2490858B (en) * | 2011-03-22 | 2014-01-01 | Rolls Royce Plc | A bladed rotor |
| US9103283B2 (en) | 2012-06-20 | 2015-08-11 | United Technologies Corporation | Spherical-link end damper system with near constant engagement |
| EP2679770A1 (en) * | 2012-06-26 | 2014-01-01 | Siemens Aktiengesellschaft | Platform seal strip for a gas turbine |
| FR3003294B1 (fr) * | 2013-03-15 | 2018-03-30 | Safran Aircraft Engines | Soufflante de turbomoteur a flux multiple, et turbomoteur equipe d'une telle soufflante |
| US10472975B2 (en) * | 2015-09-03 | 2019-11-12 | General Electric Company | Damper pin having elongated bodies for damping adjacent turbine blades |
| RU175943U1 (ru) * | 2016-09-19 | 2017-12-25 | Публичное акционерное общество "Научно-производственное объединение "Сатурн" | Ротор турбины |
| EP3438410B1 (en) | 2017-08-01 | 2021-09-29 | General Electric Company | Sealing system for a rotary machine |
| US11268397B2 (en) * | 2020-02-07 | 2022-03-08 | Raytheon Technologies Corporation | Fan blade platform seal and method for forming same |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB670665A (en) * | 1949-07-28 | 1952-04-23 | Rolls Royce | Improvements in or relating to compressors and turbines |
| DE1079073B (de) * | 1959-04-16 | 1960-04-07 | Maschf Augsburg Nuernberg Ag | Sicherung einer in einer Axialnut einer Laeuferscheibe gehaltenen Laufschaufel einer Stroemungsmaschine |
| GB996729A (en) * | 1963-12-16 | 1965-06-30 | Rolls Royce | Improvements relating to turbines and compressors |
| JPS427042Y1 (US08124317-20120228-C00060.png) * | 1966-11-08 | 1967-04-03 | ||
| US3451654A (en) * | 1967-08-25 | 1969-06-24 | Gen Motors Corp | Blade vibration damping |
| CH494896A (de) * | 1968-08-09 | 1970-08-15 | Sulzer Ag | Halterung von Laufschaufeln im Rotor einer Turbomaschine |
| GB1259750A (en) * | 1970-07-23 | 1972-01-12 | Rolls Royce | Rotor for a fluid flow machine |
| GB1318654A (en) * | 1970-12-05 | 1973-05-31 | Secr Defence | Bladed rotors |
| US3666376A (en) * | 1971-01-05 | 1972-05-30 | United Aircraft Corp | Turbine blade damper |
| US3709631A (en) * | 1971-03-18 | 1973-01-09 | Caterpillar Tractor Co | Turbine blade seal arrangement |
| BE791375A (fr) * | 1971-12-02 | 1973-03-01 | Gen Electric | Deflecteur et amortisseur pour ailettes de turbomachines |
| GB1428365A (en) * | 1972-03-15 | 1976-03-17 | Rolls Royce | Fluid flow machines |
| GB1460714A (en) * | 1973-06-26 | 1977-01-06 | Rolls Royce | Bladed rotor for a gas turbine engine |
| GB1457417A (en) * | 1973-06-30 | 1976-12-01 | Dunlop Ltd | Vibration damping means |
| US3936230A (en) * | 1974-05-09 | 1976-02-03 | The United States Of America As Represented By The Secretary Of The Air Force | Self-supported, self-locating seal for turbine engines |
-
1977
- 1977-01-11 GB GB862/77A patent/GB1549152A/en not_active Expired
-
1978
- 1978-01-06 FR FR7800347A patent/FR2376958A1/fr active Granted
- 1978-01-09 US US05/868,228 patent/US4177013A/en not_active Expired - Lifetime
- 1978-01-10 DE DE2800862A patent/DE2800862C3/de not_active Expired
- 1978-01-11 JP JP53001822A patent/JPS5813759B2/ja not_active Expired
- 1978-01-11 IT IT19167/78A patent/IT1091746B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| DE2800862A1 (de) | 1978-07-20 |
| DE2800862B2 (de) | 1980-01-17 |
| IT1091746B (it) | 1985-07-06 |
| US4177013A (en) | 1979-12-04 |
| GB1549152A (en) | 1979-08-01 |
| IT7819167A0 (it) | 1978-01-11 |
| JPS5813759B2 (ja) | 1983-03-15 |
| FR2376958A1 (fr) | 1978-08-04 |
| DE2800862C3 (de) | 1980-09-11 |
| JPS5395414A (en) | 1978-08-21 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |