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Каталог домашних принадлежностей: лампы, светильники, столики и т. д. contents 22 ACCESSORIES:96 FURNITURE112 backyard PATIO116 LIGHTING:128 WALL DECOR:24 SCULPTURAL gadgets: ANIMALS // 32 VARIOUS46 VASES AND BOWLS62 CANDLEHOLDERS76 CONTAINERS80 TRAYS90 ornamental items: FILLERS //92 BOOKENDS // ninety four HEARTH118 LAMPS126 CHANDELIERS AND PENDANTS130 MIRRORS138 add-ons
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Extra resources for Advanced [gas] Turbine System - Conceptual Design [final rpt]
B. , 1992, Chapter 8, Elsevier Science Publishers, London. 3. G. R. Leverant, Private communication 4. H. L. Bernstein, Life Management System for General Electric Frame 7E Gas Turbine, R. Viswanathan and J. M. , eds Life Assessment and Repair Technology for Combustion Turbine Hot Section Components, ASM International, Materials Park, Ohio, 1990, 111-118 5. W. 0 Ni Bal. Bal. Bal. Appendix 1 Figure 1: Picture of CMSX-4 single crystal bars undergoing TMF testing. 13 Appendix 1 Load Load Cell Induction Coil Strain Temperature Controller Servo Controller Cycle Timer Figure 2: Control system used for TMF testing of metallic systems.
It should be noted that in this analysis no specific failure criterion was established for the TBC, and the process of crack formation and subsequent propagation was not analyzed. However, some indications of the failure mechanism can be 8 Appendix 1 determined from analysis of the behavior of testpieces coated with TBC which were exposed in a burner rig and which have also been analyzed by the FE method. In this case cracks form above the peaks in the bondcoat t and the FE calculations predict that the stresses in the valleys change from compression to tension during exposure in the burner rig and cracks then propagate from peak to peak through regions of tensile stress until fracture occurs.
6%. SV-34 coatings showed the best results for and overlay (LPPS) coating. Since both coatings have similarly low levels of ductility at lower temperatures the superior performance of SV-34 is presumably due to the higher strength of this Re-containing coating. The surprising feature of these results is the relatively good performance of the testpieces with aluminide coatings including those with SV-20 over-aluminided with SiPdAl, particularly at the higher strain ranges. The aluminide coatings are thinner so that when the cracks form during testing they are shorter than the cracks in the overlay coatings and the stress intensity at the crack tip is presumably lower.