ES2571878T3 - Procedimiento y sistema de regulación de potencia en caso de fallo de al menos un motor de aeronave - Google Patents
Procedimiento y sistema de regulación de potencia en caso de fallo de al menos un motor de aeronaveInfo
- Publication number
- ES2571878T3 ES2571878T3 ES12806565T ES12806565T ES2571878T3 ES 2571878 T3 ES2571878 T3 ES 2571878T3 ES 12806565 T ES12806565 T ES 12806565T ES 12806565 T ES12806565 T ES 12806565T ES 2571878 T3 ES2571878 T3 ES 2571878T3
- Authority
- ES
- Spain
- Prior art keywords
- emergency
- power
- regime
- gpp
- propulsive
- 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
- 238000000034 method Methods 0.000 title abstract 3
- GVVPGTZRZFNKDS-JXMROGBWSA-N geranyl diphosphate Chemical compound CC(C)=CCC\C(C)=C\CO[P@](O)(=O)OP(O)(O)=O GVVPGTZRZFNKDS-JXMROGBWSA-N 0.000 abstract 6
- 230000001141 propulsive effect Effects 0.000 abstract 5
- 230000003213 activating effect Effects 0.000 abstract 1
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 238000000605 extraction Methods 0.000 abstract 1
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
-
- 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
-
- 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
-
- 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
- B64D41/00—Power installations for auxiliary purposes
-
- 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
- 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
-
- 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
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Stand-By Power Supply Arrangements (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
Procedimiento de regulación de potencia en caso de fallo de al menos un motor (M1, M2) de una aeronave que incluye una unidad de proceso digital de datos central (100) que suministra una función de emergencia apta para activar una señal de emergencia (S), caracterizado por que el procedimiento consiste, con el concurso de un grupo de potencia principal de clase motor llamado GPP (700) que, administrado por una función de control y de supervisión, funciona permanentemente en vuelo asumiendo una parte (PGA) de la potencia no propulsiva total nominal (PTA) de la aeronave, en incrementar sus límites de funcionamiento, ante la recepción de la señal de emergencia (S), para poder proporcionar, de manera prácticamente instantánea, potencias no propulsivas (PSU, PMU, PIU) aumentadas según al menos tres regímenes de emergencia (RS, RM, RI) en el momento de dicho fallo de motor como respuesta a consumos suplementarios extraídos del GPP (700), disponiendo cada régimen de emergencia de un espacio máximo de tiempo de intervención transferible de un régimen a otro y con posibilidad de ser repartido en varias secuencias alternadas, por que estos regímenes comprenden al menos, clasificados según un orden de nivel de potencia decreciente, un régimen llamado de superemergencia (RS), de asunción de la totalidad o parte de la potencia no propulsiva con un aumento añadido de potencia para intentar el rearranque del motor (M1, M2) defectuoso, un régimen llamado de emergencia máxima (RM), de asunción de la totalidad o parte de la potencia no propulsiva, y un régimen llamado intermedio de emergencia (RI), de asunción de una fracción mínima de potencia no propulsiva correspondiente al resto de potencia disponible de modo continuo hasta el final del vuelo, por que la función de control y supervisión del GPP (700) cuenta el tiempo transcurrido para cada régimen de emergencia (RS, RM, RI), informa de ello a la unidad de proceso central (100) en conjunción con una emisión de alerta en caso de rebasamiento de los espacios máximos de tiempo de funcionamiento (xmax, ymax, zmax) atribuidos a cada régimen de emergencia (RS, RM, RI), y por que la función de emergencia ajusta las extracciones de potencia no propulsiva de la aeronave entre los motores principales (M1, M2) y el grupo GPP (700), bien sea automáticamente, o bien mediante una orden del piloto, en función de esas informaciones de tiempo de régimen transcurrido y de aviso de rebasamiento de límite de utilización de un régimen de emergencia.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1160785A FR2983319B1 (fr) | 2011-11-25 | 2011-11-25 | Procede et systeme de regulation de puissance en cas de defaillance d'au moins un moteur d'aeronef |
| PCT/FR2012/052715 WO2013076434A2 (fr) | 2011-11-25 | 2012-11-23 | Procédé et système de régulation de puissance en cas de défaillance d'au moins un moteur d'aéronef |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2571878T3 true ES2571878T3 (es) | 2016-05-27 |
Family
ID=47436062
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES12806565T Active ES2571878T3 (es) | 2011-11-25 | 2012-11-23 | Procedimiento y sistema de regulación de potencia en caso de fallo de al menos un motor de aeronave |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US9315274B2 (es) |
| EP (1) | EP2782832B1 (es) |
| JP (1) | JP6124913B2 (es) |
| KR (1) | KR102019527B1 (es) |
| CN (1) | CN103930347B (es) |
| CA (1) | CA2853195C (es) |
| ES (1) | ES2571878T3 (es) |
| FR (1) | FR2983319B1 (es) |
| PL (1) | PL2782832T3 (es) |
| RU (1) | RU2608784C2 (es) |
| WO (1) | WO2013076434A2 (es) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3015574B1 (fr) * | 2013-12-20 | 2019-05-03 | Safran Helicopter Engines | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
| DE102014204115A1 (de) * | 2014-03-06 | 2015-09-10 | Robert Bosch Gmbh | Notlaufmodus für einen Kolbenmotor in einem Flugzeug |
| US10094293B2 (en) * | 2014-08-22 | 2018-10-09 | Pratt & Whitney Canada Corp. | In flight restart system and method for free turbine engine |
| FR3025617B1 (fr) * | 2014-09-05 | 2016-12-16 | Sagem Defense Securite | Architecture bi-voies |
| FR3028839B1 (fr) | 2014-11-26 | 2016-11-18 | Airbus Helicopters | Methode d'assistance a la navigation d'un giravion multimoteur en cas de panne moteur, dans le cadre d'un entrainement a vitesse variable d'un rotor principal du giravion |
| PT3224142T (pt) * | 2015-07-16 | 2018-09-28 | Guinault S A | Unidade inteligente para assistência de aeronaves no solo |
| GB2542921B (en) | 2015-09-02 | 2019-05-29 | Bae Systems Plc | Vehicle power sharing system with engine-driven generator and fuel cell |
| WO2017037434A1 (en) * | 2015-09-02 | 2017-03-09 | Bae Systems Plc | A vehicle comprising an engine restart system |
| CN106586002B (zh) * | 2016-11-30 | 2018-12-11 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机与发动机一体化匹配调节控制方法 |
| CN106704009B (zh) * | 2016-12-13 | 2019-10-11 | 安徽航瑞航空动力装备有限公司 | 一种活塞式航空发动机负荷协调控制方法 |
| FR3065443B1 (fr) * | 2017-04-19 | 2021-01-01 | Airbus Group Sas | Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee |
| US10513341B2 (en) * | 2018-04-27 | 2019-12-24 | Wing Aviation Llc | Thrust allocation for aerial vehicle |
| US10775784B2 (en) * | 2018-06-14 | 2020-09-15 | Wing Aviation Llc | Unmanned aerial vehicle with decentralized control system |
| EP3725676A1 (en) * | 2019-04-16 | 2020-10-21 | Volocopter GmbH | Method of controlling an actuator system, emergency control system and aircraft equipped with such system |
| US11561873B2 (en) | 2019-09-26 | 2023-01-24 | General Electric Company | Test equipment interface add-on having a production support equipment module and a selectively removable test support equipment module |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4684081A (en) * | 1986-06-11 | 1987-08-04 | Lockheed Corporation | Multifunction power system for an aircraft |
| US4912921A (en) * | 1988-03-14 | 1990-04-03 | Sundstrand Corporation | Low speed spool emergency power extraction system |
| US5161363A (en) * | 1989-09-21 | 1992-11-10 | Allied-Signal Inc. | Integrated power unit |
| US5235812A (en) * | 1989-09-21 | 1993-08-17 | Allied-Signal Inc. | Integrated power unit |
| US5343778A (en) * | 1992-11-09 | 1994-09-06 | Alliedsignal Inc. | Multifunction secondary power system |
| DE59710114D1 (de) * | 1996-10-25 | 2003-06-26 | Daimler Benz Aerospace Airbus | Leistungswandler-System zur bidirektionalen Wandlung zwischen hydraulischer und elektrischer Energie |
| US6316841B1 (en) * | 2000-01-21 | 2001-11-13 | Hamilton Sundstrand Corporation | Integrated emergency power and environmental control system |
| JP4537778B2 (ja) * | 2004-06-30 | 2010-09-08 | 株式会社ディスコ | ビトリファイドボンド砥石の目立て方法 |
| US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
| JP2007015423A (ja) * | 2005-07-05 | 2007-01-25 | Shin Meiwa Ind Co Ltd | 航空機の電源システム |
| FR2890645B1 (fr) * | 2005-09-13 | 2007-10-12 | Airbus France Sas | Dispositif de protection d'energie pour un avion. |
| US20100294877A1 (en) * | 2005-09-30 | 2010-11-25 | Laurentiu Jianu | VTOL lifting body flying automobile |
| US8340842B2 (en) * | 2005-12-19 | 2012-12-25 | Vertical Power, Inc. | Aircraft emergency handling |
| US8062081B2 (en) * | 2007-12-12 | 2011-11-22 | Foss Maritime Company, Inc. | Hybrid propulsion systems |
| ES2363897B1 (es) | 2008-10-24 | 2012-07-04 | Airbus Operations, S.L. | Unidad de potencia auxiliar (apu) de una aeronave |
| FR2951330B1 (fr) * | 2009-10-13 | 2013-03-08 | Messier Bugatti | Reseau de pilotage pour actionneurs mono ou multimoteurs, particulierement adapte a des applications aeronautiques telles que l'alimentation de moteurs de boitiers d'accrochage |
| FR2964087B1 (fr) * | 2010-08-25 | 2013-06-14 | Turbomeca | Procede d'optimisation de l'operabilite de motorisation d'un aeronef et groupe de puissance autonome de mise en oeuvre |
| US8820677B2 (en) * | 2011-06-18 | 2014-09-02 | Jason A. Houdek | Aircraft power systems and methods |
-
2011
- 2011-11-25 FR FR1160785A patent/FR2983319B1/fr not_active Expired - Fee Related
-
2012
- 2012-11-23 US US14/354,376 patent/US9315274B2/en not_active Expired - Fee Related
- 2012-11-23 RU RU2014118867A patent/RU2608784C2/ru active
- 2012-11-23 WO PCT/FR2012/052715 patent/WO2013076434A2/fr active Application Filing
- 2012-11-23 CN CN201280055399.2A patent/CN103930347B/zh not_active Expired - Fee Related
- 2012-11-23 CA CA2853195A patent/CA2853195C/fr active Active
- 2012-11-23 ES ES12806565T patent/ES2571878T3/es active Active
- 2012-11-23 EP EP12806565.3A patent/EP2782832B1/fr active Active
- 2012-11-23 KR KR1020147012551A patent/KR102019527B1/ko active IP Right Grant
- 2012-11-23 PL PL12806565T patent/PL2782832T3/pl unknown
- 2012-11-23 JP JP2014542920A patent/JP6124913B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US9315274B2 (en) | 2016-04-19 |
| RU2014118867A (ru) | 2015-12-27 |
| JP2014534122A (ja) | 2014-12-18 |
| WO2013076434A3 (fr) | 2013-12-05 |
| JP6124913B2 (ja) | 2017-05-10 |
| EP2782832A2 (fr) | 2014-10-01 |
| KR20150032513A (ko) | 2015-03-26 |
| CA2853195C (fr) | 2019-12-31 |
| CN103930347A (zh) | 2014-07-16 |
| EP2782832B1 (fr) | 2016-04-06 |
| KR102019527B1 (ko) | 2019-09-06 |
| CN103930347B (zh) | 2016-10-12 |
| US20140303871A1 (en) | 2014-10-09 |
| RU2608784C2 (ru) | 2017-01-24 |
| WO2013076434A2 (fr) | 2013-05-30 |
| FR2983319B1 (fr) | 2014-02-07 |
| CA2853195A1 (fr) | 2013-05-30 |
| PL2782832T3 (pl) | 2016-08-31 |
| FR2983319A1 (fr) | 2013-05-31 |
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