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Development of Diffusion Barriers for the Superalloy Blades of Gas Turbine

机译:燃气轮机高温合金叶片扩散壁垒的研制

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Nickel base superalloys are normally protected against high temperature oxidation by MCrAlY type overlays. The diffusion of Ni from the superalloy and that of Al from the overlay causes, however, structural changes capable of causing spall off of the protectng layer. In a programme of the European concerted action cOST 501/II, the development of diffusion barriers for the temperature range of 1000-1100 deg C was started, and then continued in a BRITE-EURAM project, which has been concentrating on developing suitable bondings for the most promising diffusion barriers. On the basis of laboratory scale tests, suitable candidates for the diffusion barriers as well as for their bondings towards superalloys and the overaly have been found. These candidates will be tested during the last portion of the project on real blades in real gas turbine conditions.
机译:镍基高温合金通常通过MCrAlY型覆盖层进行保护,以防高温氧化。但是,Ni从超合金中扩散出来,Al从覆盖层中扩散出来,但会引起结构变化,从而引起保护层剥落。在欧洲共同行动cOST 501 / II的程序中,开始开发1000-1100℃温度范围内的扩散阻挡层,然后在BRITE-EURAM项目中继续进行,该项目一直致力于为以下方面开发合适的粘接剂:最有前途的扩散壁垒。在实验室规模的测试基础上,已经找到了合适的候选材料,用于扩散壁垒以及它们与高温合金和整体合金的结合。这些候选对象将在项目的最后一部分中在真实燃气轮机条件下的真实叶片上进行测试。

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