DE602007002684D1 - Aufhängevorrichtung eines Turbinenleitkranzes - Google Patents
Aufhängevorrichtung eines TurbinenleitkranzesInfo
- Publication number
- DE602007002684D1 DE602007002684D1 DE602007002684T DE602007002684T DE602007002684D1 DE 602007002684 D1 DE602007002684 D1 DE 602007002684D1 DE 602007002684 T DE602007002684 T DE 602007002684T DE 602007002684 T DE602007002684 T DE 602007002684T DE 602007002684 D1 DE602007002684 D1 DE 602007002684D1
- Authority
- DE
- Germany
- Prior art keywords
- guide ring
- suspension device
- turbine guide
- turbine
- suspension
- 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.)
- Active
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/33—Retaining components in desired mutual position with a bayonet coupling
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Connection Of Plates (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0654747A FR2908153B1 (fr) | 2006-11-07 | 2006-11-07 | Dispositif d'accrochage d'un distributeur (8) d'une turbine, turbine les comportant, et moteur d'aeronef en etant equipe |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602007002684D1 true DE602007002684D1 (de) | 2009-11-19 |
Family
ID=38121758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602007002684T Active DE602007002684D1 (de) | 2006-11-07 | 2007-11-05 | Aufhängevorrichtung eines Turbinenleitkranzes |
Country Status (7)
Country | Link |
---|---|
US (1) | US8182202B2 (de) |
EP (1) | EP1921273B1 (de) |
JP (1) | JP5209939B2 (de) |
CA (1) | CA2608402C (de) |
DE (1) | DE602007002684D1 (de) |
FR (1) | FR2908153B1 (de) |
RU (1) | RU2436965C2 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
PL2350521T3 (pl) | 2008-09-18 | 2015-11-30 | Golight Pty Ltd | Przenośny zespół oświetleniowy |
DE102010007724A1 (de) * | 2010-02-12 | 2011-08-18 | Rolls-Royce Deutschland Ltd & Co KG, 15827 | Schraubenlose Zwischenstufendichtung einer Gasturbine |
FR2960907B1 (fr) | 2010-06-02 | 2012-07-27 | Snecma | Palier de roulement pour turboreacteur d'aeronef equipe de moyens ameliores de retention axiale de sa bague exterieure |
FR2981980B1 (fr) * | 2011-10-26 | 2016-01-22 | Snecma | Procede de montage d'un aubage fixe d'une turbomachine, carter et turbomachine comportant au moins un aubage fixe monte sur ce carter |
US9353767B2 (en) | 2013-01-08 | 2016-05-31 | United Technologies Corporation | Stator anti-rotation device |
FR3009740B1 (fr) | 2013-08-13 | 2017-12-15 | Snecma | Amelioration pour le verrouillage de pieces de support d'aubage |
FR3051014B1 (fr) * | 2016-05-09 | 2018-05-18 | Safran Aircraft Engines | Ensemble pour turbomachine comprenant un distributeur, un element de structure de turbomachine, et un dispositif de fixation |
FR3053384B1 (fr) | 2016-06-30 | 2018-07-27 | Safran Aircraft Engines | Ensemble de fixation d'un distributeur a un element de structure d'une turbomachine |
KR102373037B1 (ko) * | 2016-08-24 | 2022-03-11 | 도레이 카부시키가이샤 | 흑색 안료와 그의 제조 방법, 안료 분산액, 감광성 조성물 및 그의 경화물 |
FR3066226B1 (fr) * | 2017-05-10 | 2020-07-17 | Safran Aircraft Engines | Verrouillage anneau stator sous distributeur haute pression |
US11674400B2 (en) * | 2021-03-12 | 2023-06-13 | Ge Avio S.R.L. | Gas turbine engine nozzles |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3860359A (en) * | 1973-07-30 | 1975-01-14 | Curtiss Wright Corp | Mounting system for gas turbine power unit |
US3989410A (en) * | 1974-11-27 | 1976-11-02 | General Electric Company | Labyrinth seal system |
US4669959A (en) * | 1984-07-23 | 1987-06-02 | United Technologies Corporation | Breach lock anti-rotation key |
FR2663997B1 (fr) * | 1990-06-27 | 1993-12-24 | Snecma | Dispositif de fixation d'une couronne de revolution sur un disque de turbomachine. |
US5224822A (en) * | 1991-05-13 | 1993-07-06 | General Electric Company | Integral turbine nozzle support and discourager seal |
US5211536A (en) * | 1991-05-13 | 1993-05-18 | General Electric Company | Boltless turbine nozzle/stationary seal mounting |
US5271714A (en) * | 1992-07-09 | 1993-12-21 | General Electric Company | Turbine nozzle support arrangement |
US5800124A (en) * | 1996-04-12 | 1998-09-01 | United Technologies Corporation | Cooled rotor assembly for a turbine engine |
US6095750A (en) * | 1998-12-21 | 2000-08-01 | General Electric Company | Turbine nozzle assembly |
JP4432137B2 (ja) * | 1999-01-13 | 2010-03-17 | 株式会社Ihi | ジェットエンジン用ガスタービンのタービンノズル支持装置 |
US6761034B2 (en) * | 2000-12-08 | 2004-07-13 | General Electroc Company | Structural cover for gas turbine engine bolted flanges |
US6428272B1 (en) * | 2000-12-22 | 2002-08-06 | General Electric Company | Bolted joint for rotor disks and method of reducing thermal gradients therein |
US6530744B2 (en) * | 2001-05-29 | 2003-03-11 | General Electric Company | Integral nozzle and shroud |
US6742987B2 (en) * | 2002-07-16 | 2004-06-01 | General Electric Company | Cradle mounted turbine nozzle |
JP4072683B2 (ja) * | 2003-08-19 | 2008-04-09 | 豊和工業株式会社 | 旋回式クランプシリンダ |
FR2867223B1 (fr) * | 2004-03-03 | 2006-07-28 | Snecma Moteurs | Turbomachine comme par exemple un turboreacteur pour avion |
-
2006
- 2006-11-07 FR FR0654747A patent/FR2908153B1/fr active Active
-
2007
- 2007-10-30 CA CA2608402A patent/CA2608402C/fr active Active
- 2007-11-05 EP EP07119994A patent/EP1921273B1/de active Active
- 2007-11-05 DE DE602007002684T patent/DE602007002684D1/de active Active
- 2007-11-06 JP JP2007288137A patent/JP5209939B2/ja active Active
- 2007-11-06 RU RU2007141150/06A patent/RU2436965C2/ru active
- 2007-11-06 US US11/935,570 patent/US8182202B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20080107530A1 (en) | 2008-05-08 |
RU2007141150A (ru) | 2009-05-20 |
CA2608402A1 (fr) | 2008-05-07 |
CA2608402C (fr) | 2014-10-21 |
RU2436965C2 (ru) | 2011-12-20 |
EP1921273B1 (de) | 2009-10-07 |
JP2008138670A (ja) | 2008-06-19 |
JP5209939B2 (ja) | 2013-06-12 |
EP1921273A1 (de) | 2008-05-14 |
US8182202B2 (en) | 2012-05-22 |
FR2908153B1 (fr) | 2011-05-13 |
FR2908153A1 (fr) | 2008-05-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE602007002684D1 (de) | Aufhängevorrichtung eines Turbinenleitkranzes | |
DE602008002794D1 (de) | Kolbenring eines Kolbenmotors | |
DE602007000064D1 (de) | Ringförmige Brennkammer eines Turbotriebwerks | |
DE602007009436D1 (de) | Ringförmige Brennkammer eines Turbotriebwerks | |
FR2896537B1 (fr) | Turbomachine a generateur-demarreur integre | |
BRPI0908578A2 (pt) | Ensaios de atividades de sorotipo a de toxina botulínica imunobaseada | |
DE602008000388D1 (de) | Gebläse eines Turbotriebwerks | |
DE602007007334D1 (de) | Gasturbinenanordnung | |
DE602007006263D1 (de) | Turbomaschine | |
DE602008005524D1 (de) | Laufradeinheit eines Turbotriebwerks | |
DE602007000192D1 (de) | Gelenkstruktur eines roboters | |
FR2907841B1 (fr) | Secteur d'anneau de turbine de turbomachine | |
FR2952563B1 (fr) | Dispositif d'usinage axial | |
NO20063088L (no) | Vannturbin | |
DE602008000360D1 (de) | Leitschaufel eines Gebläses | |
FR2953109B1 (fr) | Dispositif d'application d'un fluide | |
DE112004002906A5 (de) | Haltevorrichtung für Solarelemente eines Solarfeldes | |
DK1878917T3 (da) | Vindenergianlæg | |
FR2956332B1 (fr) | Dispositif d'application d'un fluide | |
FR2955891B1 (fr) | Secteur d'anneau de turbine de turbomachine | |
DE602007002248D1 (de) | Begrenzungsvorrichtung gegen Überdrehzahl für die Turbine einer Turbomaschine und entsprechende Turbomaschine | |
DE602008004290D1 (de) | Rad eines Turbotriebwerks | |
DE602007013674D1 (de) | Autoklavierbarer Kolbenführungsring | |
DE602007011783D1 (de) | G eines leistungsverstärkers | |
FR2951137B1 (fr) | Dispositif anticouple d'un giravion |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |