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Conformal antenna array formed on intersecting walls of a honeycomb structure and a method of making such an antenna array

机译:形成在蜂窝结构的相交壁上的共形天线阵列及其制造方法

摘要

A conformal antenna array 10 comprises a plurality of intersecting wall portions 12 supporting a plurality of electromagnetic radiating elements 14. The intersecting walls 12 form a honeycomb core structure with a surface arranged to conform to that of a structure into which it is to be integrated. A radome formed by a single piece of composite material is secured to, and conformal with, the conformal surface of the said honeycomb structure. One surface of the honeycomb core structure may be bonded to a multi-faceted back skin 16 and the other surface may be machined to provide a desired conformal surface contour. The back skin 16 may be linked with antenna electronics and provide printed circuit connections to the radiating elements 14. The radiating elements 14 may be dipoles formed within the intersecting walls 12. Adhesive material may be used to secure the walls 12, radome and back skin 16 together in a method involving a support jig and curing in an oven under certain heat and pressure conditions. The antenna array 10 may provide a compact, light weight structure which is also strong and can form part of a load bearing structure possibly in an aircraft or some other vehicle.
机译:保形天线阵列10包括支撑多个电磁辐射元件14的多个相交壁部分12。相交壁12形成蜂窝状芯结构,该蜂窝状芯结构的表面布置成与将其集成到其中的结构的表面一致。由单片复合材料形成的天线罩固定在所述蜂窝状结构的保形表面上并与其共形。蜂窝状芯结构的一个表面可以结合到多面的背面蒙皮16上,并且另一表面可以被加工以提供期望的保形表面轮廓。后蒙皮16可以与天线电子设备链接,并提供到辐射元件14的印刷电路连接。辐射元件14可以是形成在相交壁12内的偶极子。可以使用粘合剂材料来固定壁12,天线罩和后蒙皮。包括支撑夹具并在一定的热和压力条件下在烘箱中固化的方法中,将图16中所示的方法结合在一起。天线阵列10可以提供紧凑且重量轻的结构,该结构也坚固并且可以形成可能在飞机或某些其他车辆中的承载结构的一部分。

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