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Microstructural design and mechanical properties of a cast and heat-treated intermetallic multi-phase y-TiAl based alloy

机译:铸造和热处理的金属间多相y-TiAl基合金的显微组织设计和力学性能

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摘要

Advanced intermetallic multi-phase y-TiAl based alloys, such as TNM alloys with a nominal composition of Ti-43.5Al-4Nb-lMo-0.1B (in at.%), are potential candidates to replace heavy Ni-base superalloys in the next generation of aircraft and automotive combustion engines. Aimed components are turbine blades and turbocharger turbine wheels. Concerning the cost factor arising during processing, which -additionally to material costs - significantly influences the final price of the desired components, new processing solutions regarding low-cost and highly reliable production processes are needed. This fundamental study targets the replacement of hot-working, i.e. forging, for the production of turbine blades. But without forging no grain refinement takes place by means of a recrystallization process because of the lack of stored lattice defects. Therefore, new heat treatment concepts have to be considered for obtaining final microstructures with balanced mechanical properties in respect to sufficient tensile ductility at room temperature as well as high creep strength at elevated temperatures. This work deals with the adjustment of microstructures in a cast and heat-treated TNM alloy solely by exploiting effects of phase transformations and chemical driving forces due to phase imbalances between different heat treatment steps and compares the mechanical properties to those obtained for forged and heat-treated material.
机译:先进的金属间多相y-TiAl基合金,例如标称成分为Ti-43.5Al-4Nb-1Mo-0.1B(以原子%计)的TNM合金,是替代重金属Ni基超合金的潜在选择。下一代飞机和汽车内燃机。瞄准的组件是涡轮叶片和涡轮增压器涡轮。关于在加工过程中产生的成本因素,除了材料成本外,还会显着影响所需组件的最终价格,因此需要有关低成本和高度可靠的生产工艺的新加工解决方案。这项基础研究的目标是代替热加工即锻造来生产涡轮叶片。但是由于没有储存的晶格缺陷,因此在没有锻造的情况下,没有通过再结晶过程进行晶粒细化。因此,必须考虑新的热处理概念,以获得在室温下具有足够的拉伸延展性以及在高温下具有高蠕变强度的,具有平衡机械性能的最终微结构。这项工作仅通过利用由于不同热处理步骤之间的相平衡而产生的相变和化学驱动力,来处理铸造和热处理过的TNM合金的微观结构,并将其机械性能与锻造和热处理后的力学性能进行比较。处理过的材料。

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