首页> 外国专利> Producing brake discs made of aluminum-matrix composite alloy, comprises heating spray-formed base-aluminum-matrix composite alloy having specified amount of silicon carbide particle in matrix-forming aluminum alloy in fusion mold

Producing brake discs made of aluminum-matrix composite alloy, comprises heating spray-formed base-aluminum-matrix composite alloy having specified amount of silicon carbide particle in matrix-forming aluminum alloy in fusion mold

机译:生产由铝基复合合金制成的制动盘,包括在熔模中在基体形成铝合金中加热喷射成形的具有指定量碳化硅颗粒的基铝铝基复合合金

摘要

The process comprises: providing a spray-formed base-aluminum-matrix composite alloy having a proportion of silicon carbide particle (12-25 vol.%) in a matrix-forming aluminum alloy; heating the base-aluminum-matrix composite alloy up to a solidus temperature of the matrix-forming aluminum alloy under inert gas atmosphere in a fusion mold (5) with a cylindrical cavity, which has a diameter corresponding to the brake discs, in a pressure chamber (7), where a rotation axis of the cylindrical cavity is vertically aligned; and structuring a gas pressure of 1200-2000 bar in the pressure chamber. The process comprises: providing a spray-formed base-aluminum-matrix composite alloy having a proportion of silicon carbide particle (12-25 vol.%) in a matrix-forming aluminum alloy; heating the base-aluminum-matrix composite alloy up to a solidus temperature of the matrix-forming aluminum alloy under inert gas atmosphere in a fusion mold (5) with a cylindrical cavity, which has a diameter corresponding to the brake discs, in a pressure chamber (7), where a rotation axis of the cylindrical cavity is vertically aligned; structuring a gas pressure of 1200-2000 bar in the pressure chamber; again heating the base-aluminum-matrix composite alloy over a liquidus temperature of the matrix-forming aluminum alloy and melting the aluminum alloy for applying the aluminum-matrix composite alloy heated over the liquidus temperature with the gas pressure; creating vibrations by a vibration source (6) and introducing the vibrations into the fusion mold; allowing the vibrations on the melt of the matrix-forming aluminum alloy for a certain period of time to reduce a viscosity of the melt and to reduce a gravity of a laser of the silicon carbide particles; enriching the silicon carbide particles in a lower layer of the melt present in the fusion mold and enriching a second layer of the silicon carbide particle located above the first layer; deterring the melt in the fusion mold in the pressure chamber under the gas pressure and solidifying the laser to a cylindrical aluminum-matrix composite alloy semi finished product (1) having the first layer enriched with the silicon carbide particle (45 vol.%) and having the second layer enriched with the silicon carbide particle; demolding the aluminum-matrix composite alloy semi finished product; performing a metal-cutting machining process of the aluminum-matrix composite alloy semi finished product to remove the second layer enriched with the silicon carbide particle and to remove the first layer as a cylindrical brakediscs-semifinished product with the aluminum-matrix composite alloy (40 vol.%) provided for the brake disc enriched with the silicon carbide particle; and finally machining the brake disc semi finished product to the brake disc. The machining step comprises separating the brake discs semi-finished product into the brake discs and/or performing a heat-treatment of the brake disc semi-finished product or the brake disc by a T6-heat treatment with solution annealing and artificial aging. The vibration source is proximally arranged to the cavity of the fusion mold, and is a compressed air vibrator or an ultrasonic transmitter. The method further comprises compressing the base-aluminum-matrix composite alloy by hipping, hot forging, extruding, and/or hot rolling before heating the base-aluminum-matrix composite alloy, mechanically machining the base-aluminum-matrix composite alloy, and adjusting a desired composition of the first layer by adjusting a pressure and/or a temperature exposure period of 30-120 minutes and/or by adjusting the temperature (640[deg] C) as a function of the liquidus temperature of the matrix-forming aluminum alloy. An independent claim is included for a brake disc.
机译:该方法包括:提供在基质形成铝合金中具有一定比例的碳化硅颗粒(12-25vol。%)的喷射成型的基础-铝-基质复合合金;和在具有圆筒形腔体的熔融模具(5)中,在惰性气体气氛下,在惰性气体气氛下,在压力下将基础铝基复合材料合金加热到形成基质的铝合金的固相线温度。腔(7),圆柱腔的旋转轴线垂直对准;在压力室中构造一个1200-2000 bar的气压。该方法包括:提供在基质形成铝合金中具有一定比例的碳化硅颗粒(12-25vol。%)的喷射成型的基础-铝-基质复合合金;和在具有圆筒形腔体的熔融模具(5)中,在惰性气体气氛下,在惰性气体气氛下,在压力下将基础铝基复合材料合金加热到形成基质的铝合金的固相线温度。腔(7),圆柱腔的旋转轴线垂直对准;在压力室内构造气压为1200-2000 bar;再次在形成基质的铝合金的液相线温度下加热基础-铝-基质复合合金,并熔化铝合金,以在气压下施加在液相线温度以上加热的铝-基质复合合金。通过振动源(6)产生振动,并将振动引入融合模具中;使形成基质的铝合金的熔体振动一定时间,以降低熔体的粘度并减小碳化硅颗粒的激光的重力;在存在于熔融模具中的熔体的下层中富集碳化硅颗粒,并且富集位于第一层上方的第二层碳化硅颗粒;在气压下在压力室中的熔融模具中确定熔体,并将激光固化为圆柱形的铝基复合合金半成品(1),其第一层富含碳化硅颗粒(45%(体积));使第二层富含碳化硅颗粒;脱模铝基复合合金半成品;对铝基复合合金半成品执行金属切削加工工艺,以去除富含碳化硅颗粒的第二层,并去除铝基复合合金作为圆柱形制动盘半成品的第一层(40 (vol。%)提供给富含碳化硅颗粒的制动盘;最后将制动盘半成品加工成制动盘。加工步骤包括将制动盘半成品分离成制动盘和/或通过T6热处理并通过固溶退火和人工时效对制动盘半成品或制动盘进行热处理。振动源在近端布置在融合模具的腔体上,并且是压缩空气振动器或超声波发射器。该方法还包括在加热基础-铝-基质复合合金之前,通过翘曲,热锻,挤压和/或热轧来压缩基础-铝-基质复合合金,对基础-铝-基质复合合金进行机械加工,并进行调节。通过调节30-120分钟的压力和/或温度暴露时间和/或通过调节温度(640℃)作为形成基质的铝的液相线温度的函数,使第一层具有所需的第一层组成合金。制动盘包含独立索赔。

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