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OXIDATION RESISTANT COATED NIOBIUM-BASE ALLOY AND ITS MANUFACTURING METHOD

机译:耐氧化涂层铌基合金及其制备方法

摘要

PROBLEM TO BE SOLVED: To solve the following problem: a niobium-base alloy is expected as a material used under a high temperature to improve the thermal efficiency of an aircraft engine or thermal power generation because of its melting point approximately 1,000°C higher than that of a nickel-base alloy, but the alloy is insufficient in oxidation resistance and a conventional oxidation resistant coating hardly prevents its deterioration due to interdiffusion between the alloy and the coating layer.;SOLUTION: An aluminum foil is laid on a base-material of niobium-base alloy, and a powder of a chemical compound, which forms an alumina protective coating film at a high temperature an has a linear expansion coefficient of 6-10 ppm/K, is further laid on the aluminum foil. The above overlapped materials are subjected to press sintering under a pressure of 20-80 MPa in the atmosphere of vacuum or argon gas and the aluminum foil under sintering absorbs a trace amount of oxygen in its periphery to form an alumina layer. Thereby, the oxidation resistant coated niobium- alloy having a double layer structure, where the alumina layer is interposed between the niobium-base alloy base-material and an outside coating layer forming the alumina protective coating at a high temperature and exhibiting an excellent oxidation resistance, is obtained.;COPYRIGHT: (C)2003,JPO
机译:要解决的问题:解决以下问题:铌基合金由于熔点高约1,000℃,因此有望在高温下用于提高飞机发动机或热力发电的热效率。与镍基合金相比,该合金的抗氧化性不足,并且常规的抗氧化涂层很难防止由于合金与涂层之间的相互扩散而导致其劣化。;解决方案:将铝箔铺设在基体上-进一步在铝箔上放置一层铌基合金材料和一种化合物粉末,该粉末在高温下形成氧化铝保护涂层膜,其线性膨胀系数为6-10 ppm / K。在真空或氩气气氛中,在20-80MPa的压力下对上述重叠的材料进行加压烧结,并且在烧结下的铝箔在其周围吸收痕量的氧以形成氧化铝层。从而,具有双层结构的抗氧化涂层的铌合金,其中氧化铝层在高温下介于铌基合金基材和形成氧化铝保护涂层的外涂层之间,并且表现出优异的抗氧化性;;版权所有:(C)2003,JPO

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