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.

Abstract: A method for optimizing a low cycle and optionally high-cycle fatigue test rig includes selecting variable geometric parameters of the support member and/or of the workpiece of the rig, in addition to ranges of variation of these parameters, selecting at least one aim or design objective to be achieved, a variation in the values of at least a part of the abovementioned parameters having an influence on this aim or design objective, and testing one or a plurality of the values of the abovementioned parameters, in the respective ranges of same, and determining those values that make it possible to achieve the aim or design objection. With those values, the method including producing or modifying a support member and/or a workpiece on the basis of the optimized parameters.

Abstract: A low-cycle fatigue test rig reproduces bearing of turbine engine parts. The test rig includes a support member that is fixed to a frame and defines at least one bearing surface. A test piece is connected to a traction element for loading the test piece so that the test piece bears against the at least one bearing surface of the support member. The at least one bearing surface is supported by a support element that is mounted to rotate about a first axis on the support member. The test piece is connected to the traction element for articulation around a second axis that is perpendicular to the first axis. The test rig is configured to enable adjusting and locking the support element and the test piece in positions around the above-mentioned axes.

Abstract: Test rig combining high-frequency tribological stress and low-cycle fatigue, comprising 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 traction means for loading the second test piece so that it bears against the or each bearing surface of the first test piece, means for heating the test pieces and means 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 comprising a portion which is in the shape of a turbine engine rotor blade root and which is inserted in a groove, the shape of which groove is substantially complementary to the other test piece so as to reproduce a turbine engine blade-disc attachment.

Abstract: A method for optimising a cycle and optionally high-cycle fatigue test rig, said test being intended to reproduce a support for turbomachine parts, wherein it comprises the steps consisting of determining variable geometric parameters of the support member and/or of the workpiece of the rig, in addition to ranges of variation of these parameters, determining at least one aim to be achieved, a variation in the values of at least a part of the abovementioned parameters having an influence on this aim, modifying one or a plurality of the values of the abovementioned parameters, in the respective ranges of same, and determining those that make it possible to achieve the aim, and producing or modifying a support member and/or a workpiece on the basis of the optimised parameters.

Abstract: Low-cycle, and optionally combined low-cycle and high-cycle, fatigue test rig, for reproducing bearing of turbine engine parts, comprising a support member which is fixed to a frame and defines at least one bearing surface, and a test piece which is connected to traction means for loading the test piece so that it bears against the or each bearing surface of the member, the or each bearing surface being supported by an element which is mounted so as to rotate about a first axis on the support member, and the test piece being connected to the traction means by means for articulation around a second axis which is substantially perpendicular to the first axis, the rig further comprising means for adjusting and locking the element and the test piece in positions around the above-mentioned axes wherein.