Patent ID: 11316260

Abstract:
An antenna arrangement for an aircraft for fastening to an outer side of an exterior skin of the aircraft has a body and side wall sections and a connecting section. The body is U-shaped or H-shaped if viewed from a predefined direction and can be flowed through with a low aerodynamic drag by a flow along the predefined direction. The antenna arrangement has one or more antennas in the form of a printed circuit board and of which each is fastened to the body and is fastenable directly to the outer side of the aircraft exterior skin at two first edges of the side wall sections which form two free ends of the U-shape or H-shape on a first side of the connecting section or, for the U-shape, on the connecting section and/or regions of the side wall sections, which regions adjoin the connecting section directly as the predefined direction is parallel to the flow direction during flight.