Patent · US Active

Method for installing system components in a portion of an aircraft fuselage

US11541981B2 · kind B2 · utility

0Cited by
1References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 29, 2019
Grant dateJan 3, 2023
Priority date
Expiry dateSep 11, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2211/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method is proposed for installing system components in a portion of an aircraft fuselage. The method provides at least one planar structural arrangement to be secured on or in the aircraft fuselage, secures system components on the structural arrangement, couples system lines to the system components and arranges the system lines on the structural arrangement. The method includes positioning of the structural arrangement with the system components and system lines arranged thereon at a designated installation location of the structural arrangement, and mechanical coupling of the structural arrangement to the aircraft fuselage.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.