The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 16, 2018

Filed:

May. 09, 2014
Applicants:

Turbomeca, Bordes, FR;

Snecma, Paris, FR;

Inventors:

Laurent Houze, Andoins, FR;

Jean Philippe Lapuyade, Monein, FR;

Franck Vernis, Mirepeix, FR;

François Vogel, Ousse, FR;

Jean Vincent Manuel Meriaux, Moissy-Cramayel, FR;

Assignees:

TURBOMECA, Bordes, FR;

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01N 3/32 (2006.01); G01N 3/04 (2006.01);
U.S. Cl.
CPC ...
G01N 3/32 (2013.01); G01N 2203/0005 (2013.01); G01N 2203/0073 (2013.01); G01N 2203/027 (2013.01); G01N 2203/0226 (2013.01);
Abstract

A test rig combining high-frequency tribological stress and low-cycle fatigue. The test rig includes a first test piece which is fixed to a frame and defines at least one bearing surface, a second test piece which is connected to an actuator for loading the second test piece so that it bears against the at least one bearing surface of the first test piece, a heater configured for heating the test pieces and a vibration generator, such as a shaker, for loading the test pieces in a vibratory manner so as to carry out a fretting fatigue and low-cycle and high-cycle fatigue test. One of the test pieces includes a portion in the shape of a turbine engine rotor blade root and which is inserted in a groove having a shape that is substantially complementary to the other test piece so as to reproduce a turbine engine blade-disc attachment.


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