FR3029985B1 - Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre - Google Patents

Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre

Info

Publication number
FR3029985B1
FR3029985B1 FR1462234A FR1462234A FR3029985B1 FR 3029985 B1 FR3029985 B1 FR 3029985B1 FR 1462234 A FR1462234 A FR 1462234A FR 1462234 A FR1462234 A FR 1462234A FR 3029985 B1 FR3029985 B1 FR 3029985B1
Authority
FR
France
Prior art keywords
nozzle
controlling
flow rate
variable section
implementing
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
FR1462234A
Other languages
English (en)
Other versions
FR3029985A1 (fr
Inventor
Pierre Caruel
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 Nacelles SAS
Original Assignee
Aircelle SA
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 Aircelle SA filed Critical Aircelle SA
Priority to FR1462234A priority Critical patent/FR3029985B1/fr
Priority to PCT/FR2015/053460 priority patent/WO2016092239A1/fr
Priority to GB1710297.1A priority patent/GB2548061B/en
Publication of FR3029985A1 publication Critical patent/FR3029985A1/fr
Application granted granted Critical
Publication of FR3029985B1 publication Critical patent/FR3029985B1/fr
Priority to US15/619,858 priority patent/US10787995B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control
    • F02K1/17—Control or regulation conjointly with another control with control of fuel supply
    • 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
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/07—Purpose of the control system to improve fuel economy
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/114—Purpose of the control system to prolong engine life by limiting mechanical stresses
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/31—Fuel schedule for stage combustors
    • 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
    • F05D2270/70—Type of control algorithm
    • F05D2270/703—Type of control algorithm integral
    • 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
    • F05D2270/70—Type of control algorithm
    • F05D2270/708—Type of control algorithm with comparison tables
    • 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
    • F05D2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • F05D2270/821—Displacement measuring means, e.g. inductive

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Turbines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

L'invention concerne un dispositif (44) de contrôle d'une tuyère (32) d'éjection à section variable d'une nacelle (10) de turboréacteur (20) d'un aéronef, le dispositif (44) comportant un calculateur (46) adapté pour déterminer une consigne de position de la tuyère (32), caractérisé en ce qu'il comprend des moyens de gestion de l'asservissement de la position de la tuyère (32) variable en fonction du débit du carburant alimentant le turboréacteur (20), lesdits moyens de gestion comportant au moins un capteur de débit (48) instantané du carburant et une unité de gestion (50) qui est conçue pour comparer le débit mesuré par le capteur de débit (48) à un débit de carburant théorique en fonction des paramètres du vol de l'aéronef, déterminer une valeur de correction de la position de la tuyère (32) en fonction de la comparaison du débit mesuré et du débit théorique de carburant, et corriger la consigne de position de la tuyère (32) suivant la valeur de correction.
FR1462234A 2014-12-11 2014-12-11 Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre Active FR3029985B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1462234A FR3029985B1 (fr) 2014-12-11 2014-12-11 Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre
PCT/FR2015/053460 WO2016092239A1 (fr) 2014-12-11 2015-12-11 L'invention concerne un dispositif de contrôle d'une tuyère d'éjection à section variable d'une nacelle de turboréacteur d'un aéronef et un procédé de mise en œuvre d'un tel dispositif.
GB1710297.1A GB2548061B (en) 2014-12-11 2015-12-11 Control device of a variable section nozzle and the implementation method thereof
US15/619,858 US10787995B2 (en) 2014-12-11 2017-06-12 Control device of a variable section nozzle and the implementation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1462234A FR3029985B1 (fr) 2014-12-11 2014-12-11 Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre

Publications (2)

Publication Number Publication Date
FR3029985A1 FR3029985A1 (fr) 2016-06-17
FR3029985B1 true FR3029985B1 (fr) 2017-01-27

Family

ID=52469170

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1462234A Active FR3029985B1 (fr) 2014-12-11 2014-12-11 Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre

Country Status (4)

Country Link
US (1) US10787995B2 (fr)
FR (1) FR3029985B1 (fr)
GB (1) GB2548061B (fr)
WO (1) WO2016092239A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201811852D0 (en) 2018-07-20 2018-09-05 Rolls Royce Plc Supersonic aircraft turbofan
CN114542323B (zh) * 2021-12-29 2023-11-28 中国航空工业集团公司沈阳飞机设计研究所 一种矢量喷管的控制方法及装置

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3030771A (en) 1959-03-02 1962-04-24 United Aircraft Corp Turbo rocket fuel control system
US5303545A (en) * 1992-10-05 1994-04-19 United Technologies Corporation Pressure based close loop thrust control in a turbofan engine
US5893040A (en) * 1996-05-15 1999-04-06 The Boeing Company Method and apparatus for automatically providing jet engine thrust ratings to avionic systems
US6000215A (en) * 1997-12-23 1999-12-14 United Technologies Corporation Method of operating a gas turbine engine
FR2956163B1 (fr) * 2010-02-10 2012-02-17 Aircelle Sa Systeme de commande d'un aeronef
US8615982B2 (en) * 2011-07-05 2013-12-31 Hamilton Sundstrand Corporation Integrated electric variable area fan nozzle thrust reversal actuation system
GB2524776B (en) * 2014-04-02 2016-10-12 Rolls Royce Plc Aircraft vapour trail control system

Also Published As

Publication number Publication date
FR3029985A1 (fr) 2016-06-17
GB2548061B (en) 2020-07-08
US20170276092A1 (en) 2017-09-28
US10787995B2 (en) 2020-09-29
GB2548061A (en) 2017-09-06
GB201710297D0 (en) 2017-08-09
WO2016092239A1 (fr) 2016-06-16

Similar Documents

Publication Publication Date Title
EP2685068A3 (fr) Système de commande d'une turbine à gaz fournissant de la puissance à un aéronef
UA84280C2 (ru) Способ управления потоком воздуха в газовой турбине и система для осуществления данного способа
US20190195133A1 (en) Method and system for turbine engine temperature regulation
CA2854703A1 (fr) Systeme et methode de commande d'une eolienne
FR2983529B1 (fr) Methode de surveillance d’un dispositif de commande d’un doseur de carburant d’un turboreacteur
CN103946516A (zh) 阀控制装置、燃气涡轮机以及阀控制方法
JP2014159808A5 (fr)
RU2015142449A (ru) Способ и система управления кислородным датчиком регулируемого напряжения
FR3012421B1 (fr) Procede et dispositif d'inertage d'un reservoir de carburant
EP2239439A2 (fr) Méthode et système de réglage de la position d'une vanne de turbomachine
FR3065990B1 (fr) Procede de reactualisation d’une dynamique d’adaptation d’une valeur de richesse a une consigne dans un moteur
MA39551B1 (fr) Procédé de commande d'un dispositif de pompe
FR3029985B1 (fr) Dispositif de controle d’une tuyere a section variable et son procede de mise en œuvre
RU2017104901A (ru) Вторичные системы и способы управления для вентиляторных сопел с изменяемым сечением
US11667392B2 (en) Method and system for operating a rotorcraft engine
EP2559884A3 (fr) Système et procédé de fonctionnement d'une chambre de combustion
CA3060471A1 (fr) Optimisation des moteurs axee sur un debit de carburant eleve
FR3090730B1 (fr) Système et procédé de commande d’une vitesse de rotation d’une turbomachine d’aéronef avec gestion de panne
US20160355919A1 (en) Method and device for controlling amount of hot dip galvanization adhesion
FR3078551B1 (fr) Commande anticipative d'un circuit d'alimentation en carburant d'une turbomachine
FR3062425B1 (fr) Circuit d'alimentation en carburant de turbomachine
CN107061021B (zh) 一种发动机机械液压燃油流量辅助计量调节装置
RU2476703C1 (ru) Способ управления расходом топлива в основную камеру сгорания газотурбинного двигателя на приемистости
FR3018098B1 (fr) Systeme de regulation de l'alimentation de carburant dans une turbomachine d'helicoptere
KR20170066890A (ko) 엔진을 포함하는 선박

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20160617

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

CD Change of name or company name

Owner name: SAFRAN NACELLES, FR

Effective date: 20180125

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10