Component arrangement on an aircraft structure, and a method for the installation of a component into an aircraft structure

摘要

A component arrangement on an aircraft structure, in particular on a fuselage structure of an aircraft, with at least one mounting structure connected with the aircraft structure, and at least one component to be assigned to the aircraft structure, in particular a measuring device. At least one component carrier is provided to receive the component to be mounted, wherein the component carrier is connected with the mounting structure, and an outer surface of the component carrier, facing away from the component, extends approximately flush with an outer surface of the aircraft structure. Also a method for the installation of a component into an aircraft structure with a mounting structure including the step of connecting the component with the mounting structure via a component carrier, so that an outer surface of the component carrier, facing away from the component, extends approximately flush with an outer surface of the aircraft structure.

主权项

1. A component arrangement on an aircraft structure, comprising:
at least one mounting structure connected with the aircraft structure, at least one component configured to be mounted to the aircraft structure, and at least one component carrier for the reception of the component to be mounted, wherein the component carrier is configured as a one-piece aerodynamic plate and wherein the installation of the component takes place directly on the aerodynamic plate, the component carrier being connected with the mounting structure, wherein the component carrier is inserted into a central receptacle of the round, approximately ring-shaped mounting structure from an inner side of the aircraft, wherein a supporting surface of a ring-shaped collar of the component carrier abuts against a seating face of a flange of the mounting structure, wherein the supporting surface is facing away from the inner side of the aircraft and the seating face is facing towards the inner side of the aircraft and an outer surface of the component carrier, facing away from the component, extending approximately flush with an outer surface of the aircraft structure.