# US 2021/0242576 A1 · Antenna arrangement for an aircraft > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2021/0242576 A1 - Document ID: US20210242576A1 - Status: Published application - Kind: A1 - Application number: 17/158,637 - Filed: 2021-01-26 - Published: 2021-08-05 - Earliest claimed: 2020-01-31 - Assignees: Airbus Operations GmbH - Applicants: Airbus Operations GmbH - Inventors: Christian Schaupmann; Markus Altmann - Web page: https://patentgrep.com/patent/US20210242576A1 ## CPC - H01Q 1/286: {substantially flush mounted with the skin of the craft} - H01Q 1/02: Arrangements for de-icing; Arrangements for drying-out {; Arrangements for cooling; Arrangements for preventing corrosion} - H01Q 1/2283: {mounted in or on the surface of a semiconductor substrate as a chip-type antenna or integrated with other components into an IC package} - H01Q 5/307: Individual or coupled radiating elements, each element being fed in an unspecified way - H01Q: ANTENNAS, i.e. RADIO AERIALS (radiators or antennas for microwave heating H05B6/72) ## 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. ## Claims ### Claim 1 An antenna arrangement for an aircraft for fastening to an outer side of an exterior skin of the aircraft, the antenna arrangement comprising: a body configured from one or more non-metallic materials, and two plate-shaped side wall sections and a connecting section which connects them, which are arranged such that the body is U-shaped or H-shaped if viewed from a predefined direction; and one or more antennas in a form of a printed circuit board and of which each is fastened to the body; wherein the antenna arrangement can be fastened directly to the outer side of the exterior skin of the aircraft 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, in case of the U-shape, on the connecting section and/or regions of the side wall sections, which regions adjoin the connecting section directly, such that the predefined direction is parallel to a flow direction during flight of the aircraft. ### Claim 2 (depends on 1) The antenna arrangement according to claim 1, wherein each of the antennas is fastened either on a side of one of the side wall sections which faces another one of the side wall sections, or on the connecting section in case of the U-shape on a side which faces an interior of the U-shape. ### Claim 3 (depends on 1) The antenna arrangement according to claim 1, wherein at least one of the antennas is fastened to the body by being embedded completely or partially into the body. ### Claim 4 (depends on 1) The antenna arrangement according to claim 1, wherein at least one of the antennas has a cooling element and is embedded into the body such that only the cooling element or a part of the cooling element projects from the body. ### Claim 5 (depends on 1) The antenna arrangement according to claim 1, wherein the body is of single-piece or monolithic configuration. ### Claim 6 (depends on 1) The antenna arrangement according to claim 1, wherein the body comprises a plastic material and/or a composite material which is reinforced with glass fibers, quartz fibers, ceramic fibers or aramid fibers, or is configured from one or more of the materials. ### Claim 7 (depends on 6) The antenna arrangement according to claim 6, wherein the body comprises a composite material which is reinforced with glass fibers, quartz fibers, ceramic fibers or aramid fibers, which encloses a core made from a foam material or a honeycomb material. ### Claim 8 (depends on 1) The antenna arrangement according to claim 1, wherein a maximum extent of the connecting section in the predefined direction is smaller than a maximum extent of the side wall sections in the predefined direction. ### Claim 9 (depends on 1) The antenna arrangement according to claim 1, wherein a maximum extent of the connecting section in the predefined direction is greater than a maximum extent of the side wall sections in the predefined direction. ### Claim 10 (depends on 1) The antenna arrangement according to claim 1, wherein at least one of the antennas is fastened to the connecting section, and which antenna arrangement has a heat conduction device which is arranged on or in the body and connects the at least one antenna which is fastened to the connecting section to one or more heat sinks which is/are arranged on one of the or both side wall sections. ### Claim 11 (depends on 1) The antenna arrangement according to claim 1, wherein the body is H-shaped if viewed from the predefined direction, and in case of which the connecting section is arranged closer to the first edges of the side wall sections than to two second edges of the side wall sections which form other free ends of the H-shape on a second side of the connecting section which lies opposite the first side of the connecting section. ### Claim 12 (depends on 1) The antenna arrangement according to claim 1, wherein each of the antennas is in each case a KU-band, KA-band or L-band antenna. ### Claim 13 (depends on 1) An aircraft with an exterior skin and an antenna arrangement according to claim 1, the antenna arrangement being fastened directly to the outer side of the exterior skin of the aircraft at the two first edges of the side wall sections or, in case of the U-shape, on the connecting section and/or regions of the side wall sections, which regions adjoin the connecting section directly, such that the predefined direction is parallel to the flow direction during the flight of the aircraft. ### Claim 14 (depends on 13) The aircraft according to claim 13, comprising an arrangement of fastening elements on the outer side of the exterior skin, the antenna arrangement being fastened to the fastening elements by two first edges of the side wall sections or, in case of the U-shape, being fastened to the fastening elements by the connecting section and/or regions of the side wall sections, which regions adjoin the connecting section directly.