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DETAIL OF THE AIRCRAFT ENGINE, INCLUDING COATING FOR PROTECTION FROM EROSION, AND METHOD FOR PRODUCING SUCH DETAIL
DETAIL OF THE AIRCRAFT ENGINE, INCLUDING COATING FOR PROTECTION FROM EROSION, AND METHOD FOR PRODUCING SUCH DETAIL
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机译:飞机发动机的详细信息,包括用于防腐蚀的涂层以及产生这种详细信息的方法
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摘要
An aircraft engine-part including at least a metal substrate and a protective coating for protection against erosion that is present on the substrate, the coating including at least one phase including at least chromium at an atom content greater than or equal to 45% and carbon at an atom content lying in the range 5% to 20%, the phase including Cr7C3 and Cr23C6 chromium carbides. A method of fabricating such a part in which electroplating is used to deposit a coating composition on the part and the part is subjected to heat treatment at a temperature lying in the range 250° C to 70° C.
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机译:一种飞机发动机零件,包括至少一个金属基底和一个用于防止腐蚀的保护涂层,该保护涂层包括在基底上,该涂层包括至少一个相,该相至少包含原子含量大于或等于45%的铬和碳当原子含量在5%至20%的范围内时,该相包括Cr 7 C 3和Cr 23 C 6碳化铬。一种制造这种部件的方法,其中使用电镀将涂料组合物沉积在该部件上,并使该部件在250°C至70°C的温度范围内进行热处理。
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