PL3607190T3 - Sposób sprawdzania maksymalnej dostępnej mocy maszyny wirowej statku powietrznego wyposażonego w dwie maszyny wirowe - Google Patents

Sposób sprawdzania maksymalnej dostępnej mocy maszyny wirowej statku powietrznego wyposażonego w dwie maszyny wirowe

Info

Publication number
PL3607190T3
PL3607190T3 PL18722116T PL18722116T PL3607190T3 PL 3607190 T3 PL3607190 T3 PL 3607190T3 PL 18722116 T PL18722116 T PL 18722116T PL 18722116 T PL18722116 T PL 18722116T PL 3607190 T3 PL3607190 T3 PL 3607190T3
Authority
PL
Poland
Prior art keywords
checking
available power
maximum available
turbine
aircraft equipped
Prior art date
Application number
PL18722116T
Other languages
English (en)
Inventor
Pierre DARFEUIL
Patrick Marconi
Caroline SEVE
Original Assignee
Safran Helicopter Engines
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 Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3607190T3 publication Critical patent/PL3607190T3/pl

Links

Classifications

    • 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
    • F02C9/26—Control of fuel supply
    • F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • 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
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • 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
    • F05D2260/00—Function
    • F05D2260/80—Diagnostics
    • 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
    • F05D2260/00—Function
    • F05D2260/83—Testing, e.g. methods, components or tools therefor
    • 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
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/053—Explicitly mentioned power
    • 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
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/093—Purpose of the control system to cope with emergencies of one engine in a multi-engine system

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
PL18722116T 2017-04-03 2018-03-30 Sposób sprawdzania maksymalnej dostępnej mocy maszyny wirowej statku powietrznego wyposażonego w dwie maszyny wirowe PL3607190T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1752849A FR3064680B1 (fr) 2017-04-03 2017-04-03 Procede de verification de la puissance maximale disponible d'une turbomachine d'un aeronef equipe de deux turbomachines
EP18722116.3A EP3607190B1 (fr) 2017-04-03 2018-03-30 Procédé de vérification de la puissance maximale disponible d'une turbomachine d'un aéronef équipé de deux turbomachines
PCT/FR2018/050802 WO2018185409A1 (fr) 2017-04-03 2018-03-30 Procédé de vérification de la puissance maximale disponible d'une turbomachine d'un aéronef équipé de deux turbomachines

Publications (1)

Publication Number Publication Date
PL3607190T3 true PL3607190T3 (pl) 2021-06-28

Family

ID=59381401

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18722116T PL3607190T3 (pl) 2017-04-03 2018-03-30 Sposób sprawdzania maksymalnej dostępnej mocy maszyny wirowej statku powietrznego wyposażonego w dwie maszyny wirowe

Country Status (7)

Country Link
US (1) US11459960B2 (pl)
EP (1) EP3607190B1 (pl)
CN (1) CN110621858B (pl)
CA (1) CA3058614A1 (pl)
FR (1) FR3064680B1 (pl)
PL (1) PL3607190T3 (pl)
WO (1) WO2018185409A1 (pl)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020107310A1 (zh) * 2018-11-29 2020-06-04 深圳市大疆创新科技有限公司 无人飞行器控制方法、控制装置及无人飞行器
WO2020158136A1 (ja) * 2019-02-01 2020-08-06 パナソニックＩｐマネジメント株式会社 無人飛行体、情報処理方法およびプログラム
US11391218B2 (en) * 2019-03-22 2022-07-19 Pratt & Whitney Canada Corp. Method and system for setting power of an aircraft engine
FR3095196B1 (fr) * 2019-04-17 2021-12-03 Airbus Helicopters Procédé et dispositif pour estimer la santé d’une installation motrice d’un aéronef pourvu d’au moins un moteur et d’un filtre colmatable filtrant de l’air en amont du moteur
US12078074B2 (en) * 2019-05-13 2024-09-03 Pratt & Whitney Canada Corp. System and method for detecting an uncommanded or uncontrollable high thrust event in an aircraft
US11667392B2 (en) * 2019-06-20 2023-06-06 Pratt & Whitney Canada Corp. Method and system for operating a rotorcraft engine
US12017784B2 (en) * 2019-10-09 2024-06-25 Beta Air, Llc In-flight stabilization of an aircraft
US12054239B2 (en) * 2019-10-09 2024-08-06 Beta Air, Llc In-flight stabilization of an aircraft
US11427353B2 (en) 2019-12-13 2022-08-30 Pratt & Whitney Canada Corp. System and method for testing engine performance in-flight
FR3129923B1 (fr) * 2021-12-07 2026-03-06 Safran Helicopter Engines Procédé de vérification de la puissance maximale disponible de différents organes d’une chaîne propulsive d’un aéronef.
US12392255B2 (en) * 2022-08-22 2025-08-19 Pratt & Whitney Canada Corp. Systems and methods for determining gas turbine engine operating margins
CN119460142B (zh) * 2024-10-15 2025-10-24 中国直升机设计研究所 一种通过试飞数据确定直升机飞行性能的方法

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU627952B2 (en) * 1989-12-11 1992-09-03 Westinghouse Electric Corporation Gas turbine control system having maximum instantaneous load pickup limiter
US6687596B2 (en) * 2001-08-31 2004-02-03 General Electric Company Diagnostic method and system for turbine engines
RU2306446C1 (ru) * 2005-11-25 2007-09-20 Открытое акционерное общество "Авиадвигатель" Способ управления силовой установкой самолета
FR2899640B1 (fr) * 2006-04-05 2011-11-25 Eurocopter France Procede et dispositif pour realiser un controle de l'etat de sante d'un turbomoteur d'un giravion bimoteur
FR2964154B1 (fr) * 2010-08-31 2012-08-10 Eurocopter France Procede et dispositif pour optimiser l'utilisation d'un moteur
FR2967132B1 (fr) * 2010-11-04 2012-11-09 Turbomeca Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre
FR2986649B1 (fr) 2012-02-06 2014-01-31 Eurocopter France Procede de simulation de panne sur un aeronef
FR2986505B1 (fr) * 2012-02-06 2015-06-26 Eurocopter France Procede d'optimisation de performances d'un aeronef, dispositif et aeronef
FR2986507B1 (fr) * 2012-02-06 2014-01-17 Eurocopter France Procede et dispositif pour realiser un controle de l'etat de sante d'un turbomoteur d'un aeronef pourvu d'au moins un turbomoteur
FR2986506B1 (fr) * 2012-02-06 2015-06-26 Eurocopter France Procede et dispositif pour realiser un controle de sante d'un turbomoteur d'un aeronef pourvu d'au moins un turbomoteur
FR2997382B1 (fr) * 2012-10-29 2014-11-21 Eurocopter France Procede de gestion d'une panne moteur sur un aeronef multimoteur muni d'une installation motrice hybride
EP2762852A1 (en) * 2013-02-05 2014-08-06 Siemens Aktiengesellschaft Automatic Testing System for a Gas Turbine
GB2515141B (en) * 2013-03-25 2015-10-21 Honeywell Int Inc Multi-engine performance margin synchronization adaptive control system and method
CN104515683A (zh) * 2013-09-30 2015-04-15 哈尔滨飞机工业集团有限责任公司 一种双发直升机的发动机功率裕度和热裕度检查方法
RU2551013C1 (ru) * 2013-11-07 2015-05-20 Открытое Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Оао "Умпо") Способ серийного производства газотурбинного двигателя и газотурбинный двигатель, выполненный этим способом
FR3015428B1 (fr) * 2013-12-20 2017-04-28 Eurocopter France Installation motrice disposant d'un moteur secondaire compensant les pertes de puissance des moteurs principaux pour un aeronef a voilure tournante
FR3019225B1 (fr) * 2014-03-27 2018-06-22 Safran Helicopter Engines Procede de detection d'une defaillance d'un premier turbomoteur d'un helicoptere bimoteur et de commande du second turbomoteur, et dispositif correspondant
BE1022512B1 (fr) * 2014-11-17 2016-05-18 Techspace Aero S.A. Banc d'essai pour turbomachine axiale avec eolienne verticale
US9784183B2 (en) * 2014-11-18 2017-10-10 General Electric Company Power outlet, emissions, fuel flow and water flow based probabilistic control in liquid-fueled gas turbine tuning, related control systems, computer program products and methods
FR3034403B1 (fr) * 2015-03-31 2017-03-31 Airbus Helicopters Procede et dispositif pour arreter un turbomoteur en fonctionnement nominal

Also Published As

Publication number Publication date
US20210108578A1 (en) 2021-04-15
CA3058614A1 (fr) 2018-10-11
EP3607190B1 (fr) 2021-02-17
CN110621858A (zh) 2019-12-27
US11459960B2 (en) 2022-10-04
FR3064680B1 (fr) 2019-04-05
CN110621858B (zh) 2022-02-08
EP3607190A1 (fr) 2020-02-12
WO2018185409A1 (fr) 2018-10-11
FR3064680A1 (fr) 2018-10-05

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