High stress capability, intermetallic phase titanium aluminide coated
components
    193.
    发明授权
    High stress capability, intermetallic phase titanium aluminide coated components 失效
    高应力能力,金属间相钛化铝涂层组件

    公开(公告)号:US5281484A

    公开(公告)日:1994-01-25

    申请号:US10312

    申请日:1993-01-28

    摘要: Coated components are produced to withstand high stresses and are composed of the intermetallic phase titanium aluminide material for use, in particular, in piston engines, gas turbines and exhaust gas turbochargers. This material has good technical properties but otherwise only a low resistance to oxidation and wear as a result of friction processes. These disadvantages are overcome in that the components are coated, at least on the parts of their surface which are at risk of hot corrosion and/or wear, with a sheet of a solderable nickel-based alloy soldered on under vacuum. A coating thickness of 0.1 to 0.4 mm is adequate. The nickel-based alloys, of which the soldered-on sheet is composed, preferably have a melting point of below 1180.degree. C.

    摘要翻译: 制造涂覆部件以承受高应力,并且由用于特别是活塞发动机,燃气轮机和废气涡轮增压器的金属间相铝化钛材料组成。 该材料具有良好的技术性能,但是由于摩擦过程而仅仅具有较低的耐氧化和耐磨性。 克服了这些缺点,因为在真空下焊接有可焊接的镍基合金的片材,至少在其表面上具有热腐蚀和/或磨损危险的部分被涂覆。 涂层厚度为0.1〜0.4mm就足够了。 构成焊接片材的镍基合金的熔点优选低于1180℃。