FR3036798B1 - Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant - Google Patents

Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant Download PDF

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Publication number
FR3036798B1
FR3036798B1 FR1554941A FR1554941A FR3036798B1 FR 3036798 B1 FR3036798 B1 FR 3036798B1 FR 1554941 A FR1554941 A FR 1554941A FR 1554941 A FR1554941 A FR 1554941A FR 3036798 B1 FR3036798 B1 FR 3036798B1
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FR
France
Prior art keywords
turbomachine
aircraft
detecting
gas generator
implementation device
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
FR1554941A
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English (en)
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FR3036798A1 (fr
Inventor
Fabien Mercier-Calvairac
Philippe Vallart
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.)
Safran Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines SAS
Turbomeca SA
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 Safran Helicopter Engines SAS, Turbomeca SA filed Critical Safran Helicopter Engines SAS
Priority to FR1554941A priority Critical patent/FR3036798B1/fr
Priority to PCT/FR2016/051281 priority patent/WO2016193603A1/fr
Publication of FR3036798A1 publication Critical patent/FR3036798A1/fr
Application granted granted Critical
Publication of FR3036798B1 publication Critical patent/FR3036798B1/fr
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Classifications

    • 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

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
FR1554941A 2015-06-01 2015-06-01 Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant Active FR3036798B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1554941A FR3036798B1 (fr) 2015-06-01 2015-06-01 Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant
PCT/FR2016/051281 WO2016193603A1 (fr) 2015-06-01 2016-05-30 Procédé de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1554941A FR3036798B1 (fr) 2015-06-01 2015-06-01 Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant
FR1554941 2015-06-01

Publications (2)

Publication Number Publication Date
FR3036798A1 FR3036798A1 (fr) 2016-12-02
FR3036798B1 true FR3036798B1 (fr) 2018-06-15

Family

ID=54366276

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1554941A Active FR3036798B1 (fr) 2015-06-01 2015-06-01 Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant

Country Status (2)

Country Link
FR (1) FR3036798B1 (fr)
WO (1) WO2016193603A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10442547B2 (en) 2017-06-22 2019-10-15 General Electric Company Engine and electrical machine health monitoring

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2769952A1 (fr) * 1997-10-20 1999-04-23 Aerospatiale Dispositif de demarrage pour turbine a gaz dans un aeronef
JP2006291762A (ja) * 2005-04-07 2006-10-26 Honda Motor Co Ltd ガスタービンエンジンの運転制御装置
US20100089067A1 (en) * 2008-10-10 2010-04-15 General Electric Company Adaptive performance model and methods for system maintenance
US9097197B2 (en) * 2011-03-31 2015-08-04 Robert Bosch Gmbh Defining a region of optimization based on engine usage data
EP2762852A1 (fr) * 2013-02-05 2014-08-06 Siemens Aktiengesellschaft Système de test automatique pour turbine à gaz
US10956534B2 (en) * 2013-02-20 2021-03-23 Honeywell International Inc. System and method for continuous performance analysis of systems that exhibit variable performance characteristics at different operating conditions

Also Published As

Publication number Publication date
WO2016193603A1 (fr) 2016-12-08
FR3036798A1 (fr) 2016-12-02

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