GB9518424D0 - Turbines - Google Patents
TurbinesInfo
- Publication number
- GB9518424D0 GB9518424D0 GBGB9518424.8A GB9518424A GB9518424D0 GB 9518424 D0 GB9518424 D0 GB 9518424D0 GB 9518424 A GB9518424 A GB 9518424A GB 9518424 D0 GB9518424 D0 GB 9518424D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbines
- 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- Withdrawn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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/02—Arrangement of sensing elements
- F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0246—Surge control by varying geometry within the pumps, e.g. by adjusting vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9420412A GB9420412D0 (en) | 1994-10-11 | 1994-10-11 | Turbines |
GB9421047A GB9421047D0 (en) | 1994-10-11 | 1994-10-19 | Turbines |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9518424D0 true GB9518424D0 (en) | 1995-11-08 |
GB2294094A GB2294094A (en) | 1996-04-17 |
Family
ID=26305771
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9421047A Pending GB9421047D0 (en) | 1994-10-11 | 1994-10-19 | Turbines |
GB9518424A Withdrawn GB2294094A (en) | 1994-10-11 | 1995-09-08 | Gas turbine vane control |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9421047A Pending GB9421047D0 (en) | 1994-10-11 | 1994-10-19 | Turbines |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB9421047D0 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113661306A (en) * | 2019-04-05 | 2021-11-16 | 诺沃皮尼奥内技术股份有限公司 | Steam turbine with rotatable stator blades |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2410530A (en) * | 2004-01-27 | 2005-08-03 | Rolls Royce Plc | Electrically actuated stator vane arrangement |
US7665959B2 (en) * | 2005-07-20 | 2010-02-23 | United Technologies Corporation | Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud |
US7588415B2 (en) | 2005-07-20 | 2009-09-15 | United Technologies Corporation | Synch ring variable vane synchronizing mechanism for inner diameter vane shroud |
US7753647B2 (en) | 2005-07-20 | 2010-07-13 | United Technologies Corporation | Lightweight cast inner diameter vane shroud for variable stator vanes |
EP1860282A1 (en) * | 2006-05-24 | 2007-11-28 | Siemens Aktiengesellschaft | Compressor airfoil with integrated sensing elements and associated compressor |
EP1867877A1 (en) | 2006-06-16 | 2007-12-19 | Ansaldo Energia S.P.A. | Gas turbine compressor |
US9194301B2 (en) * | 2012-06-04 | 2015-11-24 | United Technologies Corporation | Protecting the operating margin of a gas turbine engine having variable vanes from aerodynamic distortion |
DE102012216656B3 (en) * | 2012-09-18 | 2013-08-08 | Siemens Aktiengesellschaft | Adjustable diffuser |
US20170218854A1 (en) * | 2016-02-02 | 2017-08-03 | General Electric Company | Controlling a Gas Turbine Engine to Account for Airflow Distortion |
US10794281B2 (en) | 2016-02-02 | 2020-10-06 | General Electric Company | Gas turbine engine having instrumented airflow path components |
US10753278B2 (en) | 2016-03-30 | 2020-08-25 | General Electric Company | Translating inlet for adjusting airflow distortion in gas turbine engine |
US11073090B2 (en) | 2016-03-30 | 2021-07-27 | General Electric Company | Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine |
US10288079B2 (en) | 2016-06-27 | 2019-05-14 | Rolls-Royce North America Technologies, Inc. | Singular stator vane control |
BE1024492B1 (en) * | 2016-08-12 | 2018-03-12 | Safran Aero Boosters S.A. | ARAB A VARIABLE ORIENTATION OF AXIAL TURBOMACHINE COMPRESSOR |
US20230358144A1 (en) * | 2022-05-06 | 2023-11-09 | General Electric Company Polska Sp. Z O.O. | Actuation assembly for a fan of a gas turbine engine |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4245162A (en) * | 1973-08-15 | 1981-01-13 | Westinghouse Electric Corp. | Steam turbine power plant having improved testing method and system for turbine inlet valves associated with downstream inlet valves preferably having feedforward position managed control |
US3974645A (en) * | 1974-08-08 | 1976-08-17 | Westinghouse Electric Corporation | Control apparatus for matching the exhaust flow of a gas turbine employed in a combined cycle electric power generating plant to the requirements of a steam generator also employed therein |
US4159625A (en) * | 1977-02-01 | 1979-07-03 | United Technologies Corporation | Control for gas turbine engine |
US4380893A (en) * | 1981-02-19 | 1983-04-26 | The Garrett Corporation | Compressor bleed air control apparatus and method |
GB2119862A (en) * | 1982-05-06 | 1983-11-23 | Gen Electric | Variable stator vane (VSV) closed loop control system of a compressor |
GB8610297D0 (en) * | 1986-04-28 | 1986-10-01 | Rolls Royce | Turbomachinery |
US4809500A (en) * | 1987-02-03 | 1989-03-07 | United Technologies Corporation | Transient control system for gas turbine engine |
US4959955A (en) * | 1989-02-27 | 1990-10-02 | United Technologies Corporation | Method of operating gas turbine engine with fan damage |
US5165845A (en) * | 1991-11-08 | 1992-11-24 | United Technologies Corporation | Controlling stall margin in a gas turbine engine during acceleration |
US5327742A (en) * | 1993-05-07 | 1994-07-12 | Carrier Corporation | Hierarchial control for discrete chiller units |
-
1994
- 1994-10-19 GB GB9421047A patent/GB9421047D0/en active Pending
-
1995
- 1995-09-08 GB GB9518424A patent/GB2294094A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113661306A (en) * | 2019-04-05 | 2021-11-16 | 诺沃皮尼奥内技术股份有限公司 | Steam turbine with rotatable stator blades |
CN113661306B (en) * | 2019-04-05 | 2024-04-30 | 诺沃皮尼奥内技术股份有限公司 | Steam turbine with rotatable stator blades |
Also Published As
Publication number | Publication date |
---|---|
GB9421047D0 (en) | 1994-12-07 |
GB2294094A (en) | 1996-04-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |