IT1151860B - Impianto sincronizzatore e di assetto della temperatura - Google Patents

Impianto sincronizzatore e di assetto della temperatura

Info

Publication number
IT1151860B
IT1151860B IT20466/82A IT2046682A IT1151860B IT 1151860 B IT1151860 B IT 1151860B IT 20466/82 A IT20466/82 A IT 20466/82A IT 2046682 A IT2046682 A IT 2046682A IT 1151860 B IT1151860 B IT 1151860B
Authority
IT
Italy
Prior art keywords
temperature setting
synchronizing system
synchronizing
setting
temperature
Prior art date
Application number
IT20466/82A
Other languages
English (en)
Italian (it)
Other versions
IT8220466A0 (it
Inventor
Thomas A Dickey
Original Assignee
Avco Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Avco Corp filed Critical Avco Corp
Publication of IT8220466A0 publication Critical patent/IT8220466A0/it
Application granted granted Critical
Publication of IT1151860B publication Critical patent/IT1151860B/it

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; 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)
IT20466/82A 1981-03-30 1982-03-30 Impianto sincronizzatore e di assetto della temperatura IT1151860B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US24912581A 1981-03-30 1981-03-30

Publications (2)

Publication Number Publication Date
IT8220466A0 IT8220466A0 (it) 1982-03-30
IT1151860B true IT1151860B (it) 1986-12-24

Family

ID=22942151

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20466/82A IT1151860B (it) 1981-03-30 1982-03-30 Impianto sincronizzatore e di assetto della temperatura

Country Status (8)

Country Link
JP (1) JPS57165632A (fr)
BR (1) BR8201832A (fr)
CA (1) CA1161527A (fr)
DE (1) DE3201010A1 (fr)
FR (1) FR2502697A1 (fr)
GB (1) GB2095755A (fr)
IT (1) IT1151860B (fr)
SE (1) SE8107800L (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
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
WO2006059970A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine equipe d'un ventilateur et d'un compresseur entraines par un engrenage differentiel
WO2006059982A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Regulateur a distance de carburant moteur et regulateur electronique moteur pour moteur a turbine
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
US7934902B2 (en) 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
EP1825113B1 (fr) 2004-12-01 2012-10-24 United Technologies Corporation Boîte de vitesses contre-rotative pour moteur à turbine en bout
EP2333287A1 (fr) 2004-12-01 2011-06-15 United Technologies Corporation Vectorisation de conduite de transition pour moteur de turbine
EP1825116A2 (fr) 2004-12-01 2007-08-29 United Technologies Corporation Refroidissement par ejecteur de l'enveloppe exterieure d'un moteur a turbine de bout
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
EP1828591B1 (fr) 2004-12-01 2010-07-21 United Technologies Corporation Foyer peripherique pour moteur a turbine de bout
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
EP1828683B1 (fr) 2004-12-01 2013-04-10 United Technologies Corporation Dispositif de combustion pour moteur de turbine
WO2006060000A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Ensemble aubes de guidage d'admission de soufflante variable, turbomachine dotee d'un tel ensemble et procede de commande correspondant
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
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)

* Cited by examiner, † Cited by third party
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
FR2502697A1 (fr) 1982-10-01
BR8201832A (pt) 1983-03-01
SE8107800L (sv) 1982-10-01
JPS57165632A (en) 1982-10-12
DE3201010A1 (de) 1982-10-07
CA1161527A (fr) 1984-01-31
IT8220466A0 (it) 1982-03-30
GB2095755A (en) 1982-10-06

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