Suspension Sprayed YSZ Thermal Barrier Coatings on Inconel 718 Aerospike Manufactured by Laser Powder Bed Fusion

F. Toma, S. Gruber, A. Selbmann, C. Leyens, Martin Propst, T. Dorau
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Abstract

Additive Manufacturing (AM) processes offer geometrical freedom to design complex shaped parts that cannot be manufactured with conventional processes. This leads to new applications including aerospace propulsion systems where the Ni-superalloy based material has to withstand high operating temperatures. In this contribution suspension plasma sprayed YSZ TBC coating was applied on the spike contour of an additively manufactured aerospike engine demonstrator. The engine was designed for a hydrogen peroxide / kerosene 6 kN thrust at 2.0 MPa chamber pressure and was manufactured from nickel-based superalloy Inconel 718 powder using the laser powder bed fusion process (LPBF). Due to the novelty of the application of suspension sprayed YSZ thermal protection coatings on additively manufactured Inconel 718 components, extensive tests were necessary to characterize the interaction between the coating and the component.
悬浮喷涂YSZ热障涂层在激光粉末床熔合生产的Inconel 718航空钉上的应用
增材制造(AM)工艺为设计传统工艺无法制造的复杂形状零件提供了几何自由度。这导致了新的应用,包括航空航天推进系统,其中镍高温合金基材料必须承受高工作温度。在增材制造的航空发动机验证机的尖峰轮廓上,应用悬浮等离子喷涂YSZ TBC涂层。该发动机的推力为过氧化氢/煤油6 kN,室压为2.0 MPa,发动机材料为镍基高温合金Inconel 718粉末,采用激光粉末床熔合工艺(LPBF)制造。由于悬浮喷涂YSZ热防护涂层在增材制造的Inconel 718部件上应用的新颖性,需要进行大量的测试来表征涂层与部件之间的相互作用。
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