FR2937008B1 - Procede et dispositif pour la protection d'energie d'un aeronef. - Google Patents

Procede et dispositif pour la protection d'energie d'un aeronef.

Info

Publication number
FR2937008B1
FR2937008B1 FR0805576A FR0805576A FR2937008B1 FR 2937008 B1 FR2937008 B1 FR 2937008B1 FR 0805576 A FR0805576 A FR 0805576A FR 0805576 A FR0805576 A FR 0805576A FR 2937008 B1 FR2937008 B1 FR 2937008B1
Authority
FR
France
Prior art keywords
aircraft
energy protection
engines
verified
calculated
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.)
Active
Application number
FR0805576A
Other languages
English (en)
Other versions
FR2937008A1 (fr
Inventor
Emmanuel Blanvillain
Florian Constans
David Chabe
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 FR0805576A priority Critical patent/FR2937008B1/fr
Priority to US12/575,286 priority patent/US8249792B2/en
Publication of FR2937008A1 publication Critical patent/FR2937008A1/fr
Application granted granted Critical
Publication of FR2937008B1 publication Critical patent/FR2937008B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • B64D31/09—Initiating means actuated automatically in response to power plant failure
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0072—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements to counteract a motor failure

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Turbines (AREA)

Abstract

Selon l'invention, on calcule un seuil de vitesse de l'aéronef (AC) afin de pouvoir déterminer une puissance totale à appliquer aux moteurs de l'aéronef (AC). Lorsque des conditions d'activation sont vérifiées, on modifie progressivement la puissance courante individuelle de chacun des moteurs de l'aéronef (AC) non en panne commandés par une fonction de protection.
FR0805576A 2008-10-09 2008-10-09 Procede et dispositif pour la protection d'energie d'un aeronef. Active FR2937008B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0805576A FR2937008B1 (fr) 2008-10-09 2008-10-09 Procede et dispositif pour la protection d'energie d'un aeronef.
US12/575,286 US8249792B2 (en) 2008-10-09 2009-10-07 Method and device for the energy protection of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0805576A FR2937008B1 (fr) 2008-10-09 2008-10-09 Procede et dispositif pour la protection d'energie d'un aeronef.

Publications (2)

Publication Number Publication Date
FR2937008A1 FR2937008A1 (fr) 2010-04-16
FR2937008B1 true FR2937008B1 (fr) 2010-11-05

Family

ID=40756670

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0805576A Active FR2937008B1 (fr) 2008-10-09 2008-10-09 Procede et dispositif pour la protection d'energie d'un aeronef.

Country Status (2)

Country Link
US (1) US8249792B2 (fr)
FR (1) FR2937008B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2973777B1 (fr) * 2011-04-07 2014-04-18 Airbus Operations Sas Dispositif de protection d'energie pour un aeronef.
FR3016158B1 (fr) * 2014-01-09 2017-09-01 Airbus Operations Sas Dispositif de protection d'energie pour un aeronef.
GB201405894D0 (en) 2014-04-02 2014-05-14 Rolls Royce Plc Aircraft vapour trail control system
FR3035642B1 (fr) * 2015-04-30 2017-04-21 Airbus Operations Sas Aeronef equipe d'un dispositif de surveillance de la gestion electronique des moteurs
US9862499B2 (en) * 2016-04-25 2018-01-09 Airbus Operations (S.A.S.) Human machine interface for displaying information relative to the energy of an aircraft
US10737798B2 (en) * 2016-09-12 2020-08-11 Ansel Misfeldt Integrated feedback to flight controller
FR3065443B1 (fr) * 2017-04-19 2021-01-01 Airbus Group Sas Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee
FR3092317B1 (fr) * 2019-02-01 2021-01-08 Safran Electrical & Power Systeme de propulsion d’aeronef
US11002185B2 (en) * 2019-03-27 2021-05-11 Pratt & Whitney Canada Corp. Compounded internal combustion engine
CN113488981B (zh) * 2021-06-15 2023-09-29 南京航空航天大学 无人机配电系统双路供电短路保护电路及方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4662171A (en) * 1986-03-31 1987-05-05 The Boeing Company Automatic thrust restoration system
US5353022A (en) * 1987-08-06 1994-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5363317A (en) * 1992-10-29 1994-11-08 United Technologies Corporation Engine failure monitor for a multi-engine aircraft having partial engine failure and driveshaft failure detection
FR2753171B1 (fr) * 1996-09-09 1998-11-13 Aerospatiale Dispositif de controle de la poussee d'un aeronef a plusieurs moteurs
US6695264B2 (en) * 2000-05-16 2004-02-24 Bell Helicopter Textron, Inc. Power lever tactile cueing system
FR2845350B1 (fr) * 2002-10-02 2004-12-17 Airbus France Procede et dispositif pour commander automatiquement la pousse d'au moins un moteur d'un aeronef lors d'une phase de vol horizontal a vitesse stabilisee
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
US7406370B2 (en) * 2004-08-24 2008-07-29 Honeywell International Inc. Electrical energy management system on a more electric vehicle
FR2890645B1 (fr) * 2005-09-13 2007-10-12 Airbus France Sas Dispositif de protection d'energie pour un avion.

Also Published As

Publication number Publication date
US20100100262A1 (en) 2010-04-22
FR2937008A1 (fr) 2010-04-16
US8249792B2 (en) 2012-08-21

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