An aircraft structural component is described, including an aircraft skeleton component which divides a space along a longitudinal axis of the aircraft skeleton component into two spatial portions arranged on opposite sides of the aircraft skeleton component, and including a fluid conduit component which runs on an outer side of the aircraft skeleton component and fluidically connects the two spatial portions. Also described is an aircraft wing with an aircraft structural component, as well as an aircraft with an aircraft structural component or with an aircraft wing.
UNKNOWN
2020-09-24
Patent
Electronic Resource
English
Tokio Prada &unknown;Epicenter&unknown;
Online Contents | 2003
Tokio Prada &unknown;Epicenter&unknown;
Online Contents | 2003