FR3050177B1 - Systeme et procede de commande de la poussee des moteurs d'un aeronef - Google Patents

Systeme et procede de commande de la poussee des moteurs d'un aeronef Download PDF

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Publication number
FR3050177B1
FR3050177B1 FR1653426A FR1653426A FR3050177B1 FR 3050177 B1 FR3050177 B1 FR 3050177B1 FR 1653426 A FR1653426 A FR 1653426A FR 1653426 A FR1653426 A FR 1653426A FR 3050177 B1 FR3050177 B1 FR 3050177B1
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France
Prior art keywords
aircraft
setpoint
engines
thrust
controlling
Prior art date
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Active
Application number
FR1653426A
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English (en)
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FR3050177A1 (fr
Inventor
Fabien Guignard
Priteche Venilal
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1653426A priority Critical patent/FR3050177B1/fr
Priority to US15/478,765 priority patent/US10494114B2/en
Publication of FR3050177A1 publication Critical patent/FR3050177A1/fr
Application granted granted Critical
Publication of FR3050177B1 publication Critical patent/FR3050177B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • B64D31/08—Initiating means actuated automatically for keeping cruising speed constant
    • 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
    • F02C9/44—Control of fuel supply responsive to the speed of aircraft, e.g. Mach number control, optimisation of fuel consumption
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B15/00—Systems controlled by a computer
    • G05B15/02—Systems controlled by a computer electric
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/063—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the motors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/051—Thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/12—Purpose of the control system to maintain desired vehicle trajectory parameters
    • F05D2270/122—Speed or Mach number

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Control Of Turbines (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Velocity Or Acceleration (AREA)

Abstract

Le système (20) de commande de la poussée des moteurs d'un aéronef (1) comprend une unité de traitement (24) configurée pour recevoir une consigne de vitesse (VT) de l'aéronef, pour déterminer une consigne de commande d'au moins un moteur de l'aéronef en fonction de ladite consigne de vitesse et pour transmettre une consigne (COM) à un contrôleur (30) dudit au moins un moteur de l'aéronef en fonction de ladite consigne de commande. L'unité de traitement est en outre configurée pour recevoir une information (Turb) de mesure de niveau de turbulence courant et pour ajouter une consigne complémentaire de vitesse (VTC), fonction du niveau de turbulence, à ladite consigne de vitesse.
FR1653426A 2016-04-19 2016-04-19 Systeme et procede de commande de la poussee des moteurs d'un aeronef Active FR3050177B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1653426A FR3050177B1 (fr) 2016-04-19 2016-04-19 Systeme et procede de commande de la poussee des moteurs d'un aeronef
US15/478,765 US10494114B2 (en) 2016-04-19 2017-04-04 System and method for controlling the thrust of the engines of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1653426A FR3050177B1 (fr) 2016-04-19 2016-04-19 Systeme et procede de commande de la poussee des moteurs d'un aeronef

Publications (2)

Publication Number Publication Date
FR3050177A1 FR3050177A1 (fr) 2017-10-20
FR3050177B1 true FR3050177B1 (fr) 2021-06-25

Family

ID=56802554

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1653426A Active FR3050177B1 (fr) 2016-04-19 2016-04-19 Systeme et procede de commande de la poussee des moteurs d'un aeronef

Country Status (2)

Country Link
US (1) US10494114B2 (fr)
FR (1) FR3050177B1 (fr)

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3758764A (en) * 1970-10-29 1973-09-11 United Aircraft Corp Turbine power plant control with an on-line optimization control
US3840200A (en) * 1973-03-19 1974-10-08 Boeing Co Turbulence compensated throttle control system
US4312041A (en) * 1978-02-22 1982-01-19 Lear Siegler, Inc. Flight performance data computer system
US4422147A (en) * 1980-09-08 1983-12-20 The Boeing Company Wind shear responsive turbulence compensated aircraft throttle control system
US7411519B1 (en) * 1999-05-14 2008-08-12 Honeywell International Inc. System and method for predicting and displaying wake vortex turbulence
US6273370B1 (en) * 1999-11-01 2001-08-14 Lockheed Martin Corporation Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements
DE10101829A1 (de) * 2001-01-17 2002-07-18 Bosch Gmbh Robert Schaltablaufsteuerung und Verfahren zum Koordinieren von Schaltungsabläufen
FR2841008B1 (fr) * 2002-06-12 2004-08-20 Airbus France Procede et systeme de pilotage d'un aeronef
GB0307035D0 (en) * 2003-03-26 2003-04-30 Rolls Royce Plc Acceleration control in a multi-spool gas turbine engine
US7109912B1 (en) * 2004-05-04 2006-09-19 Rockwell Collins, Inc. Weather radar hazard detection system and method
US7512464B2 (en) * 2005-12-22 2009-03-31 The Boeing Company System and method for controlling the speed of an aircraft
FR2899350B1 (fr) * 2006-03-30 2011-04-22 Airbus France Procede et dispositif pour determiner la turbulence de l'air susceptible d'etre rencontree par un aeronef
FR2903964B1 (fr) * 2006-07-18 2009-05-29 Airbus France Sas Procede et dispositif pour detecter une turbulence de l'air dans l'environnement d'un aeronef.
US7438259B1 (en) * 2006-08-16 2008-10-21 Piasecki Aircraft Corporation Compound aircraft control system and method
FR2907541B1 (fr) * 2006-10-24 2009-01-16 Thales Sa Procede de gestion automatique de la vitesse d'un aeronef en air turbulent et dispositif pour sa mise en oeuvre
FR2917508B1 (fr) * 2007-06-15 2009-08-28 Thales Sa Procede de caracterisation d'une turbulence atmospherique par des parametres representatifs mesures par un radar
US7917255B1 (en) * 2007-09-18 2011-03-29 Rockwell Colllins, Inc. System and method for on-board adaptive characterization of aircraft turbulence susceptibility as a function of radar observables
US7696921B1 (en) * 2008-05-06 2010-04-13 Rockwell Collins, Inc. System and method for turbulence detection
NL2002064C (nl) * 2008-10-07 2010-04-08 Robertus Gerardus De Boer Gedifferentieerde stuwkracht startmethode voor een vliegtuig.
US7982658B2 (en) * 2009-03-31 2011-07-19 Honeywell International Inc. Systems and methods for assessing weather in proximity to an airborne aircraft
US8742973B1 (en) * 2011-09-22 2014-06-03 Rockwell Collins, Inc. System and method of determining increased turbulence susceptibility with elapsed flight time
US9019146B1 (en) * 2011-09-27 2015-04-28 Rockwell Collins, Inc. Aviation display depiction of weather threats
US20130226373A1 (en) * 2012-02-27 2013-08-29 Ge Aviation Systems Llc Methods for in-flight adjusting of a flight plan
WO2014143219A1 (fr) * 2013-03-13 2014-09-18 Phillips Steven D Contrôle de santé de moteur et commande d'attribution de puissance pour un moteur à turbine à l'aide de générateurs électriques
US20150203215A1 (en) * 2014-01-17 2015-07-23 Eric T. Falangas Early performance evaluation of conceptual flight and space vehicles
FR3022355B1 (fr) * 2014-06-16 2018-03-30 Thales Procede et dispositif de commande d'au moins un systeme de controle d'actionneur d'un aeronef, produit programme d'ordinateur et aeronef associes
US20160208742A1 (en) * 2015-01-17 2016-07-21 John Bradley Pande DiscThruster, pressure thrust based aircraft engine
US10203700B2 (en) * 2016-02-29 2019-02-12 Garmin International, Inc. Emergency autoland system

Also Published As

Publication number Publication date
FR3050177A1 (fr) 2017-10-20
US20170297731A1 (en) 2017-10-19
US10494114B2 (en) 2019-12-03

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