发明名称 Improvements in erosion resistant flame-sprayed coatings
摘要 <p>A metal base is protected by applying thereto a corrosion-resistant layer of uncured liquid adhesive synthetic resin, curing the layer, and applying a flame-sprayed metal layer thereover, followed by an impact-resistant flame-sprayed layer of at least one hard metal, e.g. tungsten or molybdenum, refractory metal carbide, fused metal oxide, or combination of silicon dioxide with at least one metal oxide. A powdered metal, e.g. aluminium or aluminium alloy, may be applied to the surface of the resin, which may be an epoxy resin, prior to curing, or it may be incorporated in the layer before application, the resin layer afterwards being treated to expose the particles. A final layer of synthetic resin, e.g. epoxy resin, may be applied over the impact-resistant layer. The metal base, e.g. an aluminium alloy blade, may be anodized or primed, e.g. chromate- or etch-primed, before coating. The protective layers are removable by a resin degrading material. Specification 745,257 is referred to.ALSO:A metal base is protected by applying thereto a corrosion-resistant layer of uncured liquid adhesive synthetic resin, curing the layer, and applying a flame-sprayed metal layer thereover, followed by an impact-resistant flame-sprayed layer of at least one hard metal, e.g. tungsten or molybdenum, refractory metal carbide, fused metal oxide or combination of silicon dioxide with at least one metal oxide. A powdered metal, e.g. aluminium or aluminium alloy, may be applied to the surface of the resin, which may be an epoxy resin, prior to curing, or it may be incorporated in the resin before application, the resin layer afterwards being treated to expose the particles. A final sealing coating of synthetic resin, e.g. epoxy resin, may be applied over the impact-resistant layer. The metal base, e.g. an aluminium alloy blade, may be anodized or primed, e.g. chromate- or etch-primed, before coating. The protective layers are removable by a resin-degrading material. Specification 745,257 is referred to.</p>
申请公布号 GB951231(A) 申请公布日期 1964.03.04
申请号 GB19590011885 申请日期 1959.04.08
申请人 THE DE HAVILLAND AIRCRAFT COMPANY LIMITED;NORTON GRINDING WHEEL COMPANY LIMITED 发明人 SWINGLER RALPH FRANCIS NEWMAN;TEAGUE ERNEST DOUGLAS
分类号 B05D1/10;B05D3/02;B05D7/14;B32B15/08;B64C3/26;B64C11/20;C23C4/02;C23C4/10 主分类号 B05D1/10
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