FR2960319B1 - METHOD FOR INCREASING THE RELIABILITY OF VIBRATION INFORMATION PROVIDED BY AIRCRAFT SENSORS - Google Patents

METHOD FOR INCREASING THE RELIABILITY OF VIBRATION INFORMATION PROVIDED BY AIRCRAFT SENSORS

Info

Publication number
FR2960319B1
FR2960319B1 FR1053882A FR1053882A FR2960319B1 FR 2960319 B1 FR2960319 B1 FR 2960319B1 FR 1053882 A FR1053882 A FR 1053882A FR 1053882 A FR1053882 A FR 1053882A FR 2960319 B1 FR2960319 B1 FR 2960319B1
Authority
FR
France
Prior art keywords
reliability
increasing
information provided
vibration information
aircraft sensors
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
Application number
FR1053882A
Other languages
French (fr)
Other versions
FR2960319A1 (en
Inventor
Philippe Chareyre
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
Original Assignee
Airbus Operations SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1053882A priority Critical patent/FR2960319B1/en
Publication of FR2960319A1 publication Critical patent/FR2960319A1/en
Application granted granted Critical
Publication of FR2960319B1 publication Critical patent/FR2960319B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
FR1053882A 2010-05-19 2010-05-19 METHOD FOR INCREASING THE RELIABILITY OF VIBRATION INFORMATION PROVIDED BY AIRCRAFT SENSORS Active FR2960319B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1053882A FR2960319B1 (en) 2010-05-19 2010-05-19 METHOD FOR INCREASING THE RELIABILITY OF VIBRATION INFORMATION PROVIDED BY AIRCRAFT SENSORS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1053882A FR2960319B1 (en) 2010-05-19 2010-05-19 METHOD FOR INCREASING THE RELIABILITY OF VIBRATION INFORMATION PROVIDED BY AIRCRAFT SENSORS

Publications (2)

Publication Number Publication Date
FR2960319A1 FR2960319A1 (en) 2011-11-25
FR2960319B1 true FR2960319B1 (en) 2012-08-03

Family

ID=43302627

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1053882A Active FR2960319B1 (en) 2010-05-19 2010-05-19 METHOD FOR INCREASING THE RELIABILITY OF VIBRATION INFORMATION PROVIDED BY AIRCRAFT SENSORS

Country Status (1)

Country Link
FR (1) FR2960319B1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3064064B1 (en) * 2017-03-20 2021-09-17 Safran Aircraft Engines TURBOMACHINE ROTOR BALANCING
FR3075359B1 (en) 2017-12-18 2019-11-22 Safran Aircraft Engines DETECTION AND ACCOMODATION OF INTERMITTENT OPEN CIRCUITS ON A MOTOR SENSOR OF AN AIRCRAFT TURBOMACHINE
FR3092368B1 (en) * 2019-02-05 2021-01-08 Safran Aircraft Engines Monitoring the health of at least two vibration sensors of a twin-barrel turbomachine
FR3132901A1 (en) * 2022-02-21 2023-08-25 Airbus Operations (S.A.S). Method for detecting vibrations coming from a rotating machine of an aircraft.

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4485678A (en) * 1982-09-27 1984-12-04 Mechanical Technology Incorporated Rotor diagnostic and balancing system
US4566101A (en) * 1983-02-28 1986-01-21 United Technologies Corporation Oscillatory failure monitor
GB2248110B (en) * 1990-09-19 1994-08-31 Rolls Royce Plc Engine vibration analysis system for a multi shaft turbine
EP0913746A3 (en) * 1997-10-31 2000-04-12 Honeywell Inc. Sensor invalidation system

Also Published As

Publication number Publication date
FR2960319A1 (en) 2011-11-25

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