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1.发明授权Aerodynamic profile for aircraft and wind power stations and method of measuring the thickness of ice on an aerodynamic profile 有权飞机和风力发电站的空气动力学特性以及测量空气动力学特性中冰的厚度的方法公开(公告)号：US08434365B2
公开(公告)日：2013-05-07
申请号：US12280770
申请日：2007-02-26
CPC分类号： B64D15/20 , F03D80/40 , G01B17/025 , Y02E10/72
摘要： An aerodynamically shaped profile member for aircraft and wind power stations includes, for example, phased-array ultrasonic generator arrangement arranged therein. During operation of the profile member, the ultrasonic generator emits ultrasonic waves in a targeted manner in multiple directions to determine a profile of the thickness of an ice layer on the surface of the aerodynamic profile. The structure may be, for example, a composite fiber material arranged around a foam core, with the ultrasonic generator arrangement being laminated into the composite fiber material. For measurement of the ice thickness, ultrasonic waves are transmitted in a targeted manner to different positions of the surface of the aerodynamic profile, and the ultrasonic waves reflected on the interfaces of the ice layer are detected. At least one region of the surface is scanned by means of the targeted ultrasonic waves, to determine an ice thickness profile.
摘要翻译： 用于飞机和风力发电站的空气动力学形状的构件包括例如布置在其中的相控阵超声波发生器装置。 在轮廓构件的操作期间，超声波发生器以多个方向以目标方式发射超声波，以确定空气动力学轮廓表面上的冰层的厚度分布。 该结构可以是例如布置在泡沫芯周围的复合纤维材料，其中超声波发生器装置被层压到复合纤维材料中。 为了测量冰厚度，超声波以目标方式传播到空气动力学轮廓表面的不同位置，并且检测在冰层的界面上反射的超声波。 通过目标超声波扫描表面的至少一个区域，以确定冰厚度分布。
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2.发明申请Aerodynamic Profile for Aircraft and Wind Power Stations and Method of Measuring the Thickness of Ice on an Aerodynamic Profile 有权飞机和风力发电站的空气动力学参数和测量空气动力学剖面上的冰厚度的方法公开(公告)号：US20090189020A1
公开(公告)日：2009-07-30
申请号：US12280770
申请日：2007-02-26
IPC分类号： B64D15/20
CPC分类号： B64D15/20 , F03D80/40 , G01B17/025 , Y02E10/72
摘要： An aerodynamically shaped profile member for aircraft and wind power stations includes, for example, phased-array ultrasonic generator arrangement is arranged therein. During operation of the profile member, the ultrasonic generator emits ultrasonic waves in a targeted manner in multiple directions to determine a profile of the thickness of an ice layer on the surface of the aerodynamic profile. The structure may be, for example, a composite fiber material arranged around a foam core, with the ultrasonic generator arrangement being laminated into the composite fiber material. For measurement of the ice thickness, ultrasonic waves are transmitted in a targeted manner to different positions of the surface of the aerodynamic profile, and the ultrasonic waves reflected on the interfaces of the ice layer are detected. At least one region of the surface is scanned by means of the targeted ultrasonic waves, to determine an ice thickness profile.
摘要翻译： 用于飞机和风力发电站的空气动力学形状的构件包括例如相关阵列超声波发生器装置。 在轮廓构件的操作期间，超声波发生器以多个方向以目标方式发射超声波，以确定空气动力学轮廓表面上的冰层的厚度分布。 该结构可以是例如布置在泡沫芯周围的复合纤维材料，其中超声波发生器装置被层压到复合纤维材料中。 为了测量冰厚度，超声波以目标方式传播到空气动力学轮廓表面的不同位置，并且检测在冰层的界面上反射的超声波。 通过目标超声波扫描表面的至少一个区域，以确定冰厚度分布。
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