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
Authority: BR; Brazil
Prior art keywords: turbine engines; speed synchronizer; balancer system; temperature balancer; temperature
Prior art date: 1981-03-30

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.)

1981-03-30

Filing date

1982-03-30

Publication date

1983-03-01

1982-03-30 Application filed by Avco Corp filed Critical Avco Corp

1983-03-01 Publication of BR8201832A publication Critical patent/BR8201832A/pt

Links

RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 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)
Control Of Turbines (AREA)
Controls For Constant Speed Travelling (AREA)
Combined Controls Of Internal Combustion Engines (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
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
DE602004016065D1 (de)	2004-12-01	2008-10-02	United Technologies Corp	Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
US20090145105A1 (en) *	2004-12-01	2009-06-11	Suciu Gabriel L	Remote engine fuel control and electronic engine control for turbine engine
EP1825117B1 (en)	2004-12-01	2012-06-13	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
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
EP1828591B1 (en)	2004-12-01	2010-07-21	United Technologies Corporation	Peripheral combustor for tip turbine engine
US7976272B2 (en)	2004-12-01	2011-07-12	United Technologies Corporation	Inflatable bleed valve for a turbine engine
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
EP1825116A2 (en)	2004-12-01	2007-08-29	United Technologies Corporation	Ejector cooling of outer case for tip turbine engine
DE602004031470D1 (de)	2004-12-01	2011-03-31	United Technologies Corp	Übergangskanal mit mitteln zur strömungsvektorbeeinflussung bei einer gasturbine
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
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

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

Also Published As

Publication number	Publication date
SE8107800L (sv)	1982-10-01
IT1151860B (it)	1986-12-24
IT8220466A0 (it)	1982-03-30
DE3201010A1 (de)	1982-10-07
CA1161527A (en)	1984-01-31
JPS57165632A (en)	1982-10-12
GB2095755A (en)	1982-10-06
FR2502697A1 (fr)	1982-10-01

Publication	Publication Date	Title
BR8201832A (pt)	1983-03-01	Sistema sincronizador de velocidade e equilibrador de temperaturas para motores de turbina
BR8008819A (pt)	1981-06-23	Sistema de suprimento de lubrificacao em um motor de turbina a gas
BR8003139A (pt)	1980-12-23	Sistema de transmissao para motores de barcos
ES547607A0 (es)	1986-09-01	Sistema de refrigeracion, en particular para motores de com-bustion
DK57781A (da)	1982-02-19	Reciprocerende termisk motor
IT1083025B (it)	1985-05-21	Sistema di lubrificazione per motori a turbina
ES504841A0 (es)	1982-05-16	Perfeccionamientos en sistemas de gobierno para motores de avion.
DK32980A (da)	1980-01-25	Motorsystem med variabel reluktans
BR8204232A (pt)	1983-07-12	Sistema de ignicao para motores a combustao
BR7808765A (pt)	1981-06-30	Sistema de lubrificacao centrifuga para mancais de cavidade de transmissao
DK147207C (da)	1984-11-05	Koelesystem ved vaeskekoelet forbraendingsmotor
DK32880A (da)	1980-01-25	Motorsystem med variabel reluktans
ES267115Y (es)	1983-12-16	Refrigerador perfeccionado para motores de combustion de automoviles.
BR8203812A (pt)	1983-06-28	Sistema de ignicao regulada para motores
MX160552A (es)	1990-03-22	Mejoras en sistema de combustion catalitica para turbina de gas estacionaria
DK182782A (da)	1982-10-26	Koelesystem til en forbraendingsmotor
AR230756A1 (es)	1984-06-29	Turbina de combustion
BR8400806A (pt)	1984-11-13	Otimizacao de sistema de turbina atraves de blocos de funcao
ES512872A0 (es)	1983-05-01	Inyector-bomba para motores diesel.
ES506134A0 (es)	1982-08-16	Sistema para refrigeracion de cilindros giratorios
BR8203784A (pt)	1983-06-21	Combustor para sistema de turbina de combustao
BR8203361A (pt)	1984-01-10	Combustor para turbina de combustao
BR8204910A (pt)	1983-08-02	Combustor para sistema de turbina de combustao
BR8407274A (pt)	1986-01-21	Sistema de combustivel para motores de explosao
BR5900998U (pt)	1981-02-03	Sistema de refrigeracao do oleo de motores