FR3104347B1 - Architecture parallélisée pour le pilotage d’actionneurs électromécaniques - Google Patents
Architecture parallélisée pour le pilotage d’actionneurs électromécaniques Download PDFInfo
- Publication number
- FR3104347B1 FR3104347B1 FR1913943A FR1913943A FR3104347B1 FR 3104347 B1 FR3104347 B1 FR 3104347B1 FR 1913943 A FR1913943 A FR 1913943A FR 1913943 A FR1913943 A FR 1913943A FR 3104347 B1 FR3104347 B1 FR 3104347B1
- Authority
- FR
- France
- Prior art keywords
- electromechanical actuators
- controlling
- electromechanical
- converter
- parallel architecture
- 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
Links
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P5/00—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors
- H02P5/46—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors for speed regulation of two or more dynamo-electric motors in relation to one another
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- 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
-
- 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
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P6/00—Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
- H02P6/04—Arrangements for controlling or regulating the speed or torque of more than one motor
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L12/407—Bus networks with decentralised control
- H04L12/413—Bus networks with decentralised control with random access, e.g. carrier-sense multiple-access with collision detection [CSMA-CD]
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- 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
- F05D2240/00—Components
- F05D2240/40—Use of a multiplicity of similar components
-
- 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
- F05D2270/40—Type of control system
- F05D2270/46—Type of control system redundant, i.e. failsafe operation
-
- 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
- F05D2270/50—Control logic embodiments
- F05D2270/52—Control logic embodiments by electrical means, e.g. relays or switches
-
- 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
- F05D2270/60—Control system actuates means
- F05D2270/62—Electrical actuators
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Operation Control Of Excavators (AREA)
- Control Of Multiple Motors (AREA)
Abstract
Architecture parallélisée pour le pilotage d’actionneurs électromécaniques Dans une chaîne d’actionnement électromécanique pour la commande du déplacement de charges mobiles (22) d’une turbomachine aéronautique depuis une unité de commande (24), chacune de ces charges mobiles étant actionnée par un actionneur électromécanique (30) commandé par un convertisseur (36), il est prévu, pour commander ce déplacement, un unique contrôleur Ethernet à commande déterministe (32) assurant via un bus Ethernet (36) le contrôle de chacun des convertisseurs (36) agissant sur les actionneurs électromécaniques et un convertisseur donné pilotant en parallèle une paire ou plusieurs paires d’actionneurs électromécaniques et chacun des actionneurs électromécaniques étant relié à ce convertisseur par un interrupteur (40). Figure pour l’abrégé : Fig. 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1913943A FR3104347B1 (fr) | 2019-12-09 | 2019-12-09 | Architecture parallélisée pour le pilotage d’actionneurs électromécaniques |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1913943 | 2019-12-09 | ||
FR1913943A FR3104347B1 (fr) | 2019-12-09 | 2019-12-09 | Architecture parallélisée pour le pilotage d’actionneurs électromécaniques |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3104347A1 FR3104347A1 (fr) | 2021-06-11 |
FR3104347B1 true FR3104347B1 (fr) | 2021-12-03 |
Family
ID=69811172
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1913943A Active FR3104347B1 (fr) | 2019-12-09 | 2019-12-09 | Architecture parallélisée pour le pilotage d’actionneurs électromécaniques |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3104347B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3125180A1 (fr) * | 2021-07-06 | 2023-01-13 | Safran Aircraft Engines | Chaîne d’actionnement électromécanique pour le pilotage du déplacement de charges mobiles d’une turbomachine aéronautique |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8125164B2 (en) * | 2008-07-18 | 2012-02-28 | The Boeing Company | Parallel motor controller architecture |
US20120185116A1 (en) * | 2011-01-14 | 2012-07-19 | Hamilton Sundstrand Corporation | Integrated bleed and engine controller |
US9209721B2 (en) * | 2014-04-29 | 2015-12-08 | The Boeing Company | Systems and methods for the control and operation of a parallel motor controller architecture |
DE102014218823A1 (de) * | 2014-09-18 | 2016-03-24 | Siemens Aktiengesellschaft | Netzknoten, Steuermodul für eine Komponente und Ethernet Ring |
EP3645391A1 (fr) * | 2017-06-30 | 2020-05-06 | A^3 By Airbus LLC | Systèmes électriques tolérants aux défaillances pour aéronef |
-
2019
- 2019-12-09 FR FR1913943A patent/FR3104347B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3104347A1 (fr) | 2021-06-11 |
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Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20210611 |
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Year of fee payment: 3 |
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Year of fee payment: 5 |