EP0103260A3 - Régulation du jeu des extrémités des aubes de turbine - Google Patents
Régulation du jeu des extrémités des aubes de turbine Download PDFInfo
- Publication number
- EP0103260A3 EP0103260A3 EP83108779A EP83108779A EP0103260A3 EP 0103260 A3 EP0103260 A3 EP 0103260A3 EP 83108779 A EP83108779 A EP 83108779A EP 83108779 A EP83108779 A EP 83108779A EP 0103260 A3 EP0103260 A3 EP 0103260A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- blade tips
- guide vane
- turbine
- turbine blade
- clearance control
- 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.)
- Withdrawn
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
-
- 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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP15392382A JPS5943905A (ja) | 1982-09-06 | 1982-09-06 | 軸流タ−ビンの動翼先端すきま調整装置 |
JP153923/82 | 1982-09-06 | ||
JP19898682A JPS5990706A (ja) | 1982-11-15 | 1982-11-15 | 軸流タ−ビンの動翼先端すきま調整装置 |
JP198986/82 | 1982-11-15 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0103260A2 EP0103260A2 (fr) | 1984-03-21 |
EP0103260A3 true EP0103260A3 (fr) | 1984-09-26 |
Family
ID=26482405
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP83108779A Withdrawn EP0103260A3 (fr) | 1982-09-06 | 1983-09-06 | Régulation du jeu des extrémités des aubes de turbine |
Country Status (1)
Country | Link |
---|---|
EP (1) | EP0103260A3 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2206651B (en) * | 1987-07-01 | 1991-05-08 | Rolls Royce Plc | Turbine blade shroud structure |
DE19618314A1 (de) * | 1996-05-08 | 1997-11-13 | Asea Brown Boveri | Abgasturbine eines Abgasturboladers |
DE50112597D1 (de) * | 2001-04-12 | 2007-07-19 | Siemens Ag | Gasturbine mit axial verschiebbaren Gehäuseteilen |
GB0119608D0 (en) | 2001-08-11 | 2001-10-03 | Rolls Royce Plc | A guide vane assembly |
EP1995413B1 (fr) * | 2007-04-05 | 2010-04-28 | ALSTOM Technology Ltd | Joint d'étanchéité pour le jeu d'aubes d'une turbomachine |
US8459035B2 (en) | 2007-07-27 | 2013-06-11 | United Technologies Corporation | Gas turbine engine with low fan pressure ratio |
US8347633B2 (en) | 2007-07-27 | 2013-01-08 | United Technologies Corporation | Gas turbine engine with variable geometry fan exit guide vane system |
WO2010085494A1 (fr) | 2009-01-20 | 2010-07-29 | Williams International Co., L.L.C. | Turbocompresseur avec cartouche de tuyère de turbine |
EP2305753B1 (fr) | 2009-09-25 | 2012-02-29 | Evonik RohMax Additives GmbH | Composition pour améliorer les propriétés d'écoulement à froid d'huiles combustibles |
CN103370400B (zh) | 2011-03-25 | 2016-12-14 | 赢创油品添加剂有限公司 | 用于改进燃料油氧化稳定性的组合物 |
CN114607474A (zh) * | 2022-03-21 | 2022-06-10 | 中国联合重型燃气轮机技术有限公司 | 静叶间隙控制系统和具有其的燃气轮机 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2849209A (en) * | 1950-10-11 | 1958-08-26 | Gen Electric | Nozzle construction for turbines |
US3532437A (en) * | 1967-11-03 | 1970-10-06 | Sulzer Ag | Stator blade assembly for axial-flow turbines |
GB1534660A (en) * | 1976-05-05 | 1978-12-06 | Stal Laval Turbin Ab | Sealing arrangement in a gas turbine |
GB2034415A (en) * | 1978-11-13 | 1980-06-04 | Gen Motors Corp | Turbine stator mounting |
GB2061396A (en) * | 1979-10-24 | 1981-05-13 | Rolls Royce | Turbine blade tip clearance control |
-
1983
- 1983-09-06 EP EP83108779A patent/EP0103260A3/fr not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2849209A (en) * | 1950-10-11 | 1958-08-26 | Gen Electric | Nozzle construction for turbines |
US3532437A (en) * | 1967-11-03 | 1970-10-06 | Sulzer Ag | Stator blade assembly for axial-flow turbines |
GB1534660A (en) * | 1976-05-05 | 1978-12-06 | Stal Laval Turbin Ab | Sealing arrangement in a gas turbine |
GB2034415A (en) * | 1978-11-13 | 1980-06-04 | Gen Motors Corp | Turbine stator mounting |
GB2061396A (en) * | 1979-10-24 | 1981-05-13 | Rolls Royce | Turbine blade tip clearance control |
Also Published As
Publication number | Publication date |
---|---|
EP0103260A2 (fr) | 1984-03-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2060077B (en) | Arrangement for controlling the clearance between turbine rotor blades and a stator shroud ring | |
EP0353498A3 (fr) | Construction de diaphragme de compresseur | |
SE7705736L (sv) | Rotor med skovlar av keramiskt material for gasturbiner | |
GB2042646B (en) | Rotor blade tip clearance control for gas turbine engine | |
GB1148590A (en) | Improvements in stator vane assembly having composite sectors | |
EP0103260A3 (fr) | Régulation du jeu des extrémités des aubes de turbine | |
CA1027484A (fr) | Groupe rotor, allette et plateau d'etancheite pour turbine a gaz a allettes de rotor refroidies | |
GB1473719A (en) | Turbomachines | |
IT8020482A0 (it) | Rotore palettato per motore a turbina a gas. | |
RU2287063C1 (ru) | Лабиринтное уплотнение для паровой турбины | |
GB1187171A (en) | Improvements in Fluid Impingement Starting Means for Gas Turbine Engines. | |
GB1020900A (en) | A seal between the rotor blades and the casing of axial-flow turbo-machines | |
GB1506360A (en) | Ceramic turbine structures | |
GB1491556A (en) | Rotor blades for turbomachines | |
AU582935B2 (en) | Improved shroud means for turbine rotor blade tip clearance | |
FR2324873A1 (fr) | Perfectionnements aux flasques de rotors de turbomachines | |
ES8104670A1 (es) | Mejoras en paletas guiadoras para maquinas dinamo-electricasrefrigeradas por flujo inverso | |
GB902064A (en) | Blade damping means for compressors and turbines | |
SE7610577L (sv) | For en gasturbin avsedd stator | |
GB751740A (en) | Improvements in and relating to the fixing of rotor blades of axial flow turbines and compressors | |
GB789733A (en) | Improvements in or relating to structural elements for axial-flow compressors or turbines or the like machines | |
IT7925758A0 (it) | Paletta rotorica e direttrice ricurva per motore a turbina a gas e relativo metodo di fabbricazione. | |
GB2048394B (en) | Blade mounting arrangement for a ring of blades on a turbomachine rotor | |
GB851323A (en) | Axial-flow compressors and turbines | |
GB1378346A (en) | Variable stator vane cascade for turbomachines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19830906 |
|
AK | Designated contracting states |
Designated state(s): CH DE FR GB IT LI |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Designated state(s): CH DE FR GB IT LI |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN |
|
18W | Application withdrawn |
Withdrawal date: 19851203 |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: NODA, MASAMI Inventor name: KATO, YASUHIRO, MR. Inventor name: IKEGUCHI, TAKASHI Inventor name: KAWAIKE, KAZUHIKO Inventor name: WADA, KATSUO |