ES2091427T3 - Dispositivo de tratamiento de las informaciones relativas a las averias detectadas por una o varias unidades centrales de un aeronave. - Google Patents
Dispositivo de tratamiento de las informaciones relativas a las averias detectadas por una o varias unidades centrales de un aeronave.Info
- Publication number
- ES2091427T3 ES2091427T3 ES92403022T ES92403022T ES2091427T3 ES 2091427 T3 ES2091427 T3 ES 2091427T3 ES 92403022 T ES92403022 T ES 92403022T ES 92403022 T ES92403022 T ES 92403022T ES 2091427 T3 ES2091427 T3 ES 2091427T3
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- information relating
- treatment
- faults detected
- central units
- 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.)
- Expired - Lifetime
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
- G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
- G06F11/0706—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment
- G06F11/0736—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function
- G06F11/0739—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function in a data processing system embedded in automotive or aircraft systems
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
- G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
- G06F11/079—Root cause analysis, i.e. error or fault diagnosis
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Quality & Reliability (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Biomedical Technology (AREA)
- Test And Diagnosis Of Digital Computers (AREA)
- Techniques For Improving Reliability Of Storages (AREA)
- Navigation (AREA)
Abstract
DISPOSITIVO DE EXPLOTACION DE LAS INFORMACIONES RELATIVAS A LAS AVERIAS DETECTADAS POR UNA UNIDAD CENTRAL (2) DE UNA AERONAVE QUE ESTA CONECTADA POR UN BUS (4) DE DIRECCION Y DE DATOS A UNA PRIMERA MEMORIA (6) QUE MEMORIZA ESTAS INFORMACIONES, QUE COMPRENDE UNA SEGUNDA MEMORIA (7) NO VOLATIL, AMOVIBLE, CONECTABLE A DICHO BUS (4) Y EN LA QUE LAS INFORMACIONES CONTENIDAS EN LA PRIMERA MEMORIA (6) PUEDEN SER RECOPIADAS CON EL FIN DE TRATARLAS EN UN CENTRO DE CALCULO. IENTO DES LOS CALCULADORES DE AERONAVE
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9114381A FR2684211B1 (fr) | 1991-11-22 | 1991-11-22 | Dispositif d'exploitation des informations relatives aux pannes detectees par une ou plusieurs unites centrales d'un aeronef. |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2091427T3 true ES2091427T3 (es) | 1996-11-01 |
Family
ID=9419199
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES92403022T Expired - Lifetime ES2091427T3 (es) | 1991-11-22 | 1992-11-10 | Dispositivo de tratamiento de las informaciones relativas a las averias detectadas por una o varias unidades centrales de un aeronave. |
Country Status (5)
Country | Link |
---|---|
US (1) | US5500797A (es) |
EP (1) | EP0543698B1 (es) |
DE (1) | DE69212284T2 (es) |
ES (1) | ES2091427T3 (es) |
FR (1) | FR2684211B1 (es) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100194354B1 (ko) * | 1995-07-28 | 1999-06-15 | 전주범 | 안티 록 브레이크 시스템의 동작기록장치 |
DE19638973C2 (de) * | 1996-09-23 | 1998-07-23 | Siemens Ag | Elektronisches Steuergerät, insbesondere für eine in einem Kraftfahrzeug vorgesehene Einrichtung |
US6115656A (en) * | 1997-06-17 | 2000-09-05 | Mcdonnell Douglas Corporation | Fault recording and reporting method |
FR2764990B1 (fr) | 1997-06-23 | 1999-08-20 | Eurocopter France | Procede et dispositif de localisation de pannes et de dysfonctionnements d'un systeme complexe |
DE19841267C1 (de) * | 1998-09-09 | 2000-03-02 | Siemens Ag | Verfahren zur Durchführung einer Fehlerdiagnose und fahrzeugeigenes Fehlerdiagnosesystem |
US6397128B1 (en) * | 1998-12-30 | 2002-05-28 | Honeywell International Inc. | Flight data recorder system |
US6671593B2 (en) * | 1999-12-01 | 2003-12-30 | Sinex Holding Llc | Dynamic aircraft maintenance production system |
US7251550B2 (en) * | 2003-10-01 | 2007-07-31 | Honeywell International Inc. | Aircraft accessory monitor |
US20080114507A1 (en) * | 2006-11-10 | 2008-05-15 | Ruth Robert S | System and method for situational control of mobile platform maintenance and operation |
WO2008089796A2 (de) | 2007-01-24 | 2008-07-31 | Swiss Reinsurance Company | Computer-gestütztes, vollautomatisiertes alarm- und/oder interventionssystem für betriebsstörungen bei flugtransport- und/oder personenflugbeförderungsmittel, sowie entsprechendes verfahren |
US20090326782A1 (en) * | 2008-04-21 | 2009-12-31 | Honeywell International Inc. | Aircraft gas turbine engine controller with removable memory and diagnostic system and method therefor |
US9845734B2 (en) | 2011-04-20 | 2017-12-19 | Honeywell International Inc. | Air turbine start system with monopole starter air valve position |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1157961A (en) * | 1965-07-28 | 1969-07-09 | Epsylon Res & Dev Co Ltd | Magnetic Recording System for Aircraft |
US4258421A (en) * | 1978-02-27 | 1981-03-24 | Rockwell International Corporation | Vehicle monitoring and recording system |
US4409670A (en) * | 1981-06-26 | 1983-10-11 | United Technologies Corporation | Solid-state digital flight data recorder |
US4470116A (en) * | 1982-08-02 | 1984-09-04 | United Technologies Corporation | Digital flight data recording system |
US4656585A (en) * | 1984-02-03 | 1987-04-07 | Sundstrand Data Control Inc. | Aircraft flight data recorder data acquisition system |
US4642775A (en) * | 1984-05-25 | 1987-02-10 | Sundstrand Data Control, Inc. | Airborne flight planning and information system |
US4646241A (en) * | 1984-06-21 | 1987-02-24 | United Technologies Corporation | Solid-state flight data recording system |
US4729102A (en) * | 1984-10-24 | 1988-03-01 | Sundstrand Data Control, Inc. | Aircraft data acquisition and recording system |
CA1247743A (en) * | 1985-01-24 | 1988-12-28 | Izuru Morita | Operation data recording system |
JP2585592B2 (ja) * | 1987-05-13 | 1997-02-26 | 株式会社日立製作所 | 電子計算機調整方法 |
US4770116A (en) * | 1987-05-21 | 1988-09-13 | Xerox Corporation | Contact fuser apparatus with release agent management system |
US4970646A (en) * | 1987-11-12 | 1990-11-13 | Nissan Motor Co., Ltd. | Vehicle having secondarily steered front and rear wheels |
US5047977A (en) * | 1988-04-08 | 1991-09-10 | International Business Machines Corporation | Methods of generating and retrieving error and task message records within a multitasking computer system |
JP3028815B2 (ja) * | 1988-08-19 | 2000-04-04 | 株式会社東芝 | 携帯可能電子装置の伝送方法と携帯可能電子装置 |
US5185700A (en) * | 1989-06-15 | 1993-02-09 | Pulse Electronics, Inc. | Solid state event recorder |
US5065321A (en) * | 1989-06-15 | 1991-11-12 | Pulse Electronics, Inc. | Solid state event recorder |
US5239468A (en) * | 1990-12-07 | 1993-08-24 | United Technologies Corporation | Automated helicopter maintenance monitoring |
US5218547A (en) * | 1991-05-20 | 1993-06-08 | Tebbs Mark C | Universal memory loader verifier |
-
1991
- 1991-11-22 FR FR9114381A patent/FR2684211B1/fr not_active Expired - Lifetime
-
1992
- 1992-11-10 DE DE69212284T patent/DE69212284T2/de not_active Expired - Lifetime
- 1992-11-10 EP EP92403022A patent/EP0543698B1/fr not_active Expired - Lifetime
- 1992-11-10 ES ES92403022T patent/ES2091427T3/es not_active Expired - Lifetime
-
1995
- 1995-05-17 US US08/443,095 patent/US5500797A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2684211B1 (fr) | 1994-02-04 |
US5500797A (en) | 1996-03-19 |
EP0543698A1 (fr) | 1993-05-26 |
FR2684211A1 (fr) | 1993-05-28 |
EP0543698B1 (fr) | 1996-07-17 |
DE69212284T2 (de) | 1997-01-02 |
DE69212284D1 (de) | 1996-08-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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