FR3126443B1 - Method for observing and dynamic analysis of the parameters of an aircraft engine and corresponding control system - Google Patents

Method for observing and dynamic analysis of the parameters of an aircraft engine and corresponding control system Download PDF

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Publication number
FR3126443B1
FR3126443B1 FR2109181A FR2109181A FR3126443B1 FR 3126443 B1 FR3126443 B1 FR 3126443B1 FR 2109181 A FR2109181 A FR 2109181A FR 2109181 A FR2109181 A FR 2109181A FR 3126443 B1 FR3126443 B1 FR 3126443B1
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FR
France
Prior art keywords
parameters
command
observing
engine
test equipment
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
FR2109181A
Other languages
French (fr)
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FR3126443A1 (en
Inventor
Mathieu Conq
Stéphanie Phung
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.)
Safran Electronics and Defense SAS
Original Assignee
Safran Electronics and Defense 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 Safran Electronics and Defense SAS filed Critical Safran Electronics and Defense SAS
Priority to FR2109181A priority Critical patent/FR3126443B1/en
Publication of FR3126443A1 publication Critical patent/FR3126443A1/en
Application granted granted Critical
Publication of FR3126443B1 publication Critical patent/FR3126443B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003Arrangements for testing or measuring
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • G05B23/0205Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0218Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
    • G05B23/0256Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults injecting test signals and analyzing monitored process response, e.g. injecting the test signal while interrupting the normal operation of the monitored system; superimposing the test signal onto a control signal during normal operation of the monitored system
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • G05B23/0205Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0259Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
    • G05B23/0283Predictive maintenance, e.g. involving the monitoring of a system and, based on the monitoring results, taking decisions on the maintenance schedule of the monitored system; Estimating remaining useful life [RUL]
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/72Maintenance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/80Diagnostics
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B2219/00Program-control systems
    • G05B2219/30Nc systems
    • G05B2219/45Nc applications
    • G05B2219/45071Aircraft, airplane, ship cleaning manipulator, paint stripping

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)

Abstract

Ce procédé d’observation et d’analyse dynamique des paramètres d’un moteur d’un aéronef comprenant un système de contrôle (1) du moteur comprenant un processeur de contrôle du moteur (2), un module (3) de gestion des paramètres du moteur collectés, et un processeur de maintenance (9) indépendant du processeur de contrôle (2) et connecté d’une part au module (3) de gestion des paramètres du moteur collectés et d’autre part à un équipement de test au sol (7), comprend les étapes suivantes : Sélection (11) sur l’équipement de test d’une commande à réaliser par le processeur de maintenance ;Envoi (12) par l’équipement de test de la commande à réaliser au processeur de maintenance ;Exécution (13) de la commande par le processeur de maintenance ; Envoi (14) du résultat de la commande à l’équipement de test ; et Affichage (15) du résultat reçu Figure de l’abrégé : Fig 2This method of observing and dynamic analysis of the parameters of an aircraft engine comprising an engine control system (1) comprising an engine control processor (2), a parameter management module (3) of the engine collected, and a maintenance processor (9) independent of the control processor (2) and connected on the one hand to the module (3) for managing the collected engine parameters and on the other hand to ground test equipment (7), comprises the following steps: Selection (11) on the test equipment of a command to be carried out by the maintenance processor; Sending (12) by the test equipment of the command to be carried out to the maintenance processor ;Execution (13) of the command by the maintenance processor; sending (14) the result of the command to the test equipment; and Display (15) of the result received Abstract figure: Fig 2

FR2109181A 2021-09-02 2021-09-02 Method for observing and dynamic analysis of the parameters of an aircraft engine and corresponding control system Active FR3126443B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2109181A FR3126443B1 (en) 2021-09-02 2021-09-02 Method for observing and dynamic analysis of the parameters of an aircraft engine and corresponding control system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2109181 2021-09-02
FR2109181A FR3126443B1 (en) 2021-09-02 2021-09-02 Method for observing and dynamic analysis of the parameters of an aircraft engine and corresponding control system

Publications (2)

Publication Number Publication Date
FR3126443A1 FR3126443A1 (en) 2023-03-03
FR3126443B1 true FR3126443B1 (en) 2024-07-12

Family

ID=78212266

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2109181A Active FR3126443B1 (en) 2021-09-02 2021-09-02 Method for observing and dynamic analysis of the parameters of an aircraft engine and corresponding control system

Country Status (1)

Country Link
FR (1) FR3126443B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7278266B2 (en) * 2004-08-31 2007-10-09 General Electric Company Methods and apparatus for gas turbine engine lean blowout avoidance
FR3032545B1 (en) * 2015-02-06 2018-06-01 Airbus (S.A.S.) DEVICE, SYSTEM AND METHOD FOR AIDING THE MAINTENANCE OF AN AIRCRAFT
US10035609B2 (en) * 2016-03-08 2018-07-31 Harris Corporation Wireless engine monitoring system for environmental emission control and aircraft networking

Also Published As

Publication number Publication date
FR3126443A1 (en) 2023-03-03

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