FR3112608B1 - TEST BENCH AND ITS IMPLEMENTATION PROCESS - Google Patents

TEST BENCH AND ITS IMPLEMENTATION PROCESS Download PDF

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Publication number
FR3112608B1
FR3112608B1 FR2007415A FR2007415A FR3112608B1 FR 3112608 B1 FR3112608 B1 FR 3112608B1 FR 2007415 A FR2007415 A FR 2007415A FR 2007415 A FR2007415 A FR 2007415A FR 3112608 B1 FR3112608 B1 FR 3112608B1
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FR
France
Prior art keywords
test bench
horn
uprights
implementation process
gantry
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
FR2007415A
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French (fr)
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FR3112608A1 (en
Inventor
Eric André François Pellion
Thibault Xavier Alexis Berranger
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 FR2007415A priority Critical patent/FR3112608B1/en
Publication of FR3112608A1 publication Critical patent/FR3112608A1/en
Application granted granted Critical
Publication of FR3112608B1 publication Critical patent/FR3112608B1/en
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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • G01M13/02Gearings; Transmission mechanisms
    • G01M13/027Test-benches with force-applying means, e.g. loading of drive shafts along several directions
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00Testing of engines
    • G01M15/14Testing gas-turbine engines or jet-propulsion engines
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0025Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of elongated objects, e.g. pipes, masts, towers or railways
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0075Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by means of external apparatus, e.g. test benches or portable test systems

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

L’invention concerne un banc d’essai (1) pour solliciter en torsion une pièce (100) d’une turbomachine d’aéronef, comprenant un système de reprise de couple (4), lui-même comprenant : - un guignol (10) solidaire en rotation de la pièce (100), - des galets (11) de support du guignol (10) et de guidage en rotation du guignol (10) autour dudit axe (X), - un portique (30) comportant deux montants verticaux (31) qui sont situés de chaque côté de la pièce (100), et - des bielles (20) de liaison du guignol (10) aux montants (31) du portique (30), chaque bielle (20) comportant une première extrémité (21) articulée sur le guignol (10) et une seconde extrémité (22) opposée articulée sur un des montants (31). L’invention concerne en outre un procédé de mise en œuvre d’un effort en torsion d’une pièce (100), telle qu’un arbre de turbomachine d’aéronef, au moyen d’un banc d’essai (1) tel que décrit précédemment. Figure pour l'abrégé : Figure 2The invention relates to a test bench (1) for stressing in torsion a part (100) of an aircraft turbomachine, comprising a torque take-up system (4), itself comprising: - a bell crank (10 ) integral in rotation with the part (100), - rollers (11) for supporting the horn (10) and for guiding the horn (10) in rotation around said axis (X), - a gantry (30) comprising two uprights vertical (31) which are located on each side of the part (100), and - connecting rods (20) of the horn (10) to the uprights (31) of the gantry (30), each connecting rod (20) comprising a first end (21) articulated on the bell crank (10) and a second opposite end (22) articulated on one of the uprights (31). The invention further relates to a method for applying a torsional force to a part (100), such as an aircraft turbomachine shaft, by means of a test bench (1) such than previously described. Figure for the abstract: Figure 2

FR2007415A 2020-07-15 2020-07-15 TEST BENCH AND ITS IMPLEMENTATION PROCESS Active FR3112608B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2007415A FR3112608B1 (en) 2020-07-15 2020-07-15 TEST BENCH AND ITS IMPLEMENTATION PROCESS

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2007415 2020-07-15
FR2007415A FR3112608B1 (en) 2020-07-15 2020-07-15 TEST BENCH AND ITS IMPLEMENTATION PROCESS

Publications (2)

Publication Number Publication Date
FR3112608A1 FR3112608A1 (en) 2022-01-21
FR3112608B1 true FR3112608B1 (en) 2022-06-10

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ID=73013596

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2007415A Active FR3112608B1 (en) 2020-07-15 2020-07-15 TEST BENCH AND ITS IMPLEMENTATION PROCESS

Country Status (1)

Country Link
FR (1) FR3112608B1 (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108225693A (en) * 2017-12-21 2018-06-29 杭州中德传动设备有限公司 A kind of rotary decelerator rigidity detection device and its detection method
CN108414170B (en) * 2018-03-15 2019-05-10 哈尔滨工业大学 Stiffness measurement device under a kind of synchronous loading environment of large-size axis parts shape part bending

Also Published As

Publication number Publication date
FR3112608A1 (en) 2022-01-21

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