BR112015007372A2 - método de vigilância de um defeito de impulso de um turborreator de aeronave - Google Patents
método de vigilância de um defeito de impulso de um turborreator de aeronaveInfo
- Publication number
- BR112015007372A2 BR112015007372A2 BR112015007372A BR112015007372A BR112015007372A2 BR 112015007372 A2 BR112015007372 A2 BR 112015007372A2 BR 112015007372 A BR112015007372 A BR 112015007372A BR 112015007372 A BR112015007372 A BR 112015007372A BR 112015007372 A2 BR112015007372 A2 BR 112015007372A2
- Authority
- BR
- Brazil
- Prior art keywords
- impulse
- pulse
- modeled
- nmod
- instruction
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 5
- 230000007547 defect Effects 0.000 title 1
- 238000012544 monitoring process Methods 0.000 abstract 2
- 230000001052 transient effect Effects 0.000 abstract 2
- 238000001914 filtration Methods 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/14—Testing gas-turbine engines or jet-propulsion engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/13—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the tractive or propulsive power of vehicles
- G01L5/133—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the tractive or propulsive power of vehicles for measuring thrust of propulsive devices, e.g. of propellers
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
-
- 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
-
- 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
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
-
- 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
- F05D2260/81—Modelling or simulation
-
- 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
- F05D2260/82—Forecasts
- F05D2260/821—Parameter estimation or prediction
-
- 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
- F05D2270/335—Output power or torque
-
- 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
- F05D2270/44—Type of control system active, predictive, or anticipative
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Ocean & Marine Engineering (AREA)
- Control Of Turbines (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Testing Electric Properties And Detecting Electric Faults (AREA)
Abstract
1/1 resumo método de vigilância de um defeito de impulso de um turborreator de aeronave um método de vigilância de um defeito de impulso de um turborreator por ocasião de uma modificação da instrução de impulso (n1cons) do dito turborreator, método que compreende uma etapa de tratamento da instrução de impulso (ncons) com o auxílio de uma função de filtragem e de um modelo de fase transitória de maneira a obter um impulso modelado (nmod), uma etapa de comparação do dito impulso modelado (nmod) com o impulso efetivo (neff) de maneira a determinar uma diferença de impulso (d), uma etapa de comparação da dita diferença de impulso (d) com um limite de alarme (s); e uma etapa de emissão de um alarme em caso de ultrapassagem do dito limite de alarme (s), método no qual a uma iteração dada, um impulso modelado anterior sendo conhecido, o modelo de fase transitória fornece uma constante de tempo a partir do impulso modelado anterior, a função de filtragem fornece um impulso modelado (nmod) a partir da constante de tempo obtida, do impulso modelado anterior e da instrução de impulso (ncons).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1259367A FR2996254B1 (fr) | 2012-10-03 | 2012-10-03 | Methode de surveillance d'un defaut de poussee d'un turboreacteur d'aeronef |
FR1259367 | 2012-10-03 | ||
PCT/FR2013/052307 WO2014053752A1 (fr) | 2012-10-03 | 2013-09-27 | Methode de surveillance d'un defaut de poussee d'un turboreacteur d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112015007372A2 true BR112015007372A2 (pt) | 2017-07-04 |
BR112015007372B1 BR112015007372B1 (pt) | 2022-01-18 |
Family
ID=47295040
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015007372-7A BR112015007372B1 (pt) | 2012-10-03 | 2013-09-27 | Método de vigilância de um defeito de impulso de um turborreator de aeronave |
Country Status (8)
Country | Link |
---|---|
US (1) | US9897517B2 (pt) |
EP (1) | EP2917537B1 (pt) |
CN (1) | CN104736819B (pt) |
BR (1) | BR112015007372B1 (pt) |
CA (1) | CA2886401C (pt) |
FR (1) | FR2996254B1 (pt) |
RU (1) | RU2638417C2 (pt) |
WO (1) | WO2014053752A1 (pt) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9625886B1 (en) * | 2012-06-22 | 2017-04-18 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | Conditionally active min-max limit regulators |
FR2996474B1 (fr) | 2012-10-05 | 2014-12-12 | Snecma | Procede pour l'integration de materiau abradable dans un logement par compression isostatique |
FR3021701B1 (fr) * | 2014-05-27 | 2016-06-17 | Snecma | Procede et dispositif de controle d'une poussee d'un turboreacteur |
US10414512B2 (en) * | 2014-10-01 | 2019-09-17 | Sikorsky Aircraft Corporation | Power management between a propulsor and a coaxial rotor of a helicopter |
US10487752B2 (en) * | 2015-03-11 | 2019-11-26 | Pratt & Whitney Canada Corp. | Overthrust protection system and method |
US9932906B2 (en) * | 2015-09-23 | 2018-04-03 | Honeywell International Inc. | Gas turbine engine uncontrolled high thrust detection system and method |
FR3064602B1 (fr) * | 2017-03-29 | 2019-06-07 | Airbus Operations | Mode de fonctionnement degrade d'un groupe propulseur d'aeronef permettant le deplafonnement d'une consigne de poussee |
US10443512B2 (en) | 2017-03-31 | 2019-10-15 | Pratt & Whitney Canada Corp. | Detection of uncommanded and uncontrollable high thrust events |
US10302021B2 (en) | 2017-05-03 | 2019-05-28 | Pratt & Whitney Canada Corp. | Detection of uncommanded and uncontrollable high thrust events |
FR3065995B1 (fr) | 2017-05-05 | 2019-07-05 | Safran Aircraft Engines | Systeme et procede de surveillance d'une turbomachine a detection d'anomalie corrigee par un facteur d'usure |
US10155578B1 (en) * | 2017-08-16 | 2018-12-18 | Brunswick Corporation | Method and system for controlling a marine drive during shift sensor fault |
US10823113B2 (en) | 2017-08-21 | 2020-11-03 | Pratt & Whitney Canada Corp. | Method and system for limiting power of an engine |
FR3076361B1 (fr) * | 2018-01-04 | 2019-12-13 | Safran Aircraft Engines | Procede de filtrage adaptatif |
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 |
CN112943453A (zh) * | 2021-01-21 | 2021-06-11 | 西北工业大学 | 气路部件故障下基于iga的发动机最大推力控制优化方法 |
CN113188799B (zh) * | 2021-04-27 | 2022-09-30 | 中国航空工业集团公司北京长城计量测试技术研究所 | 基于速度差极值法的航空发动机推力修正方法 |
US11674450B1 (en) * | 2021-12-13 | 2023-06-13 | Pratt & Whitney Canada Corp. | System and method for synthesizing engine thrust |
CN116773138B (zh) * | 2023-08-23 | 2023-12-19 | 国科大杭州高等研究院 | 冷气微推力响应时间测量系统及方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3691356A (en) * | 1970-12-10 | 1972-09-12 | Sperry Rand Corp | Speed command and throttle control system for aircraft |
US4294069A (en) * | 1978-04-26 | 1981-10-13 | United Technologies Corporation | Exhaust nozzle control and core engine fuel control for turbofan engine |
US4242864A (en) * | 1978-05-25 | 1981-01-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Integrated control system for a gas turbine engine |
US4809500A (en) * | 1987-02-03 | 1989-03-07 | United Technologies Corporation | Transient control system for gas turbine engine |
US6487490B1 (en) * | 1999-05-26 | 2002-11-26 | General Electric Company | Speed modification system for gas turbine engine to allow trimming of excess |
US6823675B2 (en) | 2002-11-13 | 2004-11-30 | General Electric Company | Adaptive model-based control systems and methods for controlling a gas turbine |
US20060212281A1 (en) * | 2005-03-21 | 2006-09-21 | Mathews Harry Kirk Jr | System and method for system-specific analysis of turbomachinery |
FR2922959B1 (fr) * | 2007-10-31 | 2009-12-04 | Airbus France | Systeme de controle et procede de controle. |
-
2012
- 2012-10-03 FR FR1259367A patent/FR2996254B1/fr active Active
-
2013
- 2013-09-27 EP EP13782763.0A patent/EP2917537B1/fr active Active
- 2013-09-27 US US14/432,878 patent/US9897517B2/en active Active
- 2013-09-27 WO PCT/FR2013/052307 patent/WO2014053752A1/fr active Application Filing
- 2013-09-27 CA CA2886401A patent/CA2886401C/fr active Active
- 2013-09-27 CN CN201380054528.0A patent/CN104736819B/zh active Active
- 2013-09-27 BR BR112015007372-7A patent/BR112015007372B1/pt active IP Right Grant
- 2013-09-27 RU RU2015114593A patent/RU2638417C2/ru active
Also Published As
Publication number | Publication date |
---|---|
BR112015007372B1 (pt) | 2022-01-18 |
FR2996254B1 (fr) | 2014-09-12 |
WO2014053752A1 (fr) | 2014-04-10 |
RU2015114593A (ru) | 2016-11-27 |
CN104736819B (zh) | 2017-07-25 |
US20150219528A1 (en) | 2015-08-06 |
US9897517B2 (en) | 2018-02-20 |
EP2917537A1 (fr) | 2015-09-16 |
CA2886401C (fr) | 2020-01-28 |
FR2996254A1 (fr) | 2014-04-04 |
RU2638417C2 (ru) | 2017-12-13 |
CN104736819A (zh) | 2015-06-24 |
EP2917537B1 (fr) | 2018-08-01 |
CA2886401A1 (fr) | 2014-04-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 27/09/2013, OBSERVADAS AS CONDICOES LEGAIS. |