FR3065443B1 - Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee - Google Patents

Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee Download PDF

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Publication number
FR3065443B1
FR3065443B1 FR1753376A FR1753376A FR3065443B1 FR 3065443 B1 FR3065443 B1 FR 3065443B1 FR 1753376 A FR1753376 A FR 1753376A FR 1753376 A FR1753376 A FR 1753376A FR 3065443 B1 FR3065443 B1 FR 3065443B1
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FR
France
Prior art keywords
propulsion system
aircraft
distributed propulsion
dissymetry
management
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
FR1753376A
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English (en)
Other versions
FR3065443A1 (fr
Inventor
Emmanuel Joubert
Laurent Juve
Clement Veillerot
Thibault Baldivia
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Priority to FR1753376A priority Critical patent/FR3065443B1/fr
Priority to CN201810343997.9A priority patent/CN108725803B/zh
Priority to US15/955,264 priority patent/US10513342B2/en
Publication of FR3065443A1 publication Critical patent/FR3065443A1/fr
Application granted granted Critical
Publication of FR3065443B1 publication Critical patent/FR3065443B1/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
    • B64D31/09—Initiating means actuated automatically in response to power plant failure
    • B64D31/10—Initiating means actuated automatically in response to power plant failure for preventing asymmetric thrust
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • 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
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Physics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Retarders (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Transmission Devices (AREA)
  • Safety Devices In Control Systems (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

Méthode pour la gestion des poussées dissymétriques causées par des pannes moteur au sein d'un aéronef muni d'un système de propulsion distribuée, ledit système de propulsion distribuée comportant 2N groupes motopropulseurs (PTi), avec N entier strictement positif et i entier compris entre 1 et 2N inclus, répartis symétriquement par rapport à un plan de symétrie dudit aéronef, suivant laquelle la puissance d'au moins un groupe motopropulseur appartenant à un premier côté dudit plan de symétrie est diminuée lorsqu'une panne survient dans un groupe motopropulseur appartenant au côté opposé, de sorte que la somme des moments des poussées générées par lesdits groupes motopropulseurs par rapport au centre de gravité dudit aéronef est nulle, à des tolérances réglementaires près.
FR1753376A 2017-04-19 2017-04-19 Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee Active FR3065443B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1753376A FR3065443B1 (fr) 2017-04-19 2017-04-19 Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee
CN201810343997.9A CN108725803B (zh) 2017-04-19 2018-04-17 管理分布式推进系统中不平衡的方法
US15/955,264 US10513342B2 (en) 2017-04-19 2018-04-17 Method for managing imbalance in a distributed propulsion system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1753376 2017-04-19
FR1753376A FR3065443B1 (fr) 2017-04-19 2017-04-19 Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee

Publications (2)

Publication Number Publication Date
FR3065443A1 FR3065443A1 (fr) 2018-10-26
FR3065443B1 true FR3065443B1 (fr) 2021-01-01

Family

ID=59070887

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1753376A Active FR3065443B1 (fr) 2017-04-19 2017-04-19 Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee

Country Status (3)

Country Link
US (1) US10513342B2 (fr)
CN (1) CN108725803B (fr)
FR (1) FR3065443B1 (fr)

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US10737798B2 (en) * 2016-09-12 2020-08-11 Ansel Misfeldt Integrated feedback to flight controller
US10101719B1 (en) * 2017-12-12 2018-10-16 Kitty Hawk Corporation Aircraft control system based on sparse set of simulation data
IL262426B2 (en) * 2018-10-14 2024-08-01 Israel Aerospace Ind Ltd Systems and methods for controlling aircraft engines
CN109653885B (zh) * 2018-11-05 2020-10-20 中国航空工业集团公司西安飞机设计研究所 一种发动机实际转速均值配平方法及其控制系统
DE102018219179B3 (de) * 2018-11-09 2019-12-05 Siemens Aktiengesellschaft Böenlastminderung bei einem Flugzeug
CN109799826B (zh) * 2019-02-20 2022-02-25 上海振华重工(集团)股份有限公司 船舶推进器系统的推力分配方法
DE102019205152A1 (de) 2019-04-10 2020-10-15 Rolls-Royce Deutschland Ltd & Co Kg Elektrisches Antriebssystem für ein Flugzeug mit minimalem Giermoment
CN110254731B (zh) * 2019-06-25 2020-12-25 辽宁壮龙无人机科技有限公司 一种基于六旋翼飞行器的断桨保护方法及装置
CN110861786B (zh) * 2019-11-06 2021-05-11 上海卫星工程研究所 航天器推力器喷气控制安全诊断方法、系统、装置及介质
CN111237062B (zh) * 2020-01-16 2021-08-17 中国商用飞机有限责任公司 一种实现发动机自动起飞推力控制功能的系统及方法
IT202000010369A1 (it) 2020-05-08 2021-11-08 Milano Politecnico Velivolo plurimotore simulante un monomotore via hardware e software
CN112947530A (zh) * 2021-03-25 2021-06-11 西安交通大学 一种分布式电推进飞机偏航的控制方法及系统
CN113086243B (zh) * 2021-04-20 2022-08-02 中国直升机设计研究所 一种直升机全机质量体惯性载荷的分配方法
US11745886B2 (en) * 2021-06-29 2023-09-05 Beta Air, Llc Electric aircraft for generating a yaw force
US11592791B1 (en) * 2021-09-14 2023-02-28 Beta Air, Llc Systems and methods for flight control system using simulator data
US11427305B1 (en) 2021-09-16 2022-08-30 Beta Air, Llc Methods and systems for flight control for managing actuators for an electric aircraft
CN113985916B (zh) * 2021-10-26 2024-04-05 西安电子科技大学 基于压强闭环控制的飞行器变推力发动机控制分配方法、系统、装置及存储介质

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FR1090772A (fr) * 1952-10-20 1955-04-04 Power Jets Res & Dev Ltd Perfectionnements apportés aux avions propulsés par réaction
DE1151178B (de) * 1961-10-07 1963-07-04 Dornier Werke Gmbh Senkrecht startendes und landendes Flugzeug mit Axialstrahltriebwerken an den Fluegelenden
US4884205A (en) * 1987-08-04 1989-11-28 Hernandez Diaz Jorge H Method and apparatus for limiting adverse yaw-induced roll during engine failure in multiengine aircraft
FR2753171B1 (fr) * 1996-09-09 1998-11-13 Aerospatiale Dispositif de controle de la poussee d'un aeronef a plusieurs moteurs
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Also Published As

Publication number Publication date
US10513342B2 (en) 2019-12-24
US20180305033A1 (en) 2018-10-25
CN108725803A (zh) 2018-11-02
FR3065443A1 (fr) 2018-10-26
CN108725803B (zh) 2023-06-13

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