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Sample text

Testing of ceramics employed a resistance furnace, which heated the test bar by radiation. 02 DIA All dimensions in mm Not Drawn to Scale Figure 3: Thermal mechanical fatigue test bar configuration. 15 Appendix 1 Figure 4: Typical hysteresis curves for TMF testing. (Note increasing tensile load with cycles) 16 Appendix 1 1000C 400C Temperature 50C Strain Time Figure 5: Typical temperature strain cycle for “Out of Phase” TMF test, with a compressive hold at the maximum temperature. 1 10 100 1000 Cycles to failure, N f Figure 6: CMSX-4 baseline TMF data.

Induction heating was used but testpieces with a ceramic thermal barrier coating were heated using a silicon carbide igniter method. Strains were measured by linear-variable differential transducers attached to extensometers, which "touched on" to the testpiece gauge section and temperatures were measured by a thermocouple attached to the center of the testpiece by spring loading. In order to calibrate the equipment testpieces were heated to 400 C and to 1000 C and a small load was applied at each temperature to enable the elastic modulus to be determined.

For equivalent test conditions there were considerably fewer secondary cracks in the platinum aluminide system than in testpieces coated with SV-20 and several of these had penetrated much further into the substrate. Surface cracking was not extensive except close to the fracture surface as shown in Figure 21. 7 Appendix 1 SV-20 + SiPdAl Many more secondary cracks were observed at higher strains in these testpieces than in the comparable testpieces coated with SV-20. This may have resulted in increased lives in that cracks did not reach critical lengths until later stages.

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Advanced [gas] Turbine System - Conceptual Design [final rpt]

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