FR2575221B1 - Stator refroidissable pour un moteur a turbine a gaz - Google Patents
Stator refroidissable pour un moteur a turbine a gazInfo
- Publication number
- FR2575221B1 FR2575221B1 FR858517735A FR8517735A FR2575221B1 FR 2575221 B1 FR2575221 B1 FR 2575221B1 FR 858517735 A FR858517735 A FR 858517735A FR 8517735 A FR8517735 A FR 8517735A FR 2575221 B1 FR2575221 B1 FR 2575221B1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- turbine engine
- coolable stator
- coolable
- stator
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/684,821 US4720236A (en) | 1984-12-21 | 1984-12-21 | Coolable stator assembly for a gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2575221A1 FR2575221A1 (fr) | 1986-06-27 |
FR2575221B1 true FR2575221B1 (fr) | 1990-05-11 |
Family
ID=24749715
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR858517735A Expired - Lifetime FR2575221B1 (fr) | 1984-12-21 | 1985-11-29 | Stator refroidissable pour un moteur a turbine a gaz |
Country Status (5)
Country | Link |
---|---|
US (1) | US4720236A (fr) |
JP (1) | JP2617707B2 (fr) |
DE (1) | DE3541606C2 (fr) |
FR (1) | FR2575221B1 (fr) |
GB (1) | GB2169038B (fr) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2192233B (en) * | 1986-07-02 | 1990-11-28 | Rolls Royce Plc | A gas turbine engine load transfer structure |
US4920742A (en) * | 1988-05-31 | 1990-05-01 | General Electric Company | Heat shield for gas turbine engine frame |
US4902198A (en) * | 1988-08-31 | 1990-02-20 | Westinghouse Electric Corp. | Apparatus for film cooling of turbine van shrouds |
US4890978A (en) * | 1988-10-19 | 1990-01-02 | Westinghouse Electric Corp. | Method and apparatus for vane segment support and alignment in combustion turbines |
JPH03213602A (ja) * | 1990-01-08 | 1991-09-19 | General Electric Co <Ge> | ガスタービンエンジンの当接セグメントを連結する自己冷却式ジョイント連結構造 |
FR2664647B1 (fr) * | 1990-07-12 | 1994-08-26 | Europ Propulsion | Distributeur, notamment pour turbine, a aubes fixes en materiau composite thermostructural, et procede de fabrication. |
US5118253A (en) * | 1990-09-12 | 1992-06-02 | United Technologies Corporation | Compressor case construction with backbone |
US5354174A (en) * | 1990-09-12 | 1994-10-11 | United Technologies Corporation | Backbone support structure for compressor |
US5088888A (en) * | 1990-12-03 | 1992-02-18 | General Electric Company | Shroud seal |
US5149250A (en) * | 1991-02-28 | 1992-09-22 | General Electric Company | Gas turbine vane assembly seal and support system |
US5176496A (en) * | 1991-09-27 | 1993-01-05 | General Electric Company | Mounting arrangements for turbine nozzles |
FR2685383B1 (fr) * | 1991-12-18 | 1994-02-11 | Snecma | Bras structural du carter d'une turbomachine. |
GB2267736B (en) * | 1992-06-09 | 1995-08-09 | Gen Electric | Segmented turbine flowpath assembly |
FR2695164B1 (fr) * | 1992-08-26 | 1994-11-04 | Snecma | Turbomachine munie d'un dispositif empêchant une circulation longitudinale de gaz autour des étages d'aubes de redressement. |
FR2743603B1 (fr) * | 1996-01-11 | 1998-02-13 | Snecma | Dispositif de jonction de segments d'un distributeur circulaire a un carter de turbomachine |
EP0903467B1 (fr) * | 1997-09-17 | 2004-07-07 | Mitsubishi Heavy Industries, Ltd. | Aubes statoriques accouplées |
KR20010049364A (ko) * | 1999-06-14 | 2001-06-15 | 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 | 시일 조립체 |
US7229245B2 (en) * | 2004-07-14 | 2007-06-12 | Power Systems Mfg., Llc | Vane platform rail configuration for reduced airfoil stress |
US7160078B2 (en) * | 2004-09-23 | 2007-01-09 | General Electric Company | Mechanical solution for rail retention of turbine nozzles |
US7762761B2 (en) * | 2005-11-30 | 2010-07-27 | General Electric Company | Methods and apparatus for assembling turbine nozzles |
GB0619426D0 (en) * | 2006-10-03 | 2006-11-08 | Rolls Royce Plc | A vane arrangement |
DE102007020025A1 (de) * | 2007-04-27 | 2008-10-30 | Honda Motor Co., Ltd. | Form eines Gaskanals in einer Axialströmungs-Gasturbinenmaschine |
US8051663B2 (en) | 2007-11-09 | 2011-11-08 | United Technologies Corp. | Gas turbine engine systems involving cooling of combustion section liners |
US8439636B1 (en) * | 2009-10-20 | 2013-05-14 | Florida Turbine Technologies, Inc. | Turbine blade outer air seal |
DE102010005153A1 (de) | 2010-01-21 | 2011-07-28 | MTU Aero Engines GmbH, 80995 | Gehäusesystem für eine Axialströmungsmaschine |
US8360716B2 (en) * | 2010-03-23 | 2013-01-29 | United Technologies Corporation | Nozzle segment with reduced weight flange |
US8794911B2 (en) * | 2010-03-30 | 2014-08-05 | United Technologies Corporation | Anti-rotation slot for turbine vane |
US8920113B2 (en) * | 2011-11-28 | 2014-12-30 | United Technologies Corporation | Thermal gradiant tolerant turbomachine coupling member |
WO2014150353A1 (fr) * | 2013-03-15 | 2014-09-25 | United Technologies Corporation | Segment de conduit à faible niveau de fuite utilisant un ensemble joint de dilatation |
JP5717904B1 (ja) * | 2014-08-04 | 2015-05-13 | 三菱日立パワーシステムズ株式会社 | 静翼、ガスタービン、分割環、静翼の改造方法、および、分割環の改造方法 |
EP3015657A1 (fr) * | 2014-10-31 | 2016-05-04 | Siemens Aktiengesellschaft | Segment d'ailette de guidage d'une turbomachine à gaz |
US10018075B2 (en) | 2015-04-22 | 2018-07-10 | General Electric Company | Methods for positioning neighboring nozzles of a gas turbine engine |
US11428241B2 (en) * | 2016-04-22 | 2022-08-30 | Raytheon Technologies Corporation | System for an improved stator assembly |
DE102016115610A1 (de) | 2016-08-23 | 2018-03-01 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbine und Verfahren zum Aufhängen eines Turbinen-Leitschaufelsegments einer Gasturbine |
GB201616197D0 (en) * | 2016-09-23 | 2016-11-09 | Rolls Royce Plc | Gas turbine engine |
US10557360B2 (en) * | 2016-10-17 | 2020-02-11 | United Technologies Corporation | Vane intersegment gap sealing arrangement |
US10557412B2 (en) * | 2017-05-30 | 2020-02-11 | United Technologies Corporation | Systems for reducing deflection of a shroud that retains fan exit stators |
US20190078469A1 (en) * | 2017-09-11 | 2019-03-14 | United Technologies Corporation | Fan exit stator assembly retention system |
KR101937586B1 (ko) * | 2017-09-12 | 2019-01-10 | 두산중공업 주식회사 | 베인 조립체, 터빈 및 이를 포함하는 가스터빈 |
US11085309B2 (en) | 2017-09-22 | 2021-08-10 | General Electric Company | Outer drum rotor assembly |
DE102020115106B4 (de) * | 2020-06-08 | 2022-08-25 | Man Energy Solutions Se | Turbinenleitapparat |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL99435C (fr) * | 1957-08-22 | |||
NL267395A (fr) * | 1960-07-22 | |||
GB1086432A (en) * | 1965-09-21 | 1967-10-11 | Bristol Siddeley Engines Ltd | Gas turbine engines |
US3443791A (en) * | 1966-11-23 | 1969-05-13 | United Aircraft Corp | Turbine vane assembly |
US4017213A (en) * | 1975-10-14 | 1977-04-12 | United Technologies Corporation | Turbomachinery vane or blade with cooled platforms |
JPS555682U (fr) * | 1978-06-28 | 1980-01-14 | ||
US4176433A (en) * | 1978-06-29 | 1979-12-04 | United Technologies Corporation | Method of remanufacturing turbine vane clusters for gas turbine engines |
FR2438165A1 (fr) * | 1978-10-06 | 1980-04-30 | Snecma | Dispositif de regulation de temperature pour turbines a gaz |
GB2037901B (en) * | 1978-11-25 | 1982-07-28 | Rolls Royce | Nozzle guide vane assembly |
GB2061396B (en) * | 1979-10-24 | 1983-05-18 | Rolls Royce | Turbine blade tip clearance control |
DE3003470C2 (de) * | 1980-01-31 | 1982-02-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turbinenleitschaufelaufhängung für Gasturbinenstrahltriebwerke |
US4485620A (en) * | 1982-03-03 | 1984-12-04 | United Technologies Corporation | Coolable stator assembly for a gas turbine engine |
GB2136508B (en) * | 1983-03-11 | 1987-12-31 | United Technologies Corp | Coolable stator assembly for a gas turbine engine |
-
1984
- 1984-12-21 US US06/684,821 patent/US4720236A/en not_active Expired - Lifetime
-
1985
- 1985-11-04 GB GB08527065A patent/GB2169038B/en not_active Expired
- 1985-11-25 DE DE3541606A patent/DE3541606C2/de not_active Expired - Lifetime
- 1985-11-29 FR FR858517735A patent/FR2575221B1/fr not_active Expired - Lifetime
- 1985-12-20 JP JP60287598A patent/JP2617707B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US4720236A (en) | 1988-01-19 |
DE3541606A1 (de) | 1986-06-26 |
GB2169038B (en) | 1988-07-20 |
FR2575221A1 (fr) | 1986-06-27 |
DE3541606C2 (de) | 1996-04-11 |
GB8527065D0 (en) | 1985-12-11 |
JPS61157703A (ja) | 1986-07-17 |
JP2617707B2 (ja) | 1997-06-04 |
GB2169038A (en) | 1986-07-02 |
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