FR3043203B1 - DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE, TURBOMACHINE EQUIPPED WITH SUCH A DEVICE AND METHOD FOR MANUFACTURING A SEAL FOR SEALING SUCH A DEVICE - Google Patents

DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE, TURBOMACHINE EQUIPPED WITH SUCH A DEVICE AND METHOD FOR MANUFACTURING A SEAL FOR SEALING SUCH A DEVICE Download PDF

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Publication number
FR3043203B1
FR3043203B1 FR1560594A FR1560594A FR3043203B1 FR 3043203 B1 FR3043203 B1 FR 3043203B1 FR 1560594 A FR1560594 A FR 1560594A FR 1560594 A FR1560594 A FR 1560594A FR 3043203 B1 FR3043203 B1 FR 3043203B1
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FR
France
Prior art keywords
turbomachine
opening
seal
sealing
manufacturing
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
FR1560594A
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French (fr)
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FR3043203A1 (en
Inventor
Joseph Bernard Kockenpo Florian
Jeremy Giordan
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 Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
SNECMA SAS
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Priority to FR1560594A priority Critical patent/FR3043203B1/en
Publication of FR3043203A1 publication Critical patent/FR3043203A1/en
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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

Abstract

L'invention concerne un dispositif (1) de mesure de paramètres d'un flux aérodynamique dans une turbomachine (100), le dispositif (1) comprenant un moyen de mesure (3) apte à mesurer lesdits paramètres, un support (2) apte à être fixé à un carter (101) de la turbomachine (100) et à porter ledit moyen de mesure (3), le support (2) comprenant une paroi (5) pourvue d'une ouverture principale traversante (6) et d'au moins une lumière secondaire traversante débouchant dans l'ouverture principale, l'ouverture principale (6) et la lumière secondaire (7) traversante permettant le passage du moyen de mesure lors de son montage, un couvercle (4) configuré de manière à obturer ou libérer l'ouverture traversante (6) du support, et un joint d'étanchéité (14) moulé et agencé de manière amovible dans la lumière (7).The invention relates to a device (1) for measuring the parameters of an aerodynamic flow in a turbomachine (100), the device (1) comprising a measuring means (3) capable of measuring said parameters, a support (2) capable of to be fixed to a casing (101) of the turbomachine (100) and to carry said measuring means (3), the support (2) comprising a wall (5) provided with a main through opening (6) and at least one secondary through-hole opening into the main opening, the main opening (6) and the secondary through-hole (7) permitting passage of the measuring means during its assembly, a cover (4) configured so as to close or releasing the through opening (6) of the support, and a molded seal (14) removably arranged in the lumen (7).

FR1560594A 2015-11-04 2015-11-04 DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE, TURBOMACHINE EQUIPPED WITH SUCH A DEVICE AND METHOD FOR MANUFACTURING A SEAL FOR SEALING SUCH A DEVICE Active FR3043203B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1560594A FR3043203B1 (en) 2015-11-04 2015-11-04 DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE, TURBOMACHINE EQUIPPED WITH SUCH A DEVICE AND METHOD FOR MANUFACTURING A SEAL FOR SEALING SUCH A DEVICE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1560594 2015-11-04
FR1560594A FR3043203B1 (en) 2015-11-04 2015-11-04 DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE, TURBOMACHINE EQUIPPED WITH SUCH A DEVICE AND METHOD FOR MANUFACTURING A SEAL FOR SEALING SUCH A DEVICE

Publications (2)

Publication Number Publication Date
FR3043203A1 FR3043203A1 (en) 2017-05-05
FR3043203B1 true FR3043203B1 (en) 2019-01-25

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FR1560594A Active FR3043203B1 (en) 2015-11-04 2015-11-04 DEVICE FOR MEASURING PARAMETERS OF AERODYNAMIC FLOW OF A TURBOMACHINE, TURBOMACHINE EQUIPPED WITH SUCH A DEVICE AND METHOD FOR MANUFACTURING A SEAL FOR SEALING SUCH A DEVICE

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FR (1) FR3043203B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3067454B1 (en) * 2017-06-13 2019-07-05 Safran Aircraft Engines ASSEMBLY FOR MEASURING AT LEAST ONE PARAMETER OF A TURBOMACHINE FLOW AND SEPARATION SPOUT COMPRISING SUCH A MEASURING ASSEMBLY
FR3079299B1 (en) 2018-03-22 2020-06-05 Safran Aircraft Engines DEVICE FOR MEASURING THE CHARACTERISTICS OF AN AIR FLOW
FR3134890B1 (en) * 2022-04-25 2024-03-15 Safran Aircraft Engines Air flow characteristics measurement set

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7159401B1 (en) * 2004-12-23 2007-01-09 Kulite Semiconductor Products, Inc. System for detecting and compensating for aerodynamic instabilities in turbo-jet engines
US8204671B2 (en) * 2009-05-18 2012-06-19 United Technologies Corporation System and method of estimating gas turbine engine performance
FR2995996B1 (en) * 2012-09-26 2014-10-31 Snecma MEASURING DEVICE FOR COMBUSTION CHAMBER MOUNTED ON TEST BENCH
US9027392B2 (en) * 2013-05-07 2015-05-12 Honeywell International Inc. Multi-hole probes and methods for manufacturing multi-hole probes

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Publication number Publication date
FR3043203A1 (en) 2017-05-05

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