首页> 外文会议>TMS 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:在真空等离子体喷雾(VPS),低压等离子体喷雾(LPP)和高速氧气燃料(HVOF)沉积的不同聚焦粘结涂层上的CVD透析过程。

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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. From the metallographic characterisation the content of oxygen in the different CoNiCrAlY coating does not vary in significant way, the values of the CVD Al thickness are quite similar independently by the process used for the deposition of CoNiCrAlY. The low difference in oxygen content in the CoNiCrAlY coating does not affect substantially the deposition of Al by CVD. The oxidation tests show how the aluminium coatings "protects" the underlaying CoNiCrAlY coatings: no significant differences are notable in the oxide growth after the oxidation test.
机译:涂层技术以稳定的速率进展,涂料性能持续显着改善。在航空航天领域,以及固定式燃气轮机场,由不同工艺(热喷涂,CVD,EBPVD)沉积的涂层起到重要作用,以增加发动机的性能。特别地,为了改善高温耐氧化和腐蚀的耐腐蚀,铝通过替代或添加到热喷涂涂层(主要是McRaly合金)的替代或添加到CCraly合金中的铝合金,在其中铝合金,ni或coni)。这些麦克利涂层通常由低压等离子体喷雾(LPP)或真空等离子体喷雾(VPS)沉积,而且还通过高速氧气燃料(HVOF)和空气等离子体喷雾(AP),这也可能需要较低的成本,尽管通常认为,由于材料在喷射时经历的部分氧化而沉积的McRaly涂层的质量较低。本文介绍了CVD沉积的CVD涂层的铝涂层的研究,低压等离子体喷雾(LPP),真空等离子体喷雾(VPS)和高速氧气燃料(HVOF)进行了沉积的Coicraly键涂层。目的是确定通过氧化物和孔隙率不同的这些方法获得的同色性涂层结构可以影响Al涂层的沉积速率和质量。所获得的样品已经从金相的视角表征,以通过金相和扫描电子显微镜测定同色子和Al涂层的孔隙率,厚度和结构。已作为参数涂层厚度,以便在不同的同胞涂层上定义Al涂层沉积速率。在Al沉积之前和之后,研究了样品的表面粗糙度和形态,以确定Al涂层如何影响表面形态学。已经对氧化氧化试验进行了逾越化的同色涂层。从金相表征,不同的上皮涂层中的氧气含量不显着的方式变化,CVD Al厚度的值独立于用于沉积对同胞沉积的方法。 Conicry涂层中的氧含量的低差异不会影响Al的CVD沉积。氧化试验展示了铝涂层的“保护”底层的外表涂层:在氧化试验后氧化物生长没有显着差异。

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