公开(公告)号：US20200320961A1

公开(公告)日：2020-10-08

申请号：US16836214

申请日：2020-03-31

Applicant: Airbus Operations GmbH ,  Airbus Operations S.L.

Inventor： Matthijs PLOKKER ,  Luc Jan HORNSTRA ,  Frank NIELSEN ,  Gabrielle De Brouwer

IPC: G09G5/38 ,  B64D47/02 ,  G03B21/60

Abstract: An illumination system for illuminating outer aircraft components of an airborne vehicle, such as an aircraft, includes a light projection system configured to project visual imagery to an outer surface of the airborne vehicle, and a projection controller having a light control processor configured to control the operation of the light projection system on the basis of at least one of operational flight status of the airborne vehicle, geographical location of the airborne vehicle and configuration data of movable surfaces of the airborne vehicle or on ambient light measurement.

公开(公告)号：US20240213659A1

公开(公告)日：2024-06-27

申请号：US18391108

申请日：2023-12-20

Applicant: Airbus Operations GmbH

Inventor： Matthijs PLOKKER ,  Sebastian WICHER ,  Michael KARWIN

IPC: H01Q1/28 ,  H01Q9/04

CPC classification number: H01Q1/286 ,  H01Q9/0407

Abstract: An aircraft antenna (101) including a radome (102) wherein the radome (102) has a main body (105) shaped to enclose one or more antennae (107) when the antenna (101) is attached to a fuselage skin portion (103), wherein the main body (105) includes a front surface portion (203), a rear surface portion (401), adjacent side surface portions (205,207), and an upper surface portion (209) that form a smooth outer aerodynamic surface (211) of the antenna (101), and wherein the upper surface (209) is substantially planar in shape along a length of 60% to 80% of a length (L) of the of the radome (102).