FR3114876B1 - DIAGNOSIS OF AN AIRCRAFT ENGINE COMPUTER - Google Patents
DIAGNOSIS OF AN AIRCRAFT ENGINE COMPUTER Download PDFInfo
- Publication number
- FR3114876B1 FR3114876B1 FR2010197A FR2010197A FR3114876B1 FR 3114876 B1 FR3114876 B1 FR 3114876B1 FR 2010197 A FR2010197 A FR 2010197A FR 2010197 A FR2010197 A FR 2010197A FR 3114876 B1 FR3114876 B1 FR 3114876B1
- Authority
- FR
- France
- Prior art keywords
- aircraft engine
- diagnosis
- engine computer
- computer
- connection means
- 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
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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/005—Testing of electric installations on transport means
- G01R31/008—Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels
-
- 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
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/22—Detection or location of defective computer hardware by testing during standby operation or during idle time, e.g. start-up testing
- G06F11/26—Functional testing
- G06F11/273—Tester hardware, i.e. output processing circuits
-
- 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
- G05B2219/00—Program-control systems
- G05B2219/30—Nc systems
- G05B2219/45—Nc applications
- G05B2219/45071—Aircraft, airplane, ship cleaning manipulator, paint stripping
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Computer Hardware Design (AREA)
- Quality & Reliability (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Automation & Control Theory (AREA)
- Testing Of Engines (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
Dispositif (24) et procédé de diagnostic d’un calculateur moteur (16) d’aéronef, ce dispositif comportant une unité électronique de diagnostic (26) qui est autonome et mobile, ainsi que des moyens de raccordement (28) de l’unité à un calculateur d’un moteur d’aéronef, ces moyens de raccordement comprenant avantageusement un unique câble de raccordement (38). Figure pour l'abrégé : Figure 3Device (24) and method for diagnosing an aircraft engine computer (16), this device comprising an electronic diagnostic unit (26) which is autonomous and mobile, as well as connection means (28) of the unit to a computer of an aircraft engine, these connection means advantageously comprising a single connection cable (38). Figure for abstract: Figure 3
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2010197A FR3114876B1 (en) | 2020-10-06 | 2020-10-06 | DIAGNOSIS OF AN AIRCRAFT ENGINE COMPUTER |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2010197 | 2020-10-06 | ||
FR2010197A FR3114876B1 (en) | 2020-10-06 | 2020-10-06 | DIAGNOSIS OF AN AIRCRAFT ENGINE COMPUTER |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3114876A1 FR3114876A1 (en) | 2022-04-08 |
FR3114876B1 true FR3114876B1 (en) | 2022-11-04 |
Family
ID=74045710
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2010197A Active FR3114876B1 (en) | 2020-10-06 | 2020-10-06 | DIAGNOSIS OF AN AIRCRAFT ENGINE COMPUTER |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3114876B1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6442498B1 (en) * | 1999-06-15 | 2002-08-27 | Henrick Youval Krigel | Apparatus and method for determining the integrity of cables and wiring harnesses |
FR3005744B1 (en) * | 2013-05-14 | 2015-08-21 | Airbus Operations Sas | SYSTEM AND METHOD FOR INTEGRITY TESTING OF AN ELECTRICAL NETWORK IN AN AIRCRAFT |
FR3078791B1 (en) * | 2018-03-09 | 2020-02-28 | Safran Helicopter Engines | CALCULATOR DIAGNOSTIC TOOL |
DE102018214326A1 (en) * | 2018-08-24 | 2020-02-27 | Airbus Operations Gmbh | Wiring harness test system and test procedure for checking wiring harnesses |
-
2020
- 2020-10-06 FR FR2010197A patent/FR3114876B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3114876A1 (en) | 2022-04-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20220408 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |