IT1236706B - Sistema sincrofasatore per turbomotore d'aeroplano. - Google Patents

Sistema sincrofasatore per turbomotore d'aeroplano.

Info

Publication number
IT1236706B
IT1236706B IT02238089A IT2238089A IT1236706B IT 1236706 B IT1236706 B IT 1236706B IT 02238089 A IT02238089 A IT 02238089A IT 2238089 A IT2238089 A IT 2238089A IT 1236706 B IT1236706 B IT 1236706B
Authority
IT
Italy
Prior art keywords
turbomotor
airplane
synchrophase system
synchrophase
airplane turbomotor
Prior art date
Application number
IT02238089A
Other languages
English (en)
Other versions
IT8922380A1 (it
IT8922380A0 (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8922380A0 publication Critical patent/IT8922380A0/it
Publication of IT8922380A1 publication Critical patent/IT8922380A1/it
Application granted granted Critical
Publication of IT1236706B publication Critical patent/IT1236706B/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Reduction Or Emphasis Of Bandwidth Of Signals (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)
IT02238089A 1988-11-21 1989-11-14 Sistema sincrofasatore per turbomotore d'aeroplano. IT1236706B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/274,511 US5058376A (en) 1988-11-21 1988-11-21 Turbofan synchrophaser

Publications (3)

Publication Number Publication Date
IT8922380A0 IT8922380A0 (it) 1989-11-14
IT8922380A1 IT8922380A1 (it) 1991-05-14
IT1236706B true IT1236706B (it) 1993-03-26

Family

ID=23048498

Family Applications (1)

Application Number Title Priority Date Filing Date
IT02238089A IT1236706B (it) 1988-11-21 1989-11-14 Sistema sincrofasatore per turbomotore d'aeroplano.

Country Status (6)

Country Link
US (1) US5058376A (it)
JP (1) JPH02191824A (it)
DE (1) DE3938440A1 (it)
FR (1) FR2639444A1 (it)
GB (1) GB2225134B (it)
IT (1) IT1236706B (it)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5453943A (en) * 1994-02-18 1995-09-26 United Technologies Corporation Adaptive synchrophaser for reducing aircraft cabin noise and vibration
US5517819A (en) * 1994-12-19 1996-05-21 General Electric Company Engine full authority digital engine control automatic mach hold
DE10062252A1 (de) 2000-12-14 2002-07-11 Rolls Royce Deutschland Verfahren zur Regelung von Fluggasturbinen
FR2979901B1 (fr) * 2011-09-09 2013-09-06 Snecma Procede de synchronisation des moteurs d'un avion
FR3019913B1 (fr) 2014-04-15 2017-07-21 Snecma Procede de synchronisation des moteurs d'un avion a double etat intermediaire
US9695752B2 (en) 2014-09-05 2017-07-04 Honeywell International Inc. Engine-induced aircraft cabin resonance reduction system and method
CA2979615C (en) 2015-03-16 2023-09-26 Bombardier Inc. Synchronization of aircraft engines
US10745110B2 (en) * 2018-06-29 2020-08-18 Pratt & Whitney Canada Corp. Propeller blade synchrophasing using phonic wheel
EP3626628B1 (en) * 2018-09-18 2021-09-01 Bombardier Inc. System and method for synchrophasing aircraft engines

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2887621A (en) * 1956-01-31 1959-05-19 Curtiss Wright Corp Speed and phase synchronizers
US3186165A (en) * 1961-11-29 1965-06-01 Gen Electric Turbofan engine speed synchronizing arrangement
US3368346A (en) * 1965-05-18 1968-02-13 Lucas Industries Ltd Synchronising control means for multiple gas turbine engine installations
US3365882A (en) * 1965-07-13 1968-01-30 Greune Christian Apparatus for the control of fuel for two or more internal combustion engines operating on the same drive shaft, especially gas turbine installations
US3589832A (en) * 1969-12-15 1971-06-29 Garett Corp The Propeller synchrophaser system
US3689175A (en) * 1970-08-11 1972-09-05 Piqua Aircraft Co Inc Apparatus for controlling the speed and phase of engines
US3811273A (en) * 1973-03-08 1974-05-21 United Aircraft Corp Slaved fuel control for multi-engined aircraft
GB1573095A (en) * 1976-11-26 1980-08-13 Lucas Industries Ltd Fuel control for a multi engine gas turbine installation
US4245955A (en) * 1978-12-14 1981-01-20 The Cessna Aircraft Company Phase and speed control system
US4653981A (en) * 1985-09-30 1987-03-31 United Technologies Corporation Propeller synchrophaser
US4659283A (en) * 1985-09-30 1987-04-21 United Technologies Corporation Propeller Synchrophaser® device and mode logic

Also Published As

Publication number Publication date
DE3938440A1 (de) 1990-06-13
GB8925297D0 (en) 1989-12-28
IT8922380A1 (it) 1991-05-14
JPH0587657B2 (it) 1993-12-17
GB2225134B (en) 1993-01-20
JPH02191824A (ja) 1990-07-27
IT8922380A0 (it) 1989-11-14
GB2225134A (en) 1990-05-23
FR2639444A1 (fr) 1990-05-25
US5058376A (en) 1991-10-22

Similar Documents

Publication Publication Date Title
NO891204D0 (no) Premestrings-system.
NO894666D0 (no) Elektroakustisk system.
BR8704061A (pt) Sistema
BR8702304A (pt) Sistema de fornecimento de aerosol flavorizante
BR8707625A (pt) Sistema de tele-enlace
DE68910979D1 (de) Verbindungssystem.
IT8523321A0 (it) Sistema per il rilascio a velocita' controllata di sostanze attive.
IT1240206B (it) Sistema radar
ES2018577B3 (es) Sistema de almacenamiento.
IT1236706B (it) Sistema sincrofasatore per turbomotore d'aeroplano.
FI901125A0 (fi) Smakgivande system foer fettfria livsmedel.
IT9067292A0 (is) sistema radar
BR9007233A (pt) Sistema de barbear
IT1230308B (it) Sistema stampante modulare.
DE68920870D1 (de) Tastaturbedientes system.
IT8922176A0 (it) Sistema ottico.
BR8800786A (pt) Sistema de barbeador
IT8860437V0 (it) Sistema duesse.
LT2375B (lt) Sausinimo-drekinimo sistema
NO902816L (no) Landingsinnflyvnings-system for luftfartoey.
NO880199D0 (no) "dommerfloeyte"-system.
IT8809325A0 (it) Sistema di antifurto-antirapina per autovetture
ES1006904Y (es) Sistema de revestimiento de paramentos.
IT1234528B (it) Elioimpianto antighiaccio.
NO885230D0 (no) Bgekraft-system.

Legal Events

Date Code Title Description
0001 Granted