BR8201832A - Sistema sincronizador de velocidade e equilibrador de temperaturas para motores de turbina - Google Patents

Sistema sincronizador de velocidade e equilibrador de temperaturas para motores de turbina

Info

Publication number
BR8201832A
BR8201832A BR8201832A BR8201832A BR8201832A BR 8201832 A BR8201832 A BR 8201832A BR 8201832 A BR8201832 A BR 8201832A BR 8201832 A BR8201832 A BR 8201832A BR 8201832 A BR8201832 A BR 8201832A
Authority
BR
Brazil
Prior art keywords
turbine engines
speed synchronizer
balancer system
temperature balancer
temperature
Prior art date
Application number
BR8201832A
Other languages
English (en)
Inventor
Thomas A Dickney
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 BR8201832A publication Critical patent/BR8201832A/pt

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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Turbines (AREA)
  • Controls For Constant Speed Travelling (AREA)
BR8201832A 1981-03-30 1982-03-30 Sistema sincronizador de velocidade e equilibrador de temperaturas para motores de turbina BR8201832A (pt)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BR8201832A true BR8201832A (pt) 1983-03-01

Family

ID=22942151

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8201832A BR8201832A (pt) 1981-03-30 1982-03-30 Sistema sincronizador de velocidade e equilibrador de temperaturas para motores de turbina

Country Status (8)

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

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
EP1825116A2 (en) 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
EP1831521B1 (en) 2004-12-01 2008-08-20 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
EP1825177B1 (en) 2004-12-01 2012-01-25 United Technologies Corporation Inflatable bleed valve for turbine engine and method of controlling bleed air
US7854112B2 (en) 2004-12-01 2010-12-21 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
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006059999A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
WO2006059975A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
EP1825117B1 (en) 2004-12-01 2012-06-13 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
DE602004019710D1 (de) 2004-12-01 2009-04-09 United Technologies Corp Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
FR2902408B1 (fr) * 2006-06-19 2008-08-08 Eurocopter France Equilibrage en puissance de deux turbomoteurs d'un aeronef
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
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
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
IT1151860B (it) 1986-12-24
GB2095755A (en) 1982-10-06
FR2502697A1 (fr) 1982-10-01
SE8107800L (sv) 1982-10-01
IT8220466A0 (it) 1982-03-30
CA1161527A (en) 1984-01-31
DE3201010A1 (de) 1982-10-07
JPS57165632A (en) 1982-10-12

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