Patent ID: 8490921
Filing Date: 2013-07-23
Classification: B64C,B64D,B64G,H02G

Abstract:
1. A line system arrangement in an aircraft or spacecraft having a fuselage, comprising at least a first receiving region and a second receiving region, wherein the first and second receiving regions each receive at least one component of a line system, wherein the component of the line system in at least one of the first and second receiving regions is a line for gaseous substances, wherein the receiving regions are accessible, at least in some sections, from outside the fuselage of the aircraft or spacecraft for at least one of installation and maintenance of the line system, and wherein the first and second receiving regions are adapted to an internal pressure which corresponds to a particular external pressure of the fuselage, wherein the arrangement comprises a pressure-tight separating device for pressure-tight separation of the first and second receiving regions from an interior space of the fuselage, and wherein the pressure-tight separating device comprises a connecting device for connecting the line for gaseous substances to a consumption unit and wherein the first receiving region is arranged along the length of the fuselage and wherein the second receiving region is arranged at an angle to the first receiving region along the circumference of the fuselage.