首页> 外文会议>TMS(The Minerals, Metals Materials Society) Annual Meeting >Development of CVD overaluminising process on different CoNiCrAlY bond coats deposited by Vacuum Plasma Spray (VPS), Low Pressure Plasma Spray (LPPS) and High Velocity Oxygen Fuel (HVOF)
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Development of CVD overaluminising process on different CoNiCrAlY bond coats deposited by Vacuum Plasma Spray (VPS), Low Pressure Plasma Spray (LPPS) and High Velocity Oxygen Fuel (HVOF)

机译:在真空等离子喷涂(VPS),低压等离子喷涂(LPPS)和高速氧气燃料(HVOF)沉积的不同CoNiCrAlY键合涂层上进行CVD过铝化工艺的开发

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Coating technology is progressing at a steady rate with continuous significant improvements in the coatings performance. In the aerospace field, as well as in the stationary gas turbine field, coatings deposited by different processes (thermal spray, CVD, EBPVD) play an important role in order to increase the performances of the engines. In particular, in order to improve the resistance to oxidation and corrosion at high temperature, aluminium is deposited by several processes (pack aluminising, above the pack and CVD) in alternative or addition to thermal spray coatings (mainly MCrAlY alloys where M stands for Co, Ni or CoNi). These MCrAlY coatings are generally deposited by Low Pressure Plasma Spray (LPPS) or Vacuum Plasma Spray (VPS), but also by High Velocity Oxygen Fuel (HVOF) and Air Plasma Spray (APS), which may also be required for their lower cost, even though it is commonly held that the quality of MCrAlY coatings deposited by HVOF or APS is lower because of the partial oxidation that the materials undergoes while being sprayed. This paper addresses the study of aluminium coatings deposited by CVD on CoNiCrAlY bond coats deposited by Low Pressure Plasma Spray (LPPS), Vacuum Plasma Spray (VPS) and High Velocity Oxygen Fuel (HVOF). The aim was to determine if the CoNiCrAlY coating structures obtained by these processes with different content of oxides and porosity could affect the deposition rate and quality of the Al coatings. The obtained samples have been characterized from the metallographic point of view in order to determine porosity, thickness and structure of both CoNiCrAlY and Al coatings by means of metallographic and scanning electron microscopy. Al coating thickness has been taken as parameter in order to define the Al coating deposition rate on the different CoNiCrAlY coatings. Surface roughness and morphology of the samples has been studied on CoNiCrAlY surface before and after Al deposition in order to determine how the Al coating affect the surface morphology. Oxidation test has been performed on overaluminised CoNiCrAlY coatings.
机译:随着涂料性能的不断显着提高,涂料技术正在以稳定的速度发展。在航空航天领域以及固定式燃气轮机领域,通过不同工艺(热喷涂,CVD,EBPVD)沉积的涂层起着重要的作用,以提高发动机的性能。特别是,为了提高高温下的抗氧化和抗腐蚀能力,铝可以通过多种工艺(在包装上进行镀铝,在包装上和CVD)沉积或替代热喷涂涂层(主要是MCrAlY合金,其中M代表Co ,Ni或CoNi)。这些MCrAlY涂层通常通过低压等离子喷涂(LPPS)或真空等离子喷涂(VPS)沉积,但也可以通过高速氧气燃料(HVOF)和空气等离子喷涂(APS)沉积,这也可能是因为它们的成本较低,尽管通常认为,HVOF或APS沉积的MCrAlY涂层的质量较低,因为该材料在喷涂时会发生部分氧化。本文研究了在低压等离子喷涂(LPPS),真空等离子喷涂(VPS)和高速氧气燃料(HVOF)沉积的CoNiCrAlY粘结涂层上通过CVD沉积的铝涂层的研究。目的是确定通过这些方法获得的具有不同氧化物含量和孔隙率的CoNiCrAlY涂层结构是否会影响Al涂层的沉积速率和质量。从金相学角度对获得的样品进行了表征,以便通过金相学和扫描电子显微镜确定CoNiCrAlY和Al涂层的孔隙率,厚度和结构。为了确定在不同的CoNiCrAlY涂层上的Al涂层沉积速率,已将Al涂层厚度作为参数。在铝沉积之前和之后的CoNiCrAlY表面上研究了样品的表面粗糙度和形貌,以确定铝涂层如何影响表面形貌。已对过铝化的CoNiCrAlY涂层进行了氧化测试。

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