FR840427A - Gas turbine tuning process - Google Patents
Gas turbine tuning processInfo
- Publication number
- FR840427A FR840427A FR840427DA FR840427A FR 840427 A FR840427 A FR 840427A FR 840427D A FR840427D A FR 840427DA FR 840427 A FR840427 A FR 840427A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- tuning process
- turbine tuning
- gas
- turbine
- 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
- 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
- F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HU2305311X | 1937-07-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR840427A true FR840427A (en) | 1939-04-25 |
Family
ID=11003769
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR840427D Expired FR840427A (en) | 1937-07-07 | 1938-07-07 | Gas turbine tuning process |
Country Status (2)
Country | Link |
---|---|
US (1) | US2305311A (en) |
FR (1) | FR840427A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2390584A1 (en) * | 1977-05-11 | 1978-12-08 | Texaco Development Corp | COMBINED CYCLE ELECTRIC ENERGY PRODUCTION DEVICE |
EP0203353A1 (en) * | 1985-04-20 | 1986-12-03 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Cooled gas turbine with a load-dependent, controllable quantity of cooling air |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2473356A (en) * | 1942-04-18 | 1949-06-14 | Turbo Engineering Corp | Combustion gas turbine arrangement |
US2428830A (en) * | 1942-04-18 | 1947-10-14 | Turbo Engineering Corp | Regulation of combustion gas turbines arranged in series |
US2641324A (en) * | 1943-02-19 | 1953-06-09 | Bristol Aeroplane Co Ltd | Regulating means for gas turbine installations |
US2581275A (en) * | 1944-10-09 | 1952-01-01 | Bendix Aviat Corp | Fuel feed responsive to air pressure and temperature, fuel flow, and speed for gas turbines |
US2532469A (en) * | 1945-08-13 | 1950-12-05 | Bendix Aviat Corp | Airplane control system |
US2527732A (en) * | 1946-02-07 | 1950-10-31 | Rateau Soc | Braking device for aircraft jet turbopropellers |
US2631428A (en) * | 1946-08-28 | 1953-03-17 | Arthur H Nelson | Multiple fluid-operated rotary gear motors with treatment between stages |
US2697326A (en) * | 1951-04-30 | 1954-12-21 | Ca Nat Research Council | Reactor with adjustable stator blades |
US2936578A (en) * | 1954-05-06 | 1960-05-17 | United Aircraft Corp | Variable orifice type jet nozzle |
US2933234A (en) * | 1954-12-28 | 1960-04-19 | Gen Electric | Compressor stator assembly |
US2980394A (en) * | 1956-11-23 | 1961-04-18 | Garrett Corp | Temperature responsive variable means for controlling flow in turbomachines |
US3079127A (en) * | 1956-11-23 | 1963-02-26 | Garrett Corp | Temperature responsive variable means for controlling flow in turbomachines |
US3053086A (en) * | 1957-02-12 | 1962-09-11 | Granberg Corp | Turbine type meter |
US2936108A (en) * | 1957-04-29 | 1960-05-10 | Gen Electric | Compressor |
US3146626A (en) * | 1959-09-19 | 1964-09-01 | Voith Gmbh J M | Adjusting mechanism for blades of fluid flow machines, especially torque converters |
US3356288A (en) * | 1965-04-07 | 1967-12-05 | Gen Electric | Stator adjusting means for axial flow compressors or the like |
DE2005536B2 (en) * | 1969-02-20 | 1972-05-04 | Czkd Praha, Oborovy Podnik, Prag | CONTROL DEVICE FOR THE VANES OF A MULTISTAGE AXIAL COMPRESSOR |
US3954349A (en) * | 1975-06-02 | 1976-05-04 | United Technologies Corporation | Lever connection to syncring |
DE3913102C1 (en) * | 1989-04-21 | 1990-05-31 | Mtu Muenchen Gmbh | |
US5993152A (en) * | 1997-10-14 | 1999-11-30 | General Electric Company | Nonlinear vane actuation |
JP4115037B2 (en) * | 1999-04-02 | 2008-07-09 | 三菱重工業株式会社 | Gas turbine startup method |
FR2853930B1 (en) * | 2003-04-16 | 2007-02-23 | Snecma Moteurs | DEVICE FOR THE CONTROL OF VARIABLE-SETTING AUBES IN A TURBOMACHINE |
-
1938
- 1938-07-05 US US217506A patent/US2305311A/en not_active Expired - Lifetime
- 1938-07-07 FR FR840427D patent/FR840427A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2390584A1 (en) * | 1977-05-11 | 1978-12-08 | Texaco Development Corp | COMBINED CYCLE ELECTRIC ENERGY PRODUCTION DEVICE |
EP0203353A1 (en) * | 1985-04-20 | 1986-12-03 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Cooled gas turbine with a load-dependent, controllable quantity of cooling air |
Also Published As
Publication number | Publication date |
---|---|
US2305311A (en) | 1942-12-15 |
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