| 摘要 |
<p>The assembly has a test piece (1) with a holding end (13) mounted in a fatigue simulation device and a fixation end (11), where the fixation end is formed as shape of a blade foot. A counter-test piece (2) extends longitudinally, where a holding end (23) of the counter-test piece is mounted in the fatigue simulation device. A fixation end (21) of the counter-test piece is formed as shape of cell to receive the fixation end of the test piece to test the fixation of the blade foot in the cell. The fixation end comprises two pair of maintain recesses (D1, D2) that are moved longitudinally. An independent claim is also included for a device for simulating a blade foot of an aeronautic turbomachine, comprising a frame.</p> |
