GB1533940A - Variable geometry turbine or compressor nozzle - Google Patents
Variable geometry turbine or compressor nozzleInfo
- Publication number
- GB1533940A GB1533940A GB36149/77A GB3614977A GB1533940A GB 1533940 A GB1533940 A GB 1533940A GB 36149/77 A GB36149/77 A GB 36149/77A GB 3614977 A GB3614977 A GB 3614977A GB 1533940 A GB1533940 A GB 1533940A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- variable geometry
- geometry turbine
- adjustable
- ring gear
- 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
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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/24—Three-dimensional ellipsoidal
- F05D2250/241—Three-dimensional ellipsoidal spherical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/730,044 US4150915A (en) | 1976-12-23 | 1976-12-23 | Variable geometry turbine nozzle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1533940A true GB1533940A (en) | 1978-11-29 |
Family
ID=24933674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB36149/77A Expired GB1533940A (en) | 1976-12-23 | 1977-08-30 | Variable geometry turbine or compressor nozzle |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4150915A (enExample) |
| JP (1) | JPS5379109A (enExample) |
| CA (1) | CA1062163A (enExample) |
| GB (1) | GB1533940A (enExample) |
| SE (2) | SE434665B (enExample) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0253234A1 (de) * | 1986-07-09 | 1988-01-20 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Vorstellvorrichtung für Leitschaufeln von Turbotriebwerken |
| US4826399A (en) * | 1988-05-06 | 1989-05-02 | General Motors Corporation | Unison ring mounting arrangement |
| GB2301867A (en) * | 1995-06-05 | 1996-12-18 | Rolls Royce Plc | Supporting unison rings in pivotable vane actuating mechanisms |
| EP1705341A2 (en) | 2005-03-05 | 2006-09-27 | Rolls-Royce plc | Pivot ring |
| EP1757775A3 (de) * | 2005-08-26 | 2008-07-23 | Rolls-Royce Deutschland Ltd & Co KG | Dichtvorrichtung für eine verstellbare Statorschaufel |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4318668A (en) * | 1979-11-01 | 1982-03-09 | United Technologies Corporation | Seal means for a gas turbine engine |
| US4659295A (en) * | 1984-04-20 | 1987-04-21 | The Garrett Corporation | Gas seal vanes of variable nozzle turbine |
| US4679984A (en) * | 1985-12-11 | 1987-07-14 | The Garrett Corporation | Actuation system for variable nozzle turbine |
| US4763114A (en) * | 1987-07-09 | 1988-08-09 | Eidsmore Paul G | Fluid flow indicator |
| SE508860C2 (sv) * | 1997-03-18 | 1998-11-09 | Abb Stal Ab | Anordning vid en i en rotormaskin anordnad ledskena samt en vridbar turbinskena |
| JP2001329851A (ja) * | 2000-05-19 | 2001-11-30 | Mitsubishi Heavy Ind Ltd | 可変容量タービンの可変ノズル機構 |
| US8382436B2 (en) * | 2009-01-06 | 2013-02-26 | General Electric Company | Non-integral turbine blade platforms and systems |
| US8262345B2 (en) * | 2009-02-06 | 2012-09-11 | General Electric Company | Ceramic matrix composite turbine engine |
| US8360716B2 (en) * | 2010-03-23 | 2013-01-29 | United Technologies Corporation | Nozzle segment with reduced weight flange |
| US8668445B2 (en) | 2010-10-15 | 2014-03-11 | General Electric Company | Variable turbine nozzle system |
| US9309778B2 (en) | 2010-12-30 | 2016-04-12 | Rolls-Royce North American Technologies, Inc. | Variable vane for gas turbine engine |
| US20140119894A1 (en) * | 2012-10-25 | 2014-05-01 | Solar Turbines Incorporated | Variable area turbine nozzle |
| WO2014189547A1 (en) * | 2013-05-20 | 2014-11-27 | Volvo Truck Corporation | Variable geometry turbine with shroud support |
| EP3071796B1 (en) * | 2013-11-18 | 2021-12-01 | Raytheon Technologies Corporation | Gas turbine engine variable area vane with contoured endwalls |
| US10626739B2 (en) * | 2015-10-27 | 2020-04-21 | Mitsubishi Heavy Industries, Ltd. | Rotary machine |
| US10208619B2 (en) | 2015-11-02 | 2019-02-19 | Florida Turbine Technologies, Inc. | Variable low turbine vane with aft rotation axis |
| DE102018213983A1 (de) | 2018-08-20 | 2020-02-20 | MTU Aero Engines AG | Verstellbare Leitschaufelanordnung, Leitschaufel, Dichtungsträger und Turbomaschine |
| US12180974B2 (en) * | 2022-03-24 | 2024-12-31 | Copeland Lp | Variable inlet guide vane apparatus and compressor including same |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL75411C (enExample) * | 1946-03-20 | |||
| US3224194A (en) * | 1963-06-26 | 1965-12-21 | Curtiss Wright Corp | Gas turbine engine |
| FR2055780A1 (enExample) * | 1969-08-14 | 1971-04-30 | Bennes Marrel | |
| US3904309A (en) * | 1974-08-12 | 1975-09-09 | Caterpillar Tractor Co | Variable angle turbine nozzle actuating mechanism |
| US3995971A (en) * | 1975-06-02 | 1976-12-07 | United Technologies Corporation | Rotatable vane seal |
| US3976394A (en) * | 1975-07-18 | 1976-08-24 | The United States Of America As Represented By The Secretary Of The Air Force | Interstage bleed assembly |
| US4003675A (en) * | 1975-09-02 | 1977-01-18 | Caterpillar Tractor Co. | Actuating mechanism for gas turbine engine nozzles |
| US4030288A (en) * | 1975-11-10 | 1977-06-21 | Caterpillar Tractor Co. | Modular gas turbine engine assembly |
-
1976
- 1976-12-23 US US05/730,044 patent/US4150915A/en not_active Expired - Lifetime
-
1977
- 1977-08-30 GB GB36149/77A patent/GB1533940A/en not_active Expired
- 1977-09-20 JP JP11318377A patent/JPS5379109A/ja active Granted
- 1977-09-27 CA CA287,581A patent/CA1062163A/en not_active Expired
- 1977-11-23 SE SE7713270A patent/SE434665B/sv not_active IP Right Cessation
-
1982
- 1982-07-23 SE SE8204446A patent/SE450782B/sv not_active IP Right Cessation
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0253234A1 (de) * | 1986-07-09 | 1988-01-20 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Vorstellvorrichtung für Leitschaufeln von Turbotriebwerken |
| US4826399A (en) * | 1988-05-06 | 1989-05-02 | General Motors Corporation | Unison ring mounting arrangement |
| GB2301867A (en) * | 1995-06-05 | 1996-12-18 | Rolls Royce Plc | Supporting unison rings in pivotable vane actuating mechanisms |
| EP1705341A2 (en) | 2005-03-05 | 2006-09-27 | Rolls-Royce plc | Pivot ring |
| EP1705341A3 (en) * | 2005-03-05 | 2009-03-25 | Rolls-Royce plc | Pivot ring |
| US7802963B2 (en) | 2005-03-05 | 2010-09-28 | Rolls-Royce Plc | Pivot ring |
| EP1757775A3 (de) * | 2005-08-26 | 2008-07-23 | Rolls-Royce Deutschland Ltd & Co KG | Dichtvorrichtung für eine verstellbare Statorschaufel |
Also Published As
| Publication number | Publication date |
|---|---|
| SE7713270L (sv) | 1978-06-24 |
| CA1062163A (en) | 1979-09-11 |
| SE450782B (sv) | 1987-07-27 |
| SE8204446L (sv) | 1982-07-23 |
| US4150915A (en) | 1979-04-24 |
| JPS5379109A (en) | 1978-07-13 |
| SE434665B (sv) | 1984-08-06 |
| JPS6114323B2 (enExample) | 1986-04-18 |
| SE8204446D0 (sv) | 1982-07-23 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
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| GB1008526A (en) | Axial flow bladed rotor, e.g. for a turbine | |
| ES8401567A1 (es) | Perfeccionamientos en una turbina de vapor con admision axial. | |
| GB1020900A (en) | A seal between the rotor blades and the casing of axial-flow turbo-machines | |
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| GB1095830A (en) | Bladed rotor for a fluid flow machine such as a gas turbine engine | |
| CA2047275A1 (en) | Fully floating inlet flow guide for double-flow low pressure steam turbines | |
| GB1528421A (en) | Shroud for rotor or impeller of a turbine or compressor with abradable seal layer on inside to establish minimized running clearance | |
| ES382608A1 (es) | Turbina de gas con distribuiduidores de paso variable. | |
| CH426885A (de) | Beschaufelter Zwischenboden für Turbinen und Verfahren zu dessen Herstellung | |
| GB1385666A (en) | Sealing of vaned assemblies of gas turbine engines |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| 732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19920830 |