EP1512628A1 - Verfahren und Vorrichtung für die Wartung eines Funknavigationsgerätes eines Luftfahrzeuges - Google Patents

Verfahren und Vorrichtung für die Wartung eines Funknavigationsgerätes eines Luftfahrzeuges Download PDF

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Publication number
EP1512628A1
EP1512628A1 EP04291980A EP04291980A EP1512628A1 EP 1512628 A1 EP1512628 A1 EP 1512628A1 EP 04291980 A EP04291980 A EP 04291980A EP 04291980 A EP04291980 A EP 04291980A EP 1512628 A1 EP1512628 A1 EP 1512628A1
Authority
EP
European Patent Office
Prior art keywords
aircraft
equipment
events
radionavigation
radionavigation equipment
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.)
Granted
Application number
EP04291980A
Other languages
English (en)
French (fr)
Other versions
EP1512628B1 (de
Inventor
Dominique Pomies
Gilles Tatham
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
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Airbus Operations SAS
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Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of EP1512628A1 publication Critical patent/EP1512628A1/de
Application granted granted Critical
Publication of EP1512628B1 publication Critical patent/EP1512628B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/006—Indicating maintenance
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0841—Registering performance data
    • G07C5/085—Registering performance data using electronic data carriers

Definitions

  • the present invention relates to a method and a device for maintenance of a radionavigation equipment of an aircraft, in particular of a transport plane.
  • radionavigation equipment of an aircraft such as a distance measuring device of the DME type ("Distance Measuring Equipment "), a VHF omnidirectional range (" Very High Frequency "), a GPS-based location system (“ Global Positioning System ”) or a landing aid type GLS (“GP Landing System ”) for example, receives data that is external to the aircraft and develops information, including information relating to at the position of the aircraft, from said external data. he typically provides this information to other aircraft systems, in particular guidance systems or display of the position of the aircraft.
  • the origin is identified as coming from the said information which is provided by the said radionavigation equipment to other the aircraft, the maintenance procedures provide that the said equipment radionavigation must be submitted and sent to a repair technician for be checked and repaired if necessary.
  • radionavigation equipment may be erroneous, not only because of a failure of that radio navigation equipment, but also because of a problem relating to said external data received by said radionavigation equipment.
  • the usual maintenance procedures are unnecessarily long and costly, since radionavigation equipment is filed and sent for repair, while it is not in failure, since the said malfunction occurred on board the aircraft is due to said data external to the aircraft.
  • the present invention aims to overcome these disadvantages. It relates to a method of maintenance of a radionavigation equipment an aircraft, to reduce the number of cases, to which said radionavigation equipment is to be deposited for verification and possible repair when this equipment is suspected to be causing a malfunction on board the aircraft.
  • said radionavigation equipment is deposited to send it for repair, only if said first events recorded do not prove that the said malfunction is due to a problem with data outside the aircraft received by the said radionavigation equipment, which makes it possible understood to significantly reduce the number of unnecessary depositions, and therefore, to reduce the cost and the maintenance time.
  • said steps a) and b) are carried out during the flight of the aircraft, and said step c) at the end of said flight, after the return to the ground of the aircraft.
  • said radionavigation equipment is a landing aid device for the aircraft combined with a satellite positioning system, and said first events recorded represent the situations for which the data received by said landing aid device not provide an indication of the correct position of the aircraft.
  • the present invention also relates to a maintenance device of an aircraft.
  • Figure 1 schematically illustrates a radionavigation equipment an aircraft, to which a maintenance device is applied according to the invention.
  • Figure 2 is the block diagram of a maintenance device according to the invention.
  • the device 1 according to the invention is intended for maintenance a radionavigation equipment 2 of an aircraft A, in particular a civil transport aircraft.
  • Said radionavigation equipment 2 may, in particular, be a distance measuring device of the DME type Equipment "), a VHF omnidirectional range (" Very High Frequency "), a GPS-based location system (" Global Positioning System ”) or a landing aid type GLS (" GPS Landing System ").
  • said radionavigation equipment 2 of the usual type, which is arranged on board the aircraft A, is likely to receive data from outside the aircraft A, in particular in the form of electromagnetic waves OE, using for example of an antenna 3. It draws from this external data information, for example information or position indications, which he transmits, via links 4, to user systems 5 of the aircraft A, in particular guidance systems or systems display.
  • said radionavigation equipment 2 is a device for assisting landing of the aircraft A type GLS, which is combined with a positioning system 6.
  • This positioning system 6 comprises a set of satellites S1, S2 and / or ground stations P1, P2 which are provided on earth T. These satellites S1, S2 and these ground stations P1, P2 can communicate between them, and with said radionavigation equipment 2, using electromagnetic waves OE.
  • the maintenance device 1 is associated with said equipment of radionavigation 2, as generally represented by a 1 A link in phantom in Figure 1, and as specified below, and is intended to reduce the number of cases for which the equipment radionavigation 2 must be filed for verification and possible repair when this equipment 2 is suspected to be causing a malfunction intervened on board the aircraft A.
  • Said central unit 13 comprises means 16 and a display screen 17 which is connected by a link 18 to said means 16.
  • said means 16 is a unit acquiring information, which receives said first and second lists and displays them on the display screen 17.
  • the analysis or verification preceding is implemented by a maintenance operator, reading said two lists presented to him on the display screen 17.
  • said means 16 is a unit information processing, which automatically implements the analysis previous verification, from those two lists received, and presents the result of this analysis (whether or not the equipment radionavigation 2) to a maintenance operator by displaying it on the screen display 17.
  • the above-mentioned registration of the first and second events is performed during the flight of the aircraft A, and the analysis verification of the said recordings is carried out subsequently, after the return to the ground of this aircraft A.
  • said maintenance device 1 presents the advantage of avoiding filing (and sending for repair) equipment 2, when this equipment 2 could not provide valid information to other systems 5 of the aircraft A, while the origin the fact that he could not provide this information was not attributable to him, but was attributable to causes outside the A-aircraft.
  • maintenance 1 is therefore very advantageous in terms of duration and maintenance cost.
  • radio navigation equipment 2 a complex function, since it uses external data from a space segment (radiofrequency RF signals transmitted by GPS satellites, for example satellites S1 and S2) and a segment ground (VHF data link transmitted by ground stations GPS differential, for example ground stations P1 and P2).
  • a space segment radiofrequency RF signals transmitted by GPS satellites, for example satellites S1 and S2
  • a segment ground VHF data link transmitted by ground stations GPS differential, for example ground stations P1 and P2).
  • RF signals and VHF data are grouped together in the figure 1, under the reference OE generally designating electromagnetic waves.
  • said first recorded events represent the situations for which the external data received by said device 2 landing aid does not provide an indication correct position of the aircraft A.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Catching Or Destruction (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
EP04291980A 2003-09-05 2004-08-03 Verfahren und Vorrichtung für die Wartung eines Funknavigationsgerätes eines Luftfahrzeuges Expired - Lifetime EP1512628B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0310497 2003-09-05
FR0310497A FR2859556B1 (fr) 2003-09-05 2003-09-05 Procede et dispositif de maintenance d'un equipement de radionavigation d'un aeronef

Publications (2)

Publication Number Publication Date
EP1512628A1 true EP1512628A1 (de) 2005-03-09
EP1512628B1 EP1512628B1 (de) 2006-09-27

Family

ID=34130754

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04291980A Expired - Lifetime EP1512628B1 (de) 2003-09-05 2004-08-03 Verfahren und Vorrichtung für die Wartung eines Funknavigationsgerätes eines Luftfahrzeuges

Country Status (7)

Country Link
US (1) US7519456B2 (de)
EP (1) EP1512628B1 (de)
AT (1) ATE340736T1 (de)
CA (1) CA2478779C (de)
DE (1) DE602004002535T2 (de)
ES (1) ES2271806T3 (de)
FR (1) FR2859556B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2072399A1 (de) * 2007-12-21 2009-06-24 Snecma Services Method and system for characterising and counting excesses of a threshold by an operating parameter of an aircraft engine

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2859556B1 (fr) * 2003-09-05 2005-11-11 Airbus France Procede et dispositif de maintenance d'un equipement de radionavigation d'un aeronef
FR2914803B1 (fr) * 2007-04-06 2009-09-18 Airbus Sas Procede et dispositif de maintenance dans un aeronef
CN115481443A (zh) * 2022-10-20 2022-12-16 四川傲势科技有限公司 飞行数据保护方法、装置、终端设备及存储介质

Citations (5)

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US4943919A (en) * 1988-10-17 1990-07-24 The Boeing Company Central maintenance computer system and fault data handling method
US6115656A (en) * 1997-06-17 2000-09-05 Mcdonnell Douglas Corporation Fault recording and reporting method
WO2001097038A1 (en) * 2000-06-13 2001-12-20 Saab Ab System and method for maintenance
US20030083794A1 (en) * 2001-10-27 2003-05-01 Juergen Halm System and method for diagnosing aircraft components for maintenance purposes
US6598179B1 (en) * 2000-03-31 2003-07-22 International Business Machines Corporation Table-based error log analysis

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US4729102A (en) * 1984-10-24 1988-03-01 Sundstrand Data Control, Inc. Aircraft data acquisition and recording system
US5216611A (en) * 1991-02-08 1993-06-01 Rockwell International Corporation Integrated enroute and approach guidance system for aircraft
CA2072169A1 (en) * 1991-06-24 1992-12-25 Lih-Juan L. Danielson In-band/out-of-band alert delivery system
WO1993004546A1 (fr) * 1991-08-23 1993-03-04 Kabushiki Kaisha Toshiba Systeme d'informations et de communications radio mettant en ×uvre un systeme de transmission a porteuses multiples et a etalement du spectre
US5957995A (en) * 1996-06-17 1999-09-28 Trimble Navigation Radio navigation emulating GPS system
US5890079A (en) * 1996-12-17 1999-03-30 Levine; Seymour Remote aircraft flight recorder and advisory system
US6324592B1 (en) * 1997-02-25 2001-11-27 Keystone Aerospace Apparatus and method for a mobile computer architecture and input/output management system
US6115654A (en) * 1997-12-23 2000-09-05 Simmonds Precision Products, Inc. Universal sensor interface system and method
US6313786B1 (en) * 1998-07-02 2001-11-06 Snaptrack, Inc. Method and apparatus for measurement processing of satellite positioning system (SPS) signals
DE19839193A1 (de) * 1998-08-28 2000-03-02 Bosch Gmbh Robert Vorrichtung zur Steuerung und Überwachung eines Fahrzeuges
WO2001001366A2 (en) * 1999-06-25 2001-01-04 Telemonitor, Inc. Smart remote monitoring system and method
DE10007218B4 (de) * 2000-02-17 2009-11-26 Robert Bosch Gmbh Verfahren zur Ereignisinterpretation und Ausgabe von Bedienhinweisen in Kraftfahrzeugen
US6693558B2 (en) * 2001-06-18 2004-02-17 Innovative Solutions & Support, Inc. Aircraft flat panel display system
FR2859556B1 (fr) * 2003-09-05 2005-11-11 Airbus France Procede et dispositif de maintenance d'un equipement de radionavigation d'un aeronef
US7149612B2 (en) * 2004-01-05 2006-12-12 Arinc Incorporated System and method for monitoring and reporting aircraft quick access recorder data
FR2875901B1 (fr) * 2004-09-28 2006-12-08 Eurocopter France Systeme embarque de construction d'une route aerienne

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4943919A (en) * 1988-10-17 1990-07-24 The Boeing Company Central maintenance computer system and fault data handling method
US6115656A (en) * 1997-06-17 2000-09-05 Mcdonnell Douglas Corporation Fault recording and reporting method
US6598179B1 (en) * 2000-03-31 2003-07-22 International Business Machines Corporation Table-based error log analysis
WO2001097038A1 (en) * 2000-06-13 2001-12-20 Saab Ab System and method for maintenance
US20030083794A1 (en) * 2001-10-27 2003-05-01 Juergen Halm System and method for diagnosing aircraft components for maintenance purposes

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2072399A1 (de) * 2007-12-21 2009-06-24 Snecma Services Method and system for characterising and counting excesses of a threshold by an operating parameter of an aircraft engine
FR2925595A1 (fr) * 2007-12-21 2009-06-26 Snecma Services Sa Procede et systeme de caracterisation et de comptage de depassements d'un seuil par un parametre de fonctionnement d'un moteur d'aeronef
RU2482999C2 (ru) * 2007-12-21 2013-05-27 Снекма Сервис Способ и система характеризации и учета превышений порога рабочего параметра двигателя летательного аппарата
US8564457B2 (en) 2007-12-21 2013-10-22 Snecma Services Method and a system for characterizing and counting violations of a threshold by an aircraft engine operating parameter

Also Published As

Publication number Publication date
US20060293803A1 (en) 2006-12-28
DE602004002535T2 (de) 2007-09-06
ES2271806T3 (es) 2007-04-16
US7519456B2 (en) 2009-04-14
EP1512628B1 (de) 2006-09-27
FR2859556A1 (fr) 2005-03-11
CA2478779A1 (fr) 2005-03-05
FR2859556B1 (fr) 2005-11-11
DE602004002535D1 (de) 2006-11-09
ATE340736T1 (de) 2006-10-15
CA2478779C (fr) 2014-06-03

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