FR2502697A1 - Dispositif d'equilibrage des temperatures et des vitesses des moteurs d'avion pendant la phase de croisiere du vol - Google Patents
Dispositif d'equilibrage des temperatures et des vitesses des moteurs d'avion pendant la phase de croisiere du vol Download PDFInfo
- Publication number
- FR2502697A1 FR2502697A1 FR8200976A FR8200976A FR2502697A1 FR 2502697 A1 FR2502697 A1 FR 2502697A1 FR 8200976 A FR8200976 A FR 8200976A FR 8200976 A FR8200976 A FR 8200976A FR 2502697 A1 FR2502697 A1 FR 2502697A1
- Authority
- FR
- France
- Prior art keywords
- temperature
- engine
- turbine
- power
- speed
- 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- Withdrawn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
- 239000000446 fuel Substances 0.000 claims abstract description 25
- 239000007789 gas Substances 0.000 claims description 22
- 238000012937 correction Methods 0.000 claims description 18
- 230000007935 neutral effect Effects 0.000 claims description 10
- 238000002485 combustion reaction Methods 0.000 claims description 7
- 230000007423 decrease Effects 0.000 claims description 5
- 238000005259 measurement Methods 0.000 claims description 2
- 238000002360 preparation method Methods 0.000 claims 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 238000004891 communication Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000003247 decreasing effect Effects 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 3
- 230000006866 deterioration Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000009347 mechanical transmission Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000011664 signaling Effects 0.000 description 2
- 241000238876 Acari Species 0.000 description 1
- 229920001468 Cordura Polymers 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000013641 positive control Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Controls For Constant Speed Travelling (AREA)
- Control Of Turbines (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US24912581A | 1981-03-30 | 1981-03-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2502697A1 true FR2502697A1 (fr) | 1982-10-01 |
Family
ID=22942151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8200976A Withdrawn FR2502697A1 (fr) | 1981-03-30 | 1982-01-22 | Dispositif d'equilibrage des temperatures et des vitesses des moteurs d'avion pendant la phase de croisiere du vol |
Country Status (8)
Country | Link |
---|---|
JP (1) | JPS57165632A (it) |
BR (1) | BR8201832A (it) |
CA (1) | CA1161527A (it) |
DE (1) | DE3201010A1 (it) |
FR (1) | FR2502697A1 (it) |
GB (1) | GB2095755A (it) |
IT (1) | IT1151860B (it) |
SE (1) | SE8107800L (it) |
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 |
DE602004016065D1 (de) | 2004-12-01 | 2008-10-02 | United Technologies Corp | Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren |
EP1825113B1 (en) | 2004-12-01 | 2012-10-24 | United Technologies Corporation | Counter-rotating gearbox for tip turbine engine |
WO2006110123A2 (en) | 2004-12-01 | 2006-10-19 | United Technologies Corporation | Vectoring transition duct for turbine engine |
EP1828591B1 (en) | 2004-12-01 | 2010-07-21 | United Technologies Corporation | Peripheral combustor for tip turbine engine |
US7934902B2 (en) | 2004-12-01 | 2011-05-03 | United Technologies Corporation | Compressor variable stage remote actuation for turbine engine |
WO2006059986A1 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Tip turbine engine and operating method with reverse core airflow |
EP1825115A1 (en) * | 2004-12-01 | 2007-08-29 | United Technologies Corporation | Remote engine fuel control and electronic engine control for turbine engine |
EP1828547B1 (en) | 2004-12-01 | 2011-11-30 | United Technologies Corporation | Turbofan comprising a plurality of individually controlled inlet guide vanes and corresponding controlling method |
EP1828683B1 (en) | 2004-12-01 | 2013-04-10 | United Technologies Corporation | Combustor for turbine engine |
US7845157B2 (en) | 2004-12-01 | 2010-12-07 | United Technologies Corporation | Axial compressor for tip turbine engine |
WO2006059970A2 (en) | 2004-12-01 | 2006-06-08 | United Technologies Corporation | Turbine engine with differential gear driven fan and compressor |
EP1825177B1 (en) | 2004-12-01 | 2012-01-25 | United Technologies Corporation | Inflatable bleed valve for turbine engine and method of controlling bleed air |
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 |
Citations (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/xx 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
Patent Citations (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 |
Also Published As
Publication number | Publication date |
---|---|
DE3201010A1 (de) | 1982-10-07 |
SE8107800L (sv) | 1982-10-01 |
IT1151860B (it) | 1986-12-24 |
JPS57165632A (en) | 1982-10-12 |
GB2095755A (en) | 1982-10-06 |
BR8201832A (pt) | 1983-03-01 |
IT8220466A0 (it) | 1982-03-30 |
CA1161527A (en) | 1984-01-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2502697A1 (fr) | Dispositif d'equilibrage des temperatures et des vitesses des moteurs d'avion pendant la phase de croisiere du vol | |
US10773816B2 (en) | Single lever turboprop control systems and methods utilizing torque-based and power-based scheduling | |
US3963372A (en) | Helicopter power plant control | |
CA2509488C (fr) | Systeme et procede de controle d'un flux d'air dans une turbine a gaz | |
CA3024808A1 (en) | Torque signal dynamic compensation based on sensor location | |
US4551972A (en) | Engine management system | |
FR3037672A1 (fr) | Drone comportant des moyens perfectionnes de compensation du biais de la centrale inertielle en fonction de la temperature | |
US10961921B2 (en) | Model-based control system and method for a turboprop engine | |
US2857739A (en) | Control system for turbo-jet engine | |
FR2508104A1 (fr) | Dispositif de commande pour un moteur pouvant fonctionner avec deux carburants gaz/gazole | |
JPS6132484B2 (it) | ||
CA3011878C (en) | Method of controlling gas generator power and torque output | |
EP0637683A1 (fr) | Système de ventilation des disques et du stator de turbine d'un turboréacteur | |
US4245462A (en) | Starting system for a turbine engine | |
FR2485473A1 (fr) | Installation de conditionnement d'air pour avions | |
US20190032557A1 (en) | System and method for variable geometry mechanism control | |
US2437546A (en) | Supercharged engine control | |
EP3647568A1 (en) | Autothrottle control system on turbopropeller-powered aircraft | |
GB2065779A (en) | Gas turbine fuel system | |
FR2540182A1 (fr) | Dispositif de commande isochrone de vitesse pour moteur a turbine a gaz et methode de commande | |
CA3101537A1 (en) | System and method for propeller speed governing | |
US20210102501A1 (en) | Methods of Manufacturing Cadmium Telluride Thin Film Photovoltaic Devices | |
RU2306446C1 (ru) | Способ управления силовой установкой самолета | |
US11371436B2 (en) | Method and system for regulating oil flow to an engine | |
US3514949A (en) | Turboprop fuel control for use with contaminated or varied fuels |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |