Patent ID: 11878785
Assignee: AIRBUS OPERATIONS LIMITED
Field: Mechanical elements (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 14:
15. A method for installing a first line section and at least one second line section in a fuselage of an aircraft, comprising:
attaching a first line section having a first diameter to a structural part of the fuselage through first line brackets, which comprise a first receiving space configured to hold the first line section and a first support portion for attaching the first line brackets to the structural part,
attaching at least one second line section having a second diameter to the first line section through second line brackets, which comprise a second receiving space configured to hold the at least one second line section and a second support portion for attaching the second line brackets to the first line section,
wherein at least one second line section comprises a higher flexibility than the first line section,
wherein the first receiving space and the first support portion of at least one of the first line brackets enclose the first line section, and
wherein the at least one second line section is attached to the first line section through a plurality of second line brackets that are arranged at a distance to and are independent from the first line brackets.