Patent · US Active

Fuselage assembly for an aircraft

US10875619B2 · kind B2 · utility

0Cited by
4References
15Claims
0Family size

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Key dates

Filing dateMar 26, 2019
Grant dateDec 29, 2020
Priority date
Expiry dateMar 26, 2039

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2013/0625
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.

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