RU2001130175A - Stator ring ventilation assembly - Google Patents
Stator ring ventilation assemblyInfo
- Publication number
- RU2001130175A RU2001130175A RU2001130175/06A RU2001130175A RU2001130175A RU 2001130175 A RU2001130175 A RU 2001130175A RU 2001130175/06 A RU2001130175/06 A RU 2001130175/06A RU 2001130175 A RU2001130175 A RU 2001130175A RU 2001130175 A RU2001130175 A RU 2001130175A
- Authority
- RU
- Russia
- Prior art keywords
- stator ring
- ventilation unit
- collectors
- ring according
- stator
- Prior art date
Links
- 238000009423 ventilation Methods 0.000 title claims 8
- 230000037250 Clearance Effects 0.000 claims 1
- 210000001503 Joints Anatomy 0.000 claims 1
- 230000035512 clearance Effects 0.000 claims 1
- 230000000284 resting Effects 0.000 claims 1
Claims (7)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0014373 | 2000-11-09 | ||
FR0014373A FR2816352B1 (en) | 2000-11-09 | 2000-11-09 | VENTILATION ASSEMBLY OF A STATOR RING |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2001130175A true RU2001130175A (en) | 2003-07-10 |
RU2276733C2 RU2276733C2 (en) | 2006-05-20 |
Family
ID=8856230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2001130175/06A RU2276733C2 (en) | 2000-11-09 | 2001-11-08 | Stator ring ventilating unit |
Country Status (9)
Country | Link |
---|---|
US (1) | US6896038B2 (en) |
EP (1) | EP1205637B1 (en) |
JP (1) | JP3913032B2 (en) |
CA (1) | CA2361103C (en) |
DE (1) | DE60100448T2 (en) |
ES (1) | ES2199921T3 (en) |
FR (1) | FR2816352B1 (en) |
RU (1) | RU2276733C2 (en) |
UA (1) | UA73938C2 (en) |
Families Citing this family (41)
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FR2829525B1 (en) * | 2001-09-13 | 2004-03-12 | Snecma Moteurs | ASSEMBLY OF SECTORS OF A TURBINE DISTRIBUTOR TO A CRANKCASE |
FR2865237B1 (en) * | 2004-01-16 | 2006-03-10 | Snecma Moteurs | IMPROVEMENTS IN GAME CONTROL DEVICES IN A GAS TURBINE |
FR2867806B1 (en) * | 2004-03-18 | 2006-06-02 | Snecma Moteurs | DEVICE FOR CONTROLLING GAS TURBINE SET WITH AIR FLOW BALANCING |
FR2867805A1 (en) * | 2004-03-18 | 2005-09-23 | Snecma Moteurs | TURBOMACHINE HIGH-PRESSURE TURBINE STATOR AND METHOD OF ASSEMBLY |
US7597537B2 (en) * | 2005-12-16 | 2009-10-06 | General Electric Company | Thermal control of gas turbine engine rings for active clearance control |
US7503179B2 (en) * | 2005-12-16 | 2009-03-17 | General Electric Company | System and method to exhaust spent cooling air of gas turbine engine active clearance control |
US7785063B2 (en) * | 2006-12-15 | 2010-08-31 | Siemens Energy, Inc. | Tip clearance control |
US7914254B2 (en) * | 2007-02-13 | 2011-03-29 | General Electric Company | Integrated support/thermocouple housing for impingement cooling manifolds and cooling method |
FR2931872B1 (en) * | 2008-05-28 | 2010-08-20 | Snecma | HIGH PRESSURE TURBINE OF A TURBOMACHINE WITH IMPROVED MOUNTING OF THE PILOTAGE HOUSING OF THE MOBILE RADIAL GAMES. |
GB0906059D0 (en) * | 2009-04-08 | 2009-05-20 | Rolls Royce Plc | Thermal control system for turbines |
GB2469490B (en) * | 2009-04-16 | 2012-03-07 | Rolls Royce Plc | Turbine casing cooling |
GB201013723D0 (en) * | 2010-08-17 | 2010-09-29 | Rolls Royce Plc | Manifold mounting arrangement |
FR2977276B1 (en) * | 2011-06-30 | 2016-12-09 | Snecma | ARRANGEMENT FOR CONNECTING A DUCT TO AN AIR DISTRIBUTION HOUSING |
ITTO20120519A1 (en) | 2012-06-14 | 2013-12-15 | Avio Spa | GAS TURBINE FOR AERONAUTICAL MOTORS |
US9341074B2 (en) | 2012-07-25 | 2016-05-17 | General Electric Company | Active clearance control manifold system |
FR2999642B1 (en) * | 2012-12-17 | 2018-09-28 | Safran Aircraft Engines | STATORIC ASSEMBLY HAVING DAMAGE WITH HOLLOW OR HIGH PORTIONS |
US10330012B2 (en) * | 2014-02-04 | 2019-06-25 | United Technologies Corporation | Brackets for gas turbine engine components |
RU2567892C1 (en) * | 2014-06-02 | 2015-11-10 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | High-pressure compressor stator |
US9869196B2 (en) * | 2014-06-24 | 2018-01-16 | General Electric Company | Gas turbine engine spring mounted manifold |
RU2567885C1 (en) * | 2014-08-08 | 2015-11-10 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Compressor stator |
FR3040429B1 (en) * | 2015-08-27 | 2019-06-07 | Safran Aircraft Engines | DEVICE FOR FASTENING AIR COOLED COOLING RAMPS OF A TURBOMACHINE TURBINE |
FR3040428B1 (en) * | 2015-08-27 | 2017-09-01 | Snecma | DEVICE FOR COOLING AIR JETS OF THE CARTER OF A TURBINE OF A TURBOMACHINE |
US10513944B2 (en) * | 2015-12-21 | 2019-12-24 | General Electric Company | Manifold for use in a clearance control system and method of manufacturing |
US10329941B2 (en) * | 2016-05-06 | 2019-06-25 | United Technologies Corporation | Impingement manifold |
CN107795383B (en) * | 2016-08-29 | 2019-08-06 | 中国航发商用航空发动机有限责任公司 | A kind of gas turbine cooling air distribution system |
FR3058459B1 (en) | 2016-11-04 | 2018-11-09 | Safran Aircraft Engines | COOLING DEVICE FOR TURBINE OF A TURBOMACHINE |
FR3058460B1 (en) | 2016-11-08 | 2018-11-09 | Safran Aircraft Engines | CONNECTION ASSEMBLY FOR COOLING TURBOMACHINE TURBINE |
CN106382136B (en) * | 2016-11-18 | 2017-07-25 | 中国科学院工程热物理研究所 | A kind of transonic speed tip active control device |
US10458281B2 (en) * | 2017-06-12 | 2019-10-29 | United Technologies Corporation | Resilient mounting assembly for a turbine engine |
FR3073007B1 (en) * | 2017-10-27 | 2019-09-27 | Safran Aircraft Engines | DEVICE FOR HOLDING A COOLING TUBE FOR A TURBOMACHINE HOUSING |
FR3079874B1 (en) * | 2018-04-09 | 2020-03-13 | Safran Aircraft Engines | COOLING DEVICE FOR A TURBINE OF A TURBOMACHINE |
FR3081927B1 (en) * | 2018-05-30 | 2020-11-20 | Safran Aircraft Engines | TURBOMACHINE CASING COOLING SYSTEM |
FR3082872B1 (en) * | 2018-06-25 | 2021-06-04 | Safran Aircraft Engines | TURBOMACHINE CASE COOLING SYSTEM |
FR3089560B1 (en) * | 2018-12-06 | 2021-01-22 | Safran Aircraft Engines | Device for maintaining a cooling tube for a turbomachine casing |
FR3089545B1 (en) * | 2018-12-07 | 2021-01-29 | Safran Aircraft Engines | Device for cooling a turbine housing for a turbomachine |
FR3089544B1 (en) * | 2018-12-10 | 2021-02-19 | Safran Aircraft Engines | TURBOMACHINE CASE COOLING DEVICE |
FR3099798B1 (en) * | 2019-08-09 | 2021-12-03 | Safran Aircraft Engines | Set for a turbomachine turbine |
FR3099801B1 (en) * | 2019-08-09 | 2021-12-03 | Safran Aircraft Engines | Set for a turbomachine turbine |
FR3109406B1 (en) * | 2020-04-17 | 2022-10-07 | Safran Aircraft Engines | TURBINE CASE COOLING DEVICE |
US11788425B2 (en) * | 2021-11-05 | 2023-10-17 | General Electric Company | Gas turbine engine with clearance control system |
US12006829B1 (en) | 2023-02-16 | 2024-06-11 | General Electric Company | Seal member support system for a gas turbine engine |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1601187A1 (en) * | 1967-07-15 | 1972-01-27 | Eberspaecher J | Heat exchanger, preferably with an internal boiler room, especially for motor vehicles |
US3756020A (en) * | 1972-06-26 | 1973-09-04 | Curtiss Wright Corp | Gas turbine engine and cooling system therefor |
US3818696A (en) * | 1972-10-25 | 1974-06-25 | A Beaufrere | Regenerative air-cooled gas turbine engine |
US4279123A (en) * | 1978-12-20 | 1981-07-21 | United Technologies Corporation | External gas turbine engine cooling for clearance control |
DE2855055C2 (en) * | 1978-12-20 | 1982-12-16 | Siemens AG, 1000 Berlin und 8000 München | Insulating sleeve for a laminated core to be wound with a ring winding |
US4773981A (en) * | 1982-07-29 | 1988-09-27 | Stephen Masiuk | Apparatus for improving internal combustion engine efficiency |
US4828403A (en) * | 1987-04-03 | 1989-05-09 | Schwartzman Everett H | Resiliently mounted fluid bearing assembly |
JPH06575Y2 (en) * | 1988-06-16 | 1994-01-05 | 川崎重工業株式会社 | Muffler for internal combustion engine |
US5100291A (en) * | 1990-03-28 | 1992-03-31 | General Electric Company | Impingement manifold |
US5205115A (en) * | 1991-11-04 | 1993-04-27 | General Electric Company | Gas turbine engine case counterflow thermal control |
US5273396A (en) * | 1992-06-22 | 1993-12-28 | General Electric Company | Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud |
US5399066A (en) * | 1993-09-30 | 1995-03-21 | General Electric Company | Integral clearance control impingement manifold and environmental shield |
FR2750451B1 (en) * | 1996-06-27 | 1998-08-07 | Snecma | DEVICE FOR BLOWING GAS ADJUSTING GAMES IN A TURBOMACHINE |
FR2766517B1 (en) * | 1997-07-24 | 1999-09-03 | Snecma | DEVICE FOR VENTILATION OF A TURBOMACHINE RING |
FR2800797B1 (en) * | 1999-11-10 | 2001-12-07 | Snecma | ASSEMBLY OF A RING BORDING A TURBINE TO THE TURBINE STRUCTURE |
FR2803871B1 (en) * | 2000-01-13 | 2002-06-07 | Snecma Moteurs | DIAMETER ADJUSTMENT ARRANGEMENT OF A GAS TURBINE STATOR |
DE10026355B4 (en) * | 2000-05-27 | 2010-06-17 | Mahle Filtersysteme Gmbh | Sound-absorbing air duct |
FR2817290B1 (en) * | 2000-11-30 | 2003-02-21 | Snecma Moteurs | ROTOR BLADE DISC FLANGE AND CORRESPONDING ARRANGEMENT |
FR2819010B1 (en) * | 2001-01-04 | 2004-05-28 | Snecma Moteurs | STATOR RING SUPPORT AREA OF THE TURBINE HIGH PRESSURE TURBINE ROTATOR WITH A TURBOMACHINE |
FR2831918B1 (en) * | 2001-11-08 | 2004-05-28 | Snecma Moteurs | STATOR FOR TURBOMACHINE |
-
2000
- 2000-11-09 FR FR0014373A patent/FR2816352B1/en not_active Expired - Fee Related
-
2001
- 2001-10-26 JP JP2001328678A patent/JP3913032B2/en not_active Expired - Fee Related
- 2001-11-06 CA CA002361103A patent/CA2361103C/en not_active Expired - Fee Related
- 2001-11-08 UA UA2001117658A patent/UA73938C2/en unknown
- 2001-11-08 EP EP01402865A patent/EP1205637B1/en not_active Expired - Lifetime
- 2001-11-08 DE DE60100448T patent/DE60100448T2/en not_active Expired - Lifetime
- 2001-11-08 RU RU2001130175/06A patent/RU2276733C2/en not_active IP Right Cessation
- 2001-11-08 ES ES01402865T patent/ES2199921T3/en not_active Expired - Lifetime
- 2001-11-08 US US09/986,280 patent/US6896038B2/en not_active Expired - Lifetime
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