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公开(公告)号:US20120207611A1
公开(公告)日:2012-08-16
申请号:US13503209
申请日:2010-10-21
CPC分类号: B22D13/04 , B22C9/02 , B22C9/04 , B22D13/102 , B22D21/005 , C22C14/00
摘要: A method of production of a component having at least one dimension that is more than 200 mm, said method comprising the steps of: a) providing a titanium aluminide melt; b) providing a cold sand casting mould; c) mounting the mould and the melt in a vacuum or inert atmosphere chamber; d) rotating the mould at a distance from a rotation axis to generate an artificial gravity in all parts of the mould of at least 30 g; e) pouring the melt along said axis of rotation into a gateway that leads the melt to a radius greater than a maximum radius of any part of the mould, the gateway being arranged to open into the mould in a direction contrary to that of said artificial gravity; f) wherein said pouring is at a speed that fills the mould in less than 5 seconds. The method is useful for the casting of long turbine airfoils used in electricity generation industry or large automotive turbocharger wheels.
摘要翻译: 一种制备具有至少一个尺寸大于200mm的部件的方法,所述方法包括以下步骤:a)提供钛酸铝熔体; b)提供冷砂铸造模具; c)将模具和熔体安装在真空或惰性气氛室中; d)使模具旋转一定距离旋转轴线,以在模具的所有部分产生至少30g的人造重力; e)将熔体沿所述旋转轴倾倒入网关中,所述网关将所述熔体引导到大于所述模具的任何部分的最大半径的半径,所述网关被布置成沿与所述人造的方向相反的方向打开到所述模具中 重力; f)其中所述浇注的速度是在不到5秒内填充模具的速度。 该方法可用于铸造用于发电行业或大型汽车涡轮增压轮的长涡轮机翼型。