Patent · US Active

Pressure bulkhead for an aircraft and device as well as method for manufacturing an aircraft structural component

US9637215B2 · kind B2 · utility

4Cited by
10References
4Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 24, 2014
Grant dateMay 2, 2017
Priority date
Expiry dateNov 25, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A pressure bulkhead made of fiber composite material for an aircraft fuselage for the pressure-tight axial closure of a fuselage region configured to be put under internal pressure. The bulkhead comprises a first area element, at least one second area element and a plurality of core elements. The first area element has a plurality of receptacles. Each receptacle is configured to receive a core element. The core elements are received in the receptacles between surfaces facing one another of the first area element and of the at least one second area element. The surfaces facing one another of the first area element and of the at least one second area element are connected to one another in regions without core elements.

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