SE8107800L - Temperaturregler-/synkroniseringssystem - Google Patents
Temperaturregler-/synkroniseringssystemInfo
- Publication number
- SE8107800L SE8107800L SE8107800A SE8107800A SE8107800L SE 8107800 L SE8107800 L SE 8107800L SE 8107800 A SE8107800 A SE 8107800A SE 8107800 A SE8107800 A SE 8107800A SE 8107800 L SE8107800 L SE 8107800L
- Authority
- SE
- Sweden
- Prior art keywords
- power lever
- pilot
- closed loop
- temperature
- control system
- 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
- F02C9/26—Control of fuel supply
- F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control; Arrangement thereof
- B64D31/02—Initiating means
- B64D31/06—Initiating means actuated automatically
- B64D31/12—Initiating means actuated automatically for equalising or synchronising power plants
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US24912581A | 1981-03-30 | 1981-03-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
SE8107800L true SE8107800L (sv) | 1982-10-01 |
Family
ID=22942151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8107800A SE8107800L (sv) | 1981-03-30 | 1981-12-28 | Temperaturregler-/synkroniseringssystem |
Country Status (8)
Country | Link |
---|---|
JP (1) | JPS57165632A (sv) |
BR (1) | BR8201832A (sv) |
CA (1) | CA1161527A (sv) |
DE (1) | DE3201010A1 (sv) |
FR (1) | FR2502697A1 (sv) |
GB (1) | GB2095755A (sv) |
IT (1) | IT1151860B (sv) |
SE (1) | SE8107800L (sv) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4934825A (en) * | 1987-12-22 | 1990-06-19 | United Technologies Corporation | Propeller phase control apparatus |
US4875168A (en) * | 1987-12-22 | 1989-10-17 | United Technologies Corporation | Engine speed control apparatus |
US5006993A (en) * | 1988-11-18 | 1991-04-09 | The Boeing Company | Automatic throttle controller for aircraft with intermixed engines |
DE4329346A1 (de) * | 1993-02-08 | 1994-08-11 | Witt & Sohn Gmbh & Co | Oberflächeneffektfahrzeug |
GB0224625D0 (en) | 2002-10-23 | 2002-12-04 | Honeywell Normalair Garrett | Method of balancing the supply of bleed air from a plurality of engines |
EP1825116A2 (en) | 2004-12-01 | 2007-08-29 | United Technologies Corporation | Ejector cooling of outer case for tip turbine engine |
US8641367B2 (en) | 2004-12-01 | 2014-02-04 | United Technologies Corporation | Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method |
EP1825113B1 (en) | 2004-12-01 | 2012-10-24 | United Technologies Corporation | Counter-rotating gearbox for tip turbine engine |
WO2006060004A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Combustor for turbine engine |
WO2006059970A2 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Turbine engine with differential gear driven fan and compressor |
DE602004028297D1 (de) | 2004-12-01 | 2010-09-02 | United Technologies Corp | Umfangsbrennkammer für spitzenturbinenmotor |
WO2006059986A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Tip turbine engine and operating method with reverse core airflow |
WO2006110123A2 (en) | 2004-12-01 | 2006-10-19 | United Technologies Corporation | Vectoring transition duct for turbine engine |
EP1825115A1 (en) * | 2004-12-01 | 2007-08-29 | United Technologies Corporation | Remote engine fuel control and electronic engine control for turbine engine |
US7845157B2 (en) | 2004-12-01 | 2010-12-07 | United Technologies Corporation | Axial compressor for tip turbine engine |
EP1825177B1 (en) | 2004-12-01 | 2012-01-25 | United Technologies Corporation | Inflatable bleed valve for turbine engine and method of controlling bleed air |
EP1831530B1 (en) | 2004-12-01 | 2009-02-25 | United Technologies Corporation | Compressor variable stage remote actuation for turbine engine |
DE602004016065D1 (de) | 2004-12-01 | 2008-10-02 | United Technologies Corp | Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren |
FR2902408B1 (fr) * | 2006-06-19 | 2008-08-08 | Eurocopter France | Equilibrage en puissance de deux turbomoteurs d'un aeronef |
JP4903086B2 (ja) * | 2007-05-22 | 2012-03-21 | トッパン・フォームズ株式会社 | 紙捌き装置 |
US8967945B2 (en) | 2007-05-22 | 2015-03-03 | United Technologies Corporation | Individual inlet guide vane control for tip turbine engine |
JP2009067586A (ja) * | 2007-09-18 | 2009-04-02 | Toppan Forms Co Ltd | 紙捌き装置 |
DE102010020024B4 (de) | 2010-05-10 | 2016-05-25 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerkssynchronisierverfahren |
GB2524775B (en) * | 2014-04-02 | 2017-11-15 | Rolls Royce Plc | Aircraft vapour trail control system |
US10801361B2 (en) | 2016-09-09 | 2020-10-13 | General Electric Company | System and method for HPT disk over speed prevention |
FR3058278B1 (fr) * | 2016-10-27 | 2020-02-28 | Safran Electrical & Power | Systeme pour l'alimentation d'actionneurs electriques embarques dans un aeronef |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US299630A (en) * | 1884-06-03 | Heistet eichling | ||
GB724196A (en) * | 1950-11-08 | 1955-02-16 | Gen Motors Corp | Improved control system for an aircraft power plant |
US3174284A (en) * | 1963-02-19 | 1965-03-23 | United Aircraft Corp | Power management fuel control for plural gas turbine engines |
US4147035A (en) * | 1978-02-16 | 1979-04-03 | Semco Instruments, Inc. | Engine load sharing control system |
-
1981
- 1981-12-28 SE SE8107800A patent/SE8107800L/sv not_active Application Discontinuation
-
1982
- 1982-01-12 DE DE19823201010 patent/DE3201010A1/de not_active Withdrawn
- 1982-01-15 CA CA000394263A patent/CA1161527A/en not_active Expired
- 1982-01-22 FR FR8200976A patent/FR2502697A1/fr not_active Withdrawn
- 1982-02-10 GB GB8203816A patent/GB2095755A/en not_active Withdrawn
- 1982-03-19 JP JP57042989A patent/JPS57165632A/ja active Pending
- 1982-03-30 BR BR8201832A patent/BR8201832A/pt unknown
- 1982-03-30 IT IT20466/82A patent/IT1151860B/it active
Also Published As
Publication number | Publication date |
---|---|
GB2095755A (en) | 1982-10-06 |
CA1161527A (en) | 1984-01-31 |
DE3201010A1 (de) | 1982-10-07 |
IT8220466A0 (it) | 1982-03-30 |
IT1151860B (it) | 1986-12-24 |
JPS57165632A (en) | 1982-10-12 |
FR2502697A1 (fr) | 1982-10-01 |
BR8201832A (pt) | 1983-03-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAV | Patent application has lapsed |
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