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Airfoil including a tip shape for reducing noise and method for making the airfoil

机译:包括用于减小噪音的尖端形状的翼型及其制造方法

摘要

An airfoil, a fan assembly and an unducted contra-rotating fan engine include fabricating at least one airfoil 72 including a suction 83 and a pressure 81 side coupled together at a leading 84 and a trailing 86 edge and extending therebetween. The airfoil includes a plurality of chord sections having a chord length 94. The airfoil including a tip profile 100 defining a reducing slope extending from the leading edge at the tip portion 88 along at least a portion of the chord length. The tip profile is configured to reduce the high unsteady pressure near the tip portion of the airfoil.
机译:翼型件,风扇组件和非导管式反向旋转风扇发动机包括制造至少一个翼型件72,该翼型件包括在前缘84和后缘86处联接在一起并在其间延伸的吸力83和压力81侧。翼型件包括具有翼弦长度94的多个翼弦部分。翼型件包括尖端轮廓100,尖端轮廓100限定了减小的倾斜度,该减小的倾斜度从尖端部分88的前缘沿着弦长的至少一部分延伸。尖端轮廓被构造成减小翼型的尖端部分附近的高的不稳定压力。

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