JPS57165632A - Temperature adjustor/synchronizer - Google Patents

Temperature adjustor/synchronizer

Info

Publication number
JPS57165632A
JPS57165632A JP57042989A JP4298982A JPS57165632A JP S57165632 A JPS57165632 A JP S57165632A JP 57042989 A JP57042989 A JP 57042989A JP 4298982 A JP4298982 A JP 4298982A JP S57165632 A JPS57165632 A JP S57165632A
Authority
JP
Japan
Prior art keywords
synchronizer
temperature adjustor
adjustor
temperature
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.)
Pending
Application number
JP57042989A
Other languages
English (en)
Japanese (ja)
Inventor
Ei Deitsukii Tomasu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Avco Corp
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 JPS57165632A publication Critical patent/JPS57165632A/ja
Pending legal-status Critical Current

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
JP57042989A 1981-03-30 1982-03-19 Temperature adjustor/synchronizer Pending JPS57165632A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
JPS57165632A true JPS57165632A (en) 1982-10-12

Family

ID=22942151

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57042989A Pending JPS57165632A (en) 1981-03-30 1982-03-19 Temperature adjustor/synchronizer

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)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008290800A (ja) * 2007-05-22 2008-12-04 Toppan Forms Co Ltd 紙捌き装置
JP2009067586A (ja) * 2007-09-18 2009-04-02 Toppan Forms Co Ltd 紙捌き装置

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4875168A (en) * 1987-12-22 1989-10-17 United Technologies Corporation Engine speed control apparatus
US4934825A (en) * 1987-12-22 1990-06-19 United Technologies Corporation Propeller phase 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
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
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
US7921635B2 (en) 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006110122A2 (en) 2004-12-01 2006-10-19 United Technologies Corporation Inflatable bleed valve for a turbine engine and a method of operating therefore
EP1825115A1 (en) * 2004-12-01 2007-08-29 United Technologies Corporation Remote engine fuel control and electronic engine control for turbine engine
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US7882694B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Variable fan inlet guide vane assembly for gas turbine engine
WO2006110123A2 (en) 2004-12-01 2006-10-19 United Technologies Corporation Vectoring transition duct for turbine engine
WO2006059970A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
EP1825113B1 (en) 2004-12-01 2012-10-24 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006059972A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US7980054B2 (en) 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
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
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008290800A (ja) * 2007-05-22 2008-12-04 Toppan Forms Co Ltd 紙捌き装置
JP2009067586A (ja) * 2007-09-18 2009-04-02 Toppan Forms Co Ltd 紙捌き装置

Also Published As

Publication number Publication date
DE3201010A1 (de) 1982-10-07
FR2502697A1 (fr) 1982-10-01
CA1161527A (en) 1984-01-31
IT8220466A0 (it) 1982-03-30
BR8201832A (pt) 1983-03-01
SE8107800L (sv) 1982-10-01
IT1151860B (it) 1986-12-24
GB2095755A (en) 1982-10-06

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