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LAYER COMPOSITE MATERIAL AND METHOD FOR IMPROVING THE SURFACE HARDNESS OF LAYER COMPOSITE MATERIALS

机译:层状复合材料及提高层状复合材料表面硬度的方法

摘要

PCT No. PCT/DE97/00453 Sec. 371 Date Sep. 25, 1998 Sec. 102(e) Date Sep. 25, 1998 PCT Filed Mar. 8, 1997 PCT Pub. No. WO97/36112 PCT Pub. Date Oct. 2, 1997A laminated composite material, and a method of improving the surface hardness of laminated composite materials, wherein selected regions of the carrier material of the laminated composite system are treated with high-energy beams, and the temperature control is designed in such a manner that the rays penetrate into a maximum a 0.1-fold the entire thickness of the carrier material. The temperature increase in the region of the sliding material is a maximum of 80% of the melting temperature of the lowest melting constituent of said material. The laminated composite material with a rear steel substrate surface can be post-hardened. The steel substrate has at least in one part of the surface facing away from the function layer a level of hardness increased by a factor of 1.5 or more than at a depth which corresponds substantially to 0.1-fold of the thickness of the steel substrate.
机译:PCT号PCT / DE97 / 00453第二部分371日期1998年9月25日102(e),1998年9月25日,PCT,1997年3月8日提交。 WO97 / 36112 PCT公开日期:1997年10月2日,一种层压复合材料,以及一种改善层压复合材料表面硬度的方法,其中用高能束处理层压复合系统的载体材料的选定区域,并设计温度控制装置。这样,光线最多可以穿透载体材料整个厚度的0.1倍。滑动材料区域中的温度升高最大为所述材料的最低熔融成分的熔融温度的80%。具有钢制后表面的层压复合材料可以进行后硬化处理。该钢基底的至少一部分背对功能层的表面的硬度水平增加了1.5倍或更多倍,其深度基本上等于该钢基底厚度的0.1倍。

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