AT515626A3 - Notlaufmodus für einen Kolbenmotor in einem Flugzeug - Google Patents
Notlaufmodus für einen Kolbenmotor in einem Flugzeug Download PDFInfo
- Publication number
- AT515626A3 AT515626A3 ATA50163/2015A AT501632015A AT515626A3 AT 515626 A3 AT515626 A3 AT 515626A3 AT 501632015 A AT501632015 A AT 501632015A AT 515626 A3 AT515626 A3 AT 515626A3
- Authority
- AT
- Austria
- Prior art keywords
- piston engine
- emergency mode
- aircraft
- sensors
- relates
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/22—Safety or indicating devices for abnormal conditions
- F02D41/222—Safety or indicating devices for abnormal conditions relating to the failure of sensors or parameter detection devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
- F02D29/02—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving vehicles; peculiar to engines driving variable pitch propellers
-
- 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
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/22—Safety or indicating devices for abnormal conditions
- F02D2041/227—Limping Home, i.e. taking specific engine control measures at abnormal conditions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/22—Safety or indicating devices for abnormal conditions
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
Die vorliegende Erfindung betrifft ein Verfahren zum Betrieb eines Kolbenmotors (23) in einem Flugzeug {201) in einem Notlaufmodus,bei dem eine Mindestleistungsabgabe des Kolbenmotors {23) dadurch sichergestellt wird,dass ein von Messwerten jeweiliger für einen Betrieb des Kolbenmotors (23) vorgesehener Sensoren weitestgehend unabhängiger Notlaufmodus aktiviert wird, bei dem die Messwerte der Sensoren durch fest vorgegebene Werte ersetzt werden. Ferner betrifft die vorliegende Erfindung ein entsprechendes Flugzeug (201) sowie ein Notlaufsteuergerät (21) zur Durchführung des vorgestellten Verfahrens.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102014204115.5A DE102014204115A1 (de) | 2014-03-06 | 2014-03-06 | Notlaufmodus für einen Kolbenmotor in einem Flugzeug |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| AT515626A2 AT515626A2 (de) | 2015-10-15 |
| AT515626A3 true AT515626A3 (de) | 2019-05-15 |
| AT515626B1 AT515626B1 (de) | 2019-08-15 |
Family
ID=53883973
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ATA50163/2015A AT515626B1 (de) | 2014-03-06 | 2015-03-03 | Notlaufmodus für einen Kolbenmotor in einem Flugzeug |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20150252740A1 (de) |
| CN (1) | CN104890886B (de) |
| AT (1) | AT515626B1 (de) |
| DE (1) | DE102014204115A1 (de) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102019112387B4 (de) * | 2019-05-13 | 2022-10-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung und Verfahren zur Leistungssteuerung von Luftfahrzeugtriebwerken |
| US20240425187A1 (en) * | 2023-06-23 | 2024-12-26 | Pratt & Whitney Canada Corp. | Method and system for mitigating an electric motor fault in an aircraft power plant |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4509480A (en) * | 1983-01-20 | 1985-04-09 | Robert Bosch Gmbh | Safety arrangement for an internal combustion engine |
| US4780826A (en) * | 1985-07-23 | 1988-10-25 | Toyota Jidosha Kabushiki Kaisha | Failure judgment system for sensors installed in engine |
| US5233958A (en) * | 1990-11-16 | 1993-08-10 | Robert Bosch Gmbh | Arrangement for the open-loop and/or closed-loop control of an operating variable of an internal combustion engine |
| DE102006040337A1 (de) * | 2006-08-29 | 2008-03-06 | Robert Bosch Gmbh | Verfahren zum Betreiben einer Brennkraftmaschine |
| DE102009051390A1 (de) * | 2009-10-30 | 2011-05-05 | Mtu Friedrichshafen Gmbh | Verfahren zur Steuerung und Regelung einer Brennkraftmaschine |
| US20120191273A1 (en) * | 2009-08-11 | 2012-07-26 | Aeromechanical Services Ltd. | aircraft flight data delivery and management system with emergency mode |
| US20140303871A1 (en) * | 2011-11-25 | 2014-10-09 | Turbomeca | Method and system for regulating power in the event of at least one aircraft engine failure |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6539290B1 (en) * | 1995-06-07 | 2003-03-25 | Dabulamanzi Holdings, Llc | Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation |
| US5796922A (en) * | 1996-03-29 | 1998-08-18 | Weber State University | Trainable, state-sampled, network controller |
| CA2273932A1 (en) * | 1996-12-05 | 1998-06-11 | Shabbir Ahmed Parvez | Autonomous guidance system with position and velocity feedback using modern control theory |
| US6729139B2 (en) * | 2001-09-26 | 2004-05-04 | Goodrich Pump & Engine Control Systems, Inc. | Engine control system |
| US7277764B2 (en) * | 2002-12-09 | 2007-10-02 | Georgia Tech Research Corporation | Adaptive output feedback apparatuses and methods capable of controlling a non-minimum phase system |
| US7343232B2 (en) * | 2003-06-20 | 2008-03-11 | Geneva Aerospace | Vehicle control system including related methods and components |
| US7826954B2 (en) * | 2004-06-25 | 2010-11-02 | Honda Motor Co., Ltd. | System for monitoring sensor outputs of a gas turbine engine |
| US8948936B2 (en) * | 2004-11-08 | 2015-02-03 | Textron Innovations Inc. | Vehicle management system using finite state machines |
| US20070050100A1 (en) * | 2005-06-08 | 2007-03-01 | Gustafson Eric S | Auto-control override system for aircraft |
| FR2890645B1 (fr) * | 2005-09-13 | 2007-10-12 | Airbus France Sas | Dispositif de protection d'energie pour un avion. |
| US8588996B2 (en) * | 2005-11-09 | 2013-11-19 | Textron Innovations Inc. | Aircraft occupant protection system |
| US7551989B2 (en) * | 2006-06-21 | 2009-06-23 | Calspan Corporation | Autonomous outer loop control of man-rated fly-by-wire aircraft |
| US8131406B2 (en) * | 2008-04-09 | 2012-03-06 | Lycoming Engines, A Division Of Avco Corporation | Piston engine aircraft automated pre-flight testing |
| DE102008024955B3 (de) * | 2008-05-23 | 2009-12-24 | Continental Automotive Gmbh | Verfahren zur Erkennung einer Fehlfunktion eines Raildrucksensors bei einem Common Rail-Einspritzsystem |
| FR2933211B1 (fr) * | 2008-06-26 | 2010-11-26 | Airbus France | Dispositif d'interaction avec un systeme d'affichage, notamment pour un systeme d'affichage avionique |
| FR2946016B1 (fr) * | 2009-05-29 | 2012-09-28 | Airbus France | Systeme pour la commande d'au moins un moteur d'aeronef et aeronef comportant un tel systeme de commande. |
| DE102009050469B4 (de) * | 2009-10-23 | 2015-11-05 | Mtu Friedrichshafen Gmbh | Verfahren zur Steuerung und Regelung einer Brennkraftmaschine |
| DE102009050467B4 (de) * | 2009-10-23 | 2017-04-06 | Mtu Friedrichshafen Gmbh | Verfahren zur Steuerung und Regelung einer Brennkraftmaschine |
| US9132915B2 (en) * | 2010-05-07 | 2015-09-15 | Ohio Univeristy | Multi-modal vehicle |
| FR2963120B1 (fr) * | 2010-07-20 | 2013-08-30 | Airbus Operations Sas | Procede et dispositif de gestion automatique d'une trajectoire laterale pour une descente d'urgence d'un aeronef |
| US8311687B2 (en) * | 2010-07-30 | 2012-11-13 | Ge Aviation Systems Llc | Method and system for vertical navigation using time-of-arrival control |
| WO2012061763A2 (en) * | 2010-11-05 | 2012-05-10 | Bsst Llc | Energy management systems and methods with thermoelectric generators |
| DE102013208697A1 (de) * | 2013-05-13 | 2014-11-13 | Robert Bosch Gmbh | Verfahren zum Betreiben eines Benzinmotors mit vollständig offener Drosselklappe und Benzinmotor |
| US9142064B2 (en) * | 2013-08-07 | 2015-09-22 | Zf Friedrichshafen Ag | System for detecting vehicle driving mode and method of conducting the same |
-
2014
- 2014-03-06 DE DE102014204115.5A patent/DE102014204115A1/de not_active Ceased
-
2015
- 2015-03-03 AT ATA50163/2015A patent/AT515626B1/de not_active IP Right Cessation
- 2015-03-05 CN CN201510099007.8A patent/CN104890886B/zh not_active Expired - Fee Related
- 2015-03-06 US US14/640,723 patent/US20150252740A1/en not_active Abandoned
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4509480A (en) * | 1983-01-20 | 1985-04-09 | Robert Bosch Gmbh | Safety arrangement for an internal combustion engine |
| US4780826A (en) * | 1985-07-23 | 1988-10-25 | Toyota Jidosha Kabushiki Kaisha | Failure judgment system for sensors installed in engine |
| US5233958A (en) * | 1990-11-16 | 1993-08-10 | Robert Bosch Gmbh | Arrangement for the open-loop and/or closed-loop control of an operating variable of an internal combustion engine |
| DE102006040337A1 (de) * | 2006-08-29 | 2008-03-06 | Robert Bosch Gmbh | Verfahren zum Betreiben einer Brennkraftmaschine |
| US20120191273A1 (en) * | 2009-08-11 | 2012-07-26 | Aeromechanical Services Ltd. | aircraft flight data delivery and management system with emergency mode |
| DE102009051390A1 (de) * | 2009-10-30 | 2011-05-05 | Mtu Friedrichshafen Gmbh | Verfahren zur Steuerung und Regelung einer Brennkraftmaschine |
| US20140303871A1 (en) * | 2011-11-25 | 2014-10-09 | Turbomeca | Method and system for regulating power in the event of at least one aircraft engine failure |
Also Published As
| Publication number | Publication date |
|---|---|
| AT515626A2 (de) | 2015-10-15 |
| DE102014204115A1 (de) | 2015-09-10 |
| CN104890886B (zh) | 2020-02-18 |
| US20150252740A1 (en) | 2015-09-10 |
| CN104890886A (zh) | 2015-09-09 |
| AT515626B1 (de) | 2019-08-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM01 | Lapse because of not paying annual fees |
Effective date: 20240303 |