FR1598028A - - Google Patents
Info
- Publication number
- FR1598028A FR1598028A FR1598028DA FR1598028A FR 1598028 A FR1598028 A FR 1598028A FR 1598028D A FR1598028D A FR 1598028DA FR 1598028 A FR1598028 A FR 1598028A
- 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
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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 |
---|---|---|---|
GB58478/67A GB1186240A (en) | 1967-12-22 | 1967-12-22 | Improvements in Blades for Fluid Flow Machines. |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1598028A true FR1598028A (en) | 1970-06-29 |
Family
ID=10481718
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1598028D Expired FR1598028A (en) | 1967-12-22 | 1968-12-23 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3576377A (en) |
DE (1) | DE1816066B2 (en) |
FR (1) | FR1598028A (en) |
GB (1) | GB1186240A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2440466A1 (en) * | 1978-11-02 | 1980-05-30 | Gen Electric | DAWN OF IMPROVED TURBOMACHINE |
FR3111158A1 (en) * | 2020-06-04 | 2021-12-10 | Safran Aircraft Engines | Removable anti-wear part for dawn heel |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1419381A (en) * | 1972-03-09 | 1975-12-31 | Rolls Royce | Fan for gas turbine engines |
US4576551A (en) * | 1982-06-17 | 1986-03-18 | The Garrett Corporation | Turbo machine blading |
US4460316A (en) | 1982-12-29 | 1984-07-17 | Westinghouse Electric Corp. | Blade group with pinned root |
DE3413628C2 (en) * | 1983-04-25 | 1996-09-19 | Gen Electric | Gap seal for a steam turbine |
FR2552159B1 (en) * | 1983-09-21 | 1987-07-10 | Snecma | DEVICE FOR CONNECTING AND SEALING TURBINE STATOR BLADE SECTIONS |
EP0214393B1 (en) * | 1985-08-31 | 1989-12-13 | BBC Brown Boveri AG | Antivibration device for turbo machine blades |
US4815938A (en) * | 1987-12-24 | 1989-03-28 | Westinghouse Electric Corp. | Shroud gap control for integral shrouded blades |
GB2223276B (en) * | 1988-09-30 | 1992-09-02 | Rolls Royce Plc | Turbine aerofoil blade |
US5083903A (en) * | 1990-07-31 | 1992-01-28 | General Electric Company | Shroud insert for turbomachinery blade |
US5137426A (en) * | 1990-08-06 | 1992-08-11 | General Electric Company | Blade shroud deformable protective coating |
US5324168A (en) * | 1993-05-13 | 1994-06-28 | Eastman Kodak Company | Use of stellite to prevent silver plateout |
US6786698B2 (en) * | 2002-12-19 | 2004-09-07 | General Electric Company | Steam turbine bucket flowpath |
US7001152B2 (en) * | 2003-10-09 | 2006-02-21 | Pratt & Wiley Canada Corp. | Shrouded turbine blades with locally increased contact faces |
EP1591625A1 (en) * | 2004-04-30 | 2005-11-02 | ALSTOM Technology Ltd | Gas turbine blade shroud |
EP1767744A1 (en) * | 2005-09-22 | 2007-03-28 | Siemens Aktiengesellschaft | Shrouded turbine blades comprising a welded hardface cladding and process of manufacture |
US8182228B2 (en) * | 2007-08-16 | 2012-05-22 | General Electric Company | Turbine blade having midspan shroud with recessed wear pad and methods for manufacture |
RU2010150602A (en) * | 2010-12-09 | 2012-06-20 | Альстом Текнолоджи Лтд (Ch) | ROTOR BLADE BANDAGE |
US20120195742A1 (en) * | 2011-01-28 | 2012-08-02 | Jain Sanjeev Kumar | Turbine bucket for use in gas turbine engines and methods for fabricating the same |
US9163519B2 (en) * | 2011-07-28 | 2015-10-20 | General Electric Company | Cap for ceramic blade tip shroud |
US8894368B2 (en) * | 2012-01-04 | 2014-11-25 | General Electric Company | Device and method for aligning tip shrouds |
CN103089322B (en) * | 2013-01-29 | 2015-04-22 | 杭州汽轮机股份有限公司 | Damp lashing strip structure of industrial steam turbine high load short vane |
US9683446B2 (en) | 2013-03-07 | 2017-06-20 | Rolls-Royce Energy Systems, Inc. | Gas turbine engine shrouded blade |
FR3066780B1 (en) * | 2017-05-24 | 2019-07-19 | Safran Aircraft Engines | ANTI-WEAR REMOVABLE PIECE FOR DAWN HEEL |
US10294801B2 (en) * | 2017-07-25 | 2019-05-21 | United Technologies Corporation | Rotor blade having anti-wear surface |
FR3086692B1 (en) * | 2018-09-28 | 2022-07-29 | Safran Aircraft Engines | TURBOMACHINE BLADE EQUIPPED WITH AN ANTI-WEAR INSERT |
US11739645B2 (en) | 2020-09-30 | 2023-08-29 | General Electric Company | Vibrational dampening elements |
US11536144B2 (en) | 2020-09-30 | 2022-12-27 | General Electric Company | Rotor blade damping structures |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1159965B (en) * | 1961-08-10 | 1963-12-27 | Bbc Brown Boveri & Cie | Device for vibration damping on a turbine or compressor blade ring |
US3304056A (en) * | 1965-03-19 | 1967-02-14 | Hitachi Ltd | Turbine blades |
-
1967
- 1967-12-22 GB GB58478/67A patent/GB1186240A/en not_active Expired
-
1968
- 1968-12-13 US US783632A patent/US3576377A/en not_active Expired - Lifetime
- 1968-12-20 DE DE19681816066 patent/DE1816066B2/en not_active Withdrawn
- 1968-12-23 FR FR1598028D patent/FR1598028A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2440466A1 (en) * | 1978-11-02 | 1980-05-30 | Gen Electric | DAWN OF IMPROVED TURBOMACHINE |
FR3111158A1 (en) * | 2020-06-04 | 2021-12-10 | Safran Aircraft Engines | Removable anti-wear part for dawn heel |
Also Published As
Publication number | Publication date |
---|---|
DE1816066B2 (en) | 1970-11-05 |
US3576377A (en) | 1971-04-27 |
GB1186240A (en) | 1970-04-02 |
DE1816066A1 (en) | 1969-08-07 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
TP | Transmission of property | ||
TP | Transmission of property | ||
ST | Notification of lapse |