首页> 外国专利> Adjustable guide vane for turbine of turbocharger, has carrier ring that is formed from material with low expansion coefficient and high thermal conductivity to reduce first gap

Adjustable guide vane for turbine of turbocharger, has carrier ring that is formed from material with low expansion coefficient and high thermal conductivity to reduce first gap

机译:用于涡轮增压器涡轮的可调导向叶片,具有由低膨胀系数和高导热率的材料制成的托环,以减小第一间隙

摘要

The guide vane has a carrier ring (10) that is rotatably provided with several guide vanes (11). The carrier ring is arranged opposite to a contour of a sleeve (12) so that the guide vanes are rotatably positioned between the carrier ring and contour of the sleeve. A first gap (13) is formed between the contour of the sleeve and vanes. A second gap (14) is formed between the carrier ring and vanes. The carrier ring is formed from a material with low expansion coefficient and high thermal conductivity to reduce the first gap.
机译:导向叶片具有承载环(10),该承载环可旋转地设置有多个导向叶片(11)。支承环与套筒(12)的轮廓相对地布置,使得导向叶片可旋转地定位在支承环与套筒的轮廓之间。在套筒的轮廓和叶片的轮廓之间形成第一间隙(13)。在承载环和叶片之间形成第二间隙(14)。支承环由具有低膨胀系数和高导热率的材料形成,以减小第一间隙。

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