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AERODYNAMICALLY SHAPED BODY AND METHOD FOR COOLING BODY PROVIDED IN HOT FLUID FLOW

机译:气动成型体及热流中冷却体的方法

摘要

PROBLEM TO BE SOLVED: To provide a device for cooling an aerodynamically shaped body provided in a hot fluid flow.;SOLUTION: An aerodynamically shaped body 1 extends along a camber line 100 from a leading edge 11 to a trailing edge 12 and includes a coolant supply plenum. The coolant supply plenum is delimited by a wall of the body 1. The wall of the body 1 extends from a first side of the camber line 100 toward a second side of the camber line 100 and extends over the leading edge 11, so that a leading edge wall section is provided. A first leading edge cooling duct 20 extends from an inner surface to an outer surface, is in fluid communication with the coolant supply plenum through an inlet opening 21 and opens out onto the outer surface through a discharge opening 22. The inlet opening 21 is provided on the first side of the camber line 100, and the discharge opening 22 is provided on the second side of the camber line 100. The leading edge cooling duct 20 extends inside the wall from the first side of the camber line 100 toward the second side of the camber line 100 and crosses the camber line 100 in a leading edge 11 region.;SELECTED DRAWING: Figure 2;COPYRIGHT: (C)2017,JPO&INPIT
机译:解决的问题:提供一种用于冷却设置在热流体流中的空气动力学成形体的装置。解决方案:空气动力学成形体1沿着弧线100从前缘11延伸到后缘12,并且包括冷却剂供应气室。冷却剂供给室由主体1的壁界定。主体1的壁从弯度线100的第一侧向弯度线100的第二侧延伸并在前缘11上延伸,使得提供了前缘壁部分。第一前缘冷却管道20从内表面延伸到外表面,并通过入口开口21与冷却剂供给室流体连通,并通过排放开口22通向外表面。设置有入口开口21在弯度线100的第一侧上设置有排气口22,在弯度线100的第二侧上设置有排出口22。前缘冷却管道20从弯度线100的第一侧朝向第二侧在壁内延伸。弧度线100的横截面并在前缘11区域中与弧度线100交叉。;选定的图纸:图2;版权:(C)2017,JPO&INPIT

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