IT971440B - CLOSING AND DAMPING MEANS INSERTED BETWEEN ROTARY VANES FOR GAS TURBOMOTORS - Google Patents
CLOSING AND DAMPING MEANS INSERTED BETWEEN ROTARY VANES FOR GAS TURBOMOTORSInfo
- Publication number
- IT971440B IT971440B IT32376/72A IT3237672A IT971440B IT 971440 B IT971440 B IT 971440B IT 32376/72 A IT32376/72 A IT 32376/72A IT 3237672 A IT3237672 A IT 3237672A IT 971440 B IT971440 B IT 971440B
- Authority
- IT
- Italy
- Prior art keywords
- turbomotors
- closing
- gas
- damping means
- means inserted
- Prior art date
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
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fluid-Damping Devices (AREA)
- Centrifugal Separators (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20404971A | 1971-12-02 | 1971-12-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
IT971440B true IT971440B (en) | 1974-04-30 |
Family
ID=22756409
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT32376/72A IT971440B (en) | 1971-12-02 | 1972-12-01 | CLOSING AND DAMPING MEANS INSERTED BETWEEN ROTARY VANES FOR GAS TURBOMOTORS |
Country Status (8)
Country | Link |
---|---|
US (1) | US3751183A (en) |
JP (1) | JPS5517204B2 (en) |
BE (1) | BE791375A (en) |
CA (1) | CA951644A (en) |
DE (1) | DE2258604C2 (en) |
FR (1) | FR2164196A5 (en) |
GB (1) | GB1410607A (en) |
IT (1) | IT971440B (en) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3887298A (en) * | 1974-05-30 | 1975-06-03 | United Aircraft Corp | Apparatus for sealing turbine blade damper cavities |
US4088421A (en) * | 1976-09-30 | 1978-05-09 | General Electric Company | Coverplate damping arrangement |
US4101245A (en) * | 1976-12-27 | 1978-07-18 | United Technologies Corporation | Interblade damper and seal for turbomachinery rotor |
GB1549152A (en) * | 1977-01-11 | 1979-08-01 | Rolls Royce | Rotor stage for a gas trubine engine |
US4182598A (en) * | 1977-08-29 | 1980-01-08 | United Technologies Corporation | Turbine blade damper |
US4192633A (en) * | 1977-12-28 | 1980-03-11 | General Electric Company | Counterweighted blade damper |
GB2043796B (en) * | 1979-03-10 | 1983-04-20 | Rolls Royce | Bladed rotor for gas turbine engine |
GB2043797A (en) * | 1979-03-10 | 1980-10-08 | Rolls Royce | Bladed Rotor for Gas Turbine Engine |
US4279572A (en) * | 1979-07-09 | 1981-07-21 | United Technologies Corporation | Sideplates for rotor disk and rotor blades |
US4626169A (en) * | 1983-12-13 | 1986-12-02 | United Technologies Corporation | Seal means for a blade attachment slot of a rotor assembly |
US4872810A (en) * | 1988-12-14 | 1989-10-10 | United Technologies Corporation | Turbine rotor retention system |
FR2669686B1 (en) * | 1990-11-28 | 1994-09-02 | Snecma | BLOWER ROTOR WITH BLADES WITHOUT PLATFORMS AND SHOES RECONSTRUCTING THE VEIN PROFILE. |
US5201849A (en) * | 1990-12-10 | 1993-04-13 | General Electric Company | Turbine rotor seal body |
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 |
US5388962A (en) * | 1993-10-15 | 1995-02-14 | General Electric Company | Turbine rotor disk post cooling system |
US5478207A (en) * | 1994-09-19 | 1995-12-26 | General Electric Company | Stable blade vibration damper for gas turbine engine |
US5513955A (en) * | 1994-12-14 | 1996-05-07 | United Technologies Corporation | Turbine engine rotor blade platform seal |
US5573375A (en) * | 1994-12-14 | 1996-11-12 | United Technologies Corporation | Turbine engine rotor blade platform sealing and vibration damping device |
US5827047A (en) * | 1996-06-27 | 1998-10-27 | United Technologies Corporation | Turbine blade damper and seal |
US5924699A (en) * | 1996-12-24 | 1999-07-20 | United Technologies Corporation | Turbine blade platform seal |
US5785499A (en) * | 1996-12-24 | 1998-07-28 | United Technologies Corporation | Turbine blade damper and seal |
US6042336A (en) * | 1998-11-25 | 2000-03-28 | United Technologies Corporation | Offset center of gravity radial damper |
GB2344383B (en) * | 1998-12-01 | 2002-06-26 | Rolls Royce Plc | A bladed rotor |
US6273683B1 (en) | 1999-02-05 | 2001-08-14 | Siemens Westinghouse Power Corporation | Turbine blade platform seal |
US6409472B1 (en) * | 1999-08-09 | 2002-06-25 | United Technologies Corporation | Stator assembly for a rotary machine and clip member for a stator assembly |
GB0109033D0 (en) | 2001-04-10 | 2001-05-30 | Rolls Royce Plc | Vibration damping |
US7762780B2 (en) * | 2007-01-25 | 2010-07-27 | Siemens Energy, Inc. | Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies |
US8137072B2 (en) * | 2008-10-31 | 2012-03-20 | Solar Turbines Inc. | Turbine blade including a seal pocket |
US8393869B2 (en) * | 2008-12-19 | 2013-03-12 | Solar Turbines Inc. | Turbine blade assembly including a damper |
DE102009011964A1 (en) * | 2009-03-05 | 2010-09-09 | Mtu Aero Engines Gmbh | Rotor for a turbomachine |
DE102009011879A1 (en) * | 2009-03-05 | 2010-09-16 | Mtu Aero Engines Gmbh | Integrally bladed rotor and method of making an integrally bladed rotor |
US8696320B2 (en) * | 2009-03-12 | 2014-04-15 | General Electric Company | Gas turbine having seal assembly with coverplate and seal |
US20100232939A1 (en) * | 2009-03-12 | 2010-09-16 | General Electric Company | Machine Seal Assembly |
US8419370B2 (en) * | 2009-06-25 | 2013-04-16 | Rolls-Royce Corporation | Retaining and sealing ring assembly |
US8371816B2 (en) * | 2009-07-31 | 2013-02-12 | General Electric Company | Rotor blades for turbine engines |
US8469670B2 (en) * | 2009-08-27 | 2013-06-25 | Rolls-Royce Corporation | Fan assembly |
US8435006B2 (en) * | 2009-09-30 | 2013-05-07 | Rolls-Royce Corporation | Fan |
DE102010015211B4 (en) * | 2010-04-16 | 2013-06-20 | Mtu Aero Engines Gmbh | Damping element for damping blade vibrations, blade and rotor |
EP2434098A1 (en) * | 2010-09-24 | 2012-03-28 | Siemens Aktiengesellschaft | Blade assembly and corresponding gas turbine |
FR2972482B1 (en) * | 2011-03-07 | 2016-07-29 | Snecma | TURBINE STAGE FOR AIRCRAFT TURBOMACHINE HAVING IMPROVED SEAL BETWEEN THE FLASK DOWN AND THE TURBINE BLADES BY MECHANICAL RETENTION |
EP2520768A1 (en) * | 2011-05-02 | 2012-11-07 | MTU Aero Engines AG | Sealing device for an integrated bladed rotor base body of a turbomachine |
US9650901B2 (en) | 2012-05-31 | 2017-05-16 | Solar Turbines Incorporated | Turbine damper |
US9279332B2 (en) | 2012-05-31 | 2016-03-08 | Solar Turbines Incorporated | Turbine damper |
FR2991372B1 (en) * | 2012-06-04 | 2014-05-16 | Snecma | TURBINE WHEEL IN A TURBOMACHINE |
US9347325B2 (en) * | 2012-10-31 | 2016-05-24 | Solar Turbines Incorporated | Damper for a turbine rotor assembly |
US9297263B2 (en) * | 2012-10-31 | 2016-03-29 | Solar Turbines Incorporated | Turbine blade for a gas turbine engine |
US9303519B2 (en) * | 2012-10-31 | 2016-04-05 | Solar Turbines Incorporated | Damper for a turbine rotor assembly |
US9228443B2 (en) * | 2012-10-31 | 2016-01-05 | Solar Turbines Incorporated | Turbine rotor assembly |
EP3073052B1 (en) * | 2015-02-17 | 2018-01-24 | Rolls-Royce Corporation | Fan assembly |
US10533445B2 (en) * | 2016-08-23 | 2020-01-14 | United Technologies Corporation | Rim seal for gas turbine engine |
US10975714B2 (en) * | 2018-11-22 | 2021-04-13 | Pratt & Whitney Canada Corp. | Rotor assembly with blade sealing tab |
FR3096734B1 (en) * | 2019-05-29 | 2021-12-31 | Safran Aircraft Engines | Turbomachine kit |
RU2764565C1 (en) * | 2021-03-05 | 2022-01-18 | Акционерное общество "Силовые машины - ЗТЛ, ЛМЗ, Электросила, Энергомашэкспорт" (АО "Силовые машины") | Damper seal of the gas turbine impeller |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR989556A (en) * | 1949-06-25 | 1951-09-11 | Cem Comp Electro Mec | Improvement in turbo-machine blades |
FR1263677A (en) * | 1960-07-29 | 1961-06-09 | Havilland Engine Co Ltd | Anti-vibration device applicable to rotating parts |
US3119595A (en) * | 1961-02-23 | 1964-01-28 | Gen Electric | Bladed rotor and baffle assembly |
US3266770A (en) * | 1961-12-22 | 1966-08-16 | Gen Electric | Turbomachine rotor assembly |
US3112915A (en) * | 1961-12-22 | 1963-12-03 | Gen Electric | Rotor assembly air baffle |
US3181835A (en) * | 1964-01-07 | 1965-05-04 | Carroll C Davis | Blade vibration damping device |
CH494896A (en) * | 1968-08-09 | 1970-08-15 | Sulzer Ag | Mounting of rotor blades in the rotor of a turbomachine |
US3666376A (en) * | 1971-01-05 | 1972-05-30 | United Aircraft Corp | Turbine blade damper |
-
0
- BE BE791375D patent/BE791375A/en unknown
-
1971
- 1971-12-02 US US00204049A patent/US3751183A/en not_active Expired - Lifetime
-
1972
- 1972-11-24 GB GB5433172A patent/GB1410607A/en not_active Expired
- 1972-11-28 CA CA157,652,A patent/CA951644A/en not_active Expired
- 1972-11-30 FR FR7242565A patent/FR2164196A5/fr not_active Expired
- 1972-11-30 DE DE2258604A patent/DE2258604C2/en not_active Expired
- 1972-12-01 IT IT32376/72A patent/IT971440B/en active
- 1972-12-01 JP JP11991972A patent/JPS5517204B2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2258604A1 (en) | 1973-06-07 |
BE791375A (en) | 1973-03-01 |
DE2258604C2 (en) | 1981-10-08 |
US3751183A (en) | 1973-08-07 |
JPS4864303A (en) | 1973-09-06 |
JPS5517204B2 (en) | 1980-05-09 |
GB1410607A (en) | 1975-10-22 |
CA951644A (en) | 1974-07-23 |
FR2164196A5 (en) | 1973-07-27 |
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