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Additional resources for Advanced [gas] Turbine System - Conceptual Design [final rpt]
The advantage of this approach is that modulus changes due to variation in orientation of the single crystal, which affect the stress range, are incorporated. Conclusions 1. Coated testpieces of CMSX-4 showed reduced TMF resistance compared with the uncoated alloy in “out-of-phase” testing at various strain ranges. 2. Testpieces coated with SV-34 showed the smallest reduction in TMF resistance and aluminide overcoats also performed well, particularly at the higher strain ranges. 3. Increased maximum temperatures and the introduction of hold times both reduced TMF resistance.
Finite Element Analysis A finite element (FE) analysis was performed as part of a “Small Business R&D Project sponsored by NASA by DCT Technologies, a consulting engineering company located in Cleveland, and Figure 23 shows a schematic representation of the FE model. The model shows that the crack will initiate at the interface under the influence of a radial tensile stress. The computational results also showed that the maximum tension in the coating was concentrated at the peak region near the interface, and Figure 24 presents the axial strain profiles as a function of time for the bulk of the testpiece.
The computational results also showed that the maximum tension in the coating was concentrated at the peak region near the interface, and Figure 24 presents the axial strain profiles as a function of time for the bulk of the testpiece. 0% mechanical strain range and it can be seen that the radial stress is negative or compressive in nature at the early stage of testing. 0% the maximum radial stress changed from zero to approximately 150 MPa in less than 2,000 seconds. The analysis also revealed that the radial stress reached a maximum value at the end of each cycle as the axial compression was released and the specimen was cooled.
Advanced [gas] Turbine System - Conceptual Design [final rpt]