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Experimental study on the ECM and PECM of pressed and casted γ-TiAl alloys for aero engine applications

机译:适用于Aero发动机应用的压制和铸造γ型合金ECM和PECM的实验研究

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Based on low density and excellent high-temperature performance, Gamma Titanium Aluminide (γ-TiAl) is adequate for high temperature structural material in aero engine components, such as turbine blades, compressor casings etc. However, due to low temperature ductility and fracture toughness, problems occur by machining these alloys with traditional cutting techniques. Electrochemical machining (ECM) is a reasonable alternative because of its specific process characteristics. Therefore, this paper focuses on the experimental research of electrochemical removal behaviour of typical new materials in aero engine applications. The theoretical calculation was used to compare and analyze the test results. Furthermore, experiments with precise ECM with vibration (PECM) were performed to improve surface roughness. From the results of the examined pressed and casted γ-TiAl alloys, having almost the same chemical composition, it is concluded that the more homogeneous the phase, the higher is the reachable material dissolving rate (v_a) and less energy is needed in order to get a same value of v_a. The cross-sections attest that the electrochemical process has no influence on the rim zone.
机译:基于低密度和优异的高温性能,伽马钛铝化物(γ电)适用于航空发动机部件的高温结构材料,如涡轮机叶片,压缩机壳体等,由于低温延展性和断裂韧性,通过用传统的切割技术加工这些合金来发生问题。电化学加工(ECM)是一种合理的替代方案,因为其特定的工艺特征。因此,本文侧重于航空发动机应用中典型新材料电化学去除行为的实验研究。理论计算用于比较和分析测试结果。此外,进行具有振动(PECM)的精确ECM的实验以改善表面粗糙度。从检查的压制和铸造γ-Tial合金的结果,结论是,阶段更加均匀,较高的可达材料溶解速率(V_A)越高,而且需要更少的能量获得相同的V_A值。横截面证明电化学过程对边缘区没有影响。

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