FR3063345B1 - Dispositif de test d'une turbomachine a gaz pour aeronef - Google Patents

Dispositif de test d'une turbomachine a gaz pour aeronef Download PDF

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Publication number
FR3063345B1
FR3063345B1 FR1751576A FR1751576A FR3063345B1 FR 3063345 B1 FR3063345 B1 FR 3063345B1 FR 1751576 A FR1751576 A FR 1751576A FR 1751576 A FR1751576 A FR 1751576A FR 3063345 B1 FR3063345 B1 FR 3063345B1
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FR
France
Prior art keywords
gas
turbomachine
aircraft
test device
gas turbomachine
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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
FR1751576A
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English (en)
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FR3063345A1 (fr
Inventor
Samuel Louis-Marie Bernard
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
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Safran Aircraft Engines SAS
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Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1751576A priority Critical patent/FR3063345B1/fr
Publication of FR3063345A1 publication Critical patent/FR3063345A1/fr
Application granted granted Critical
Publication of FR3063345B1 publication Critical patent/FR3063345B1/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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • G01M15/02—Details or accessories of testing apparatus

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Est concerné un dispositif d'essais d'une turbomachine à gaz pour aéronef présentant un axe (X) le long duquel du gaz doivent globalement s'écouler dans la turbomachine, le dispositif comprenant, axialement en amont par rapport au sens de circulation du gaz vers la turbomachine à tester, un déflecteur (19) de gaz et une virole (21) de liaison, laquelle est montée axialement entre la turbomachine (1) et le déflecteur de gaz et à laquelle la turbomachine est fixée rigidement, caractérisé en ce qu'il comprend, axialement entre la virole (21) de liaison et le déflecteur (19) de gaz, un joint creux gonflable (25).
FR1751576A 2017-02-27 2017-02-27 Dispositif de test d'une turbomachine a gaz pour aeronef Active FR3063345B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1751576A FR3063345B1 (fr) 2017-02-27 2017-02-27 Dispositif de test d'une turbomachine a gaz pour aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1751576A FR3063345B1 (fr) 2017-02-27 2017-02-27 Dispositif de test d'une turbomachine a gaz pour aeronef
FR1751576 2017-02-27

Publications (2)

Publication Number Publication Date
FR3063345A1 FR3063345A1 (fr) 2018-08-31
FR3063345B1 true FR3063345B1 (fr) 2021-01-29

Family

ID=59409400

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1751576A Active FR3063345B1 (fr) 2017-02-27 2017-02-27 Dispositif de test d'une turbomachine a gaz pour aeronef

Country Status (1)

Country Link
FR (1) FR3063345B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109387370B (zh) * 2018-11-14 2023-12-22 中国空空导弹研究院 一种冲压发动机直连式高空模拟试验无轴向力进气系统

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751550C3 (de) * 1968-06-18 1975-04-17 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Dichtung zwischen dem Einlauf eines Strahltriebwerkes und einem zellenfesten Aufnahmering des Einlaufgehäuses
US20090100918A1 (en) * 2007-09-26 2009-04-23 United Technologies Corp. Systems and Methods for Testing Gas Turbine Engines
US8079809B2 (en) * 2008-06-26 2011-12-20 Honeywell International Inc. Inflatable seal assembly between an engine inlet and a vehicle
RU2439526C1 (ru) * 2010-06-25 2012-01-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Входное устройство для испытаний газотурбинных двигателей в термобарокамере
BE1022170B1 (fr) * 2014-10-15 2016-02-24 Techspace Aero S.A. Capot moteur isolant pour test de turbomachine sur banc d'essais

Also Published As

Publication number Publication date
FR3063345A1 (fr) 2018-08-31

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