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Development of TBCs for Advanced-Ultra Supercritical Steam Turbine System

机译:高级超超临界汽轮机系统开发TBCS

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We have developed a coal-fired advanced-ultra super critical steam turbine system (A-USC) for several years. The temperature of re-heated steam in the A-USC system is 700-720 °C. Many high temperature components in the A-USC system should be produced by Ni-based superalloys. Nozzle box is one of the hot components in the high pressure turbine. We have investigated feasible TBCs to reduce the thermal stress in the nozzle box. Since a remarkably high heat resistance is required, the target values of the thermal conductivity and the thickness of the topcoat are 1 W/mK and over 3 mm, respectively. In order to satisfy the specification, we have developed the TBCs with a porous and ultra-thick YSZ topcoat by APS process. The processing parameters are carefully controlled to suppressing the thermal stress during deposition process. As results of the tests for fundamental properties in laboratory, the ultra-thick TBCs shows a enough performance as the TBCs applied to the nozzle box. The several coating tests by the use of mock-up specimens were also carried out.
机译:我们已经开发了一种燃煤高级超级关键汽轮机系统(A-USC)几年。 A-USC系统中重新加热蒸汽的温度为700-720°C。 A-USC系统中的许多高温分量应由Ni基超合金生产。喷嘴盒是高压涡轮机中的热部件之一。我们已经调查了可行的TBC,以减少喷嘴箱中的热应力。由于需要具有显着高的耐热性,因此热导率的目标值和面涂层的厚度分别为1W / mk,超过3mm。为了满足规范,我们通过APS工艺开发了具有多孔和超厚YSZ面漆的TBC。仔细控制处理参数以在沉积过程中抑制热应力。随着实验室基本性质的测试结果,超厚的TBC显示出足够的性能,因为施加到喷嘴盒的TBC。还进行了几种涂层测试,也进行了使用模拟标本。

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