FR3028498B1 - Dispositif pour la commande d'un regime de poussee d'au moins un moteur d'aeronef. - Google Patents

Dispositif pour la commande d'un regime de poussee d'au moins un moteur d'aeronef. Download PDF

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Publication number
FR3028498B1
FR3028498B1 FR1461038A FR1461038A FR3028498B1 FR 3028498 B1 FR3028498 B1 FR 3028498B1 FR 1461038 A FR1461038 A FR 1461038A FR 1461038 A FR1461038 A FR 1461038A FR 3028498 B1 FR3028498 B1 FR 3028498B1
Authority
FR
France
Prior art keywords
regime
pushing
controlling
aircraft engine
aircraft
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.)
Expired - Fee Related
Application number
FR1461038A
Other languages
English (en)
Other versions
FR3028498A1 (fr
Inventor
Brice Fernandez
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 FR1461038A priority Critical patent/FR3028498B1/fr
Priority to US14/940,433 priority patent/US20160137307A1/en
Publication of FR3028498A1 publication Critical patent/FR3028498A1/fr
Application granted granted Critical
Publication of FR3028498B1 publication Critical patent/FR3028498B1/fr
Expired - Fee Related 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
    • B64D31/04—Initiating means actuated personally
    • 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
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/048—Interaction techniques based on graphical user interfaces [GUI]
    • G06F3/0484—Interaction techniques based on graphical user interfaces [GUI] for the control of specific functions or operations, e.g. selecting or manipulating an object, an image or a displayed text element, setting a parameter value or selecting a range
    • G06F3/04842—Selection of displayed objects or displayed text elements
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/048—Interaction techniques based on graphical user interfaces [GUI]
    • G06F3/0484—Interaction techniques based on graphical user interfaces [GUI] for the control of specific functions or operations, e.g. selecting or manipulating an object, an image or a displayed text element, setting a parameter value or selecting a range
    • G06F3/04847—Interaction techniques to control parameter settings, e.g. interaction with sliders or dials
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/048—Interaction techniques based on graphical user interfaces [GUI]
    • G06F3/0487—Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser
    • G06F3/0488—Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser using a touch-screen or digitiser, e.g. input of commands through traced gestures

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Human Computer Interaction (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
FR1461038A 2014-11-14 2014-11-14 Dispositif pour la commande d'un regime de poussee d'au moins un moteur d'aeronef. Expired - Fee Related FR3028498B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1461038A FR3028498B1 (fr) 2014-11-14 2014-11-14 Dispositif pour la commande d'un regime de poussee d'au moins un moteur d'aeronef.
US14/940,433 US20160137307A1 (en) 2014-11-14 2015-11-13 Device for controlling a thrust of at least one aircraft engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1461038A FR3028498B1 (fr) 2014-11-14 2014-11-14 Dispositif pour la commande d'un regime de poussee d'au moins un moteur d'aeronef.
FR1461038 2014-11-14

Publications (2)

Publication Number Publication Date
FR3028498A1 FR3028498A1 (fr) 2016-05-20
FR3028498B1 true FR3028498B1 (fr) 2018-06-01

Family

ID=52273327

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1461038A Expired - Fee Related FR3028498B1 (fr) 2014-11-14 2014-11-14 Dispositif pour la commande d'un regime de poussee d'au moins un moteur d'aeronef.

Country Status (2)

Country Link
US (1) US20160137307A1 (fr)
FR (1) FR3028498B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10106269B1 (en) * 2017-03-17 2018-10-23 Rockwell Collins, Inc. System and method for inadvertent engine shutdown prevention
US11167836B2 (en) 2018-06-21 2021-11-09 Sierra Nevada Corporation Devices and methods to attach composite core to a surrounding structure
US10988266B2 (en) * 2019-01-29 2021-04-27 The Boeing Company Aircraft auxiliary power unit (APU) control system having speed compensation
US10974844B2 (en) 2019-01-29 2021-04-13 The Boeing Company Aircraft auxiliary power unit (APU) control system having speed compensation
US11034463B2 (en) 2019-03-26 2021-06-15 The Boeing Company Aircraft auxiliary power unit (APU) control system having variably sized air inlet

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1661117A4 (fr) * 2003-07-08 2009-01-21 Supersonic Aerospace Int Systemes d'affichage pour un appareil
FR2870522B1 (fr) * 2004-05-18 2007-08-24 Airbus France Sas Indicateur de pilotage affichant les informations de poussee de l'aeronef
US8085168B2 (en) * 2006-07-05 2011-12-27 Bethel Jeffrey D Electronic flight data display instrument
US7869824B2 (en) * 2006-09-06 2011-01-11 Byung Woo Min Cell phone with remote control system
US20090225036A1 (en) * 2007-01-17 2009-09-10 Wright David G Method and apparatus for discriminating between user interactions
FR2943037B1 (fr) * 2009-03-11 2012-09-21 Airbus France Systeme de commande d'aeronef a architecture modulaire integre.
FR2946020B1 (fr) * 2009-06-02 2011-07-15 Airbus France Dispositif pour confirmer la poussee des moteurs d'un aeronef.
DE102009049367A1 (de) * 2009-10-14 2011-04-21 GM Global Technology Operations, Inc., Detroit Anzeige und Verfahren zur Berechnung eines "Eco"-Meterindex zur Darstellung für den Fahrer eines Kraftfahrzeugs
US8497784B1 (en) * 2010-09-01 2013-07-30 Rockwell Collins, Inc. Touch screen clickable crew alert system control
US8725318B1 (en) * 2011-05-20 2014-05-13 Rockwell Collins, Inc. Systems and methods for incorporating virtual network computing into a cockpit display system and controlling a remote aircraft system with the VNC-incorporated CDS
EP2971704B1 (fr) * 2013-03-14 2017-08-23 Rolls-Royce North American Technologies, Inc. Interface de configuration de moteur à turbine à gaz
JP2015066978A (ja) * 2013-09-26 2015-04-13 ヤマハ発動機株式会社 船舶用表示システムおよびそれを備えた小型船舶
US11237710B2 (en) * 2014-06-30 2022-02-01 Lenovo (Singapore) Pte. Ltd. Multi-function slide control
GB201412188D0 (en) * 2014-07-09 2014-08-20 Rolls Royce Plc Two-part gas turbine engine

Also Published As

Publication number Publication date
FR3028498A1 (fr) 2016-05-20
US20160137307A1 (en) 2016-05-19

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