Device for testing the coating of a vane base
View Patent ↗A device for testing a coating for a turbomachine rotor disk blade root, including two test piece halves, each including a bearing surface coated with the coating, one counter test piece including two bearing surfaces, and a machine including a first holding system for the counter test piece and a second holding system for holding the test piece halves around the counter test piece. With a tensile mechanism, the holding systems are subjected to predetermined tensile cycles along the tensile axis, during which the tensile force is transmitted from one holding system to the other via the respective bearing surfaces contacting the counter test piece and the test piece halves. The second holding system includes a resilient return mechanism allowing for the two test piece halves to open up in a direction perpendicular to the tensile direction.
1. A device for testing a coating capable of coating a turbomachine rotor blade root, the device comprising:
two test piece halves, each including a bearing surface coated with the coating;
one counter test piece including two bearing surfaces; and
a test machine comprising a first holding system that holds the counter test piece along a tensile axis, a second holding system that holds the test piece halves around the counter test piece, and tensile means for subjecting the holding systems to predetermined tensile cycles along the tensile axis, during which tensile strain is transmitted from one holding system to the other via the respective bearing surfaces contacting each other of the counter test piece and the test piece halves, and wherein the second holding system comprises resilient return means allowing for the two test piece halves to open up in a direction perpendicular to the tensile direction in response to an opening force applied to these two test piece halves by the counter test piece during a tensile cycle.
2. The test device according to claim 1 , wherein the side of the test piece halves located on the side of the counter test piece has no undercut.
3. The test device according to claim 1 , wherein the bearing surfaces of the test piece halves are sloping with respect to the tensile axis, so as to represent a shape of the bearing surfaces of the turbomachine rotor blade root.
4. The test device according to claim 1 , wherein the bearing surfaces of the counter test piece are sloping with respect to the tensile axis, so as to represent a shape of the bearing surfaces of a turbomachine rotor disk tenon.
5. The test device according to claim 1 , wherein the resilient return means comprises at least one bar of resilient material, deforming while remaining in its range of elastic deformation during tensile cycles.
6. The test device according to claim 1 , wherein the second holding system further comprises two posts parallel to the tensile axis and used for holding the two test piece halves, and a bar connecting the posts according to a direction perpendicular to the tensile axis.
7. The test device according to claim 1 , further comprising means for measuring opening of the test piece halves during testing.
8. The test device according to claim 1 , wherein the test piece halves include, close to the bearing surfaces thereof, a shape representing turbomachine rotor blade root halves, and the tensile axis is arranged substantially in the radial direction of the blade root halves.
9. The test device according to claim 1 , wherein the counter test piece includes, close to the bearing surfaces thereof, a shape representing a shape of a tenon of a turbomachine rotor disk.
10. The test device according to claim 1 , wherein the counter test piece is formed of a titanium or nickel base alloy.
11. The test device according to claim 1 , wherein the test piece halves are formed of a titanium or nickel base alloy.