IT1100530B - Metodo e apparato per rapidi aumenti di spinta in un motore a turboventilatore - Google Patents
Metodo e apparato per rapidi aumenti di spinta in un motore a turboventilatoreInfo
- Publication number
- IT1100530B IT1100530B IT30454/78A IT3045478A IT1100530B IT 1100530 B IT1100530 B IT 1100530B IT 30454/78 A IT30454/78 A IT 30454/78A IT 3045478 A IT3045478 A IT 3045478A IT 1100530 B IT1100530 B IT 1100530B
- Authority
- IT
- Italy
- Prior art keywords
- turbo
- fan engine
- quick increases
- quick
- increases
- Prior art date
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
- F02C9/48—Control of fuel supply conjointly with another control of the plant
- F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
- F02C9/54—Control of fuel supply conjointly with another control of the plant with control of working fluid flow by throttling the working fluid, by adjusting vanes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/858,936 US4184327A (en) | 1977-12-09 | 1977-12-09 | Method and apparatus for rapid thrust increases in a turbofan engine |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7830454A0 IT7830454A0 (it) | 1978-12-01 |
IT1100530B true IT1100530B (it) | 1985-09-28 |
Family
ID=25329549
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT30454/78A IT1100530B (it) | 1977-12-09 | 1978-12-01 | Metodo e apparato per rapidi aumenti di spinta in un motore a turboventilatore |
Country Status (6)
Country | Link |
---|---|
US (1) | US4184327A (it) |
JP (1) | JPS5495819A (it) |
DE (1) | DE2852911A1 (it) |
FR (1) | FR2411308A1 (it) |
GB (1) | GB2009858B (it) |
IT (1) | IT1100530B (it) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4928482A (en) * | 1988-09-20 | 1990-05-29 | United Technologies Corporation | Control of high compressor vanes and fuel for a gas turbine engine |
US4947643A (en) * | 1988-09-20 | 1990-08-14 | United Technologies Corporation | Active geometry control system for gas turbine engines |
US5133182A (en) * | 1988-09-20 | 1992-07-28 | United Technologies Corporation | Control of low compressor vanes and fuel for a gas turbine engine |
US6735955B2 (en) * | 2001-10-10 | 2004-05-18 | Goodrich Pump & Engine Control Systems, Inc. | Control system for positioning compressor inlet guide vanes |
US6688097B2 (en) | 2001-12-19 | 2004-02-10 | Honeywell International Inc. | Multivariant set point using N1 and N2 for engine control |
DE102007012119A1 (de) * | 2007-03-13 | 2008-09-18 | Rolls-Royce Deutschland Ltd & Co Kg | Drosselgradabhängige Schaufelverstellung bei Strömungsarbeitsmaschinen |
US8954228B2 (en) * | 2008-12-30 | 2015-02-10 | Rolls-Royce Corporation | Gas turbine engine failure detection |
US20100162720A1 (en) * | 2008-12-31 | 2010-07-01 | Bowman Ray F | Gas turbine engine |
FR2950927B1 (fr) * | 2009-10-06 | 2016-01-29 | Snecma | Systeme de commande de la position angulaire d'aubes de stator et procede d'optimisation de ladite position angulaire |
US9512784B2 (en) * | 2010-01-29 | 2016-12-06 | Pratt & Whitney Canada Corp. | Free gas turbine with constant temperature-corrected gas generator speed |
GB201112577D0 (en) * | 2011-07-22 | 2011-08-31 | Rolls Royce Plc | Method of inhibiting ice accretion within a turbine engine and control system therefor |
US8742973B1 (en) * | 2011-09-22 | 2014-06-03 | Rockwell Collins, Inc. | System and method of determining increased turbulence susceptibility with elapsed flight time |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1102493B (de) * | 1957-12-30 | 1961-03-16 | Rolls Royce | Zweikreisgasturbinenstrahltriebwerk |
US3657881A (en) * | 1969-09-02 | 1972-04-25 | Gen Motors Corp | Gas turbine control with prewhirl of air entering the compressor |
US3686859A (en) * | 1970-09-25 | 1972-08-29 | Chandler Evans Inc | Turbine engine starting circuit |
US3797233A (en) * | 1973-06-28 | 1974-03-19 | United Aircraft Corp | Integrated control for a turbopropulsion system |
US3952502A (en) * | 1974-03-04 | 1976-04-27 | General Motors Corporation | Gas turbine control |
-
1977
- 1977-12-09 US US05/858,936 patent/US4184327A/en not_active Expired - Lifetime
-
1978
- 1978-12-01 IT IT30454/78A patent/IT1100530B/it active
- 1978-12-04 GB GB7847101A patent/GB2009858B/en not_active Expired
- 1978-12-07 DE DE19782852911 patent/DE2852911A1/de active Granted
- 1978-12-07 JP JP15059178A patent/JPS5495819A/ja active Granted
- 1978-12-08 FR FR7834644A patent/FR2411308A1/fr active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS6130142B2 (it) | 1986-07-11 |
DE2852911C2 (it) | 1991-03-28 |
FR2411308B1 (it) | 1983-10-28 |
IT7830454A0 (it) | 1978-12-01 |
US4184327A (en) | 1980-01-22 |
GB2009858B (en) | 1982-02-24 |
GB2009858A (en) | 1979-06-20 |
JPS5495819A (en) | 1979-07-28 |
FR2411308A1 (fr) | 1979-07-06 |
DE2852911A1 (de) | 1979-06-13 |
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Legal Events
Date | Code | Title | Description |
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TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19921216 |