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ASSEMBLY OF AEROFOIL-SHAPED BODY AND NOISE REDUCING SERRATION AND WIND TURBINE PROVIDED THEREWITH

机译:翼型体的组装及其降噪锯齿和风轮机

摘要

An assembly is provided of, firstly, an aerofoil-shaped body, such as a wing of an airplane or a rotor blade of a wind turbine, having a trailing edge and, secondly, a noise reducing serration extending along at least part of said trailing edge. The serration comprises a base plate defining a first edge connected to the aerofoil-shaped body near to said trailing edge and a second edge having attached thereto a number of teeth defining tips facing away from the base plate. The base plate is located behind the trailing edge and is separated therefrom by a gap wherein the connection between the base plate and aerofoil-shaped body is defined by at least one tape-like member made of a material which allows the tape-like member to bend, stretch and buckle. The serration in such a manner is stiff against bending but weak against torsion that in a range of expected operational loads the serration is not able to bend substantially, whereas in said range of expected operational loads the base plate is able to twist.
机译:提供一种组件,该组件首先具有翼型形的主体,例如飞机的机翼或风力涡轮机的转子叶片,其具有后缘,其次,该噪声的锯齿沿着所述后缘的至少一部分延伸边缘。该锯齿包括基板,该基板限定了在所述后缘附近连接到翼型形体的第一边缘和第二边缘,该第二边缘附接有多个齿,这些齿限定了背对基板的尖端。基板位于后缘的后面,并且通过一间隙与之隔开,其中,基板与翼型体之间的连接由至少一个由带状材料制成的带状构件限定,该材料由带状构件制成。弯曲,伸展和扣紧。锯齿以这种方式抵抗弯曲是刚性的,但是抵抗扭转是微弱的,以致在预期的工作负载范围内,锯齿基本上不能弯曲,而在预期的工作负载范围内,基板能够扭曲。

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