Patent · US Active

Hybrid inner fixed structure with metallic and composite construction

US9885253B2 · kind B2 · utility

4Cited by
8References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 7, 2014
Grant dateFeb 6, 2018
Priority date
Expiry dateNov 17, 2035

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

Aspects of the disclosure are directed to a system for an aircraft comprising: a titanium bottle section that includes at least two sections configured to house an engine, and at least one bifurcation panel coupled to the bottle section, wherein the at least one bifurcation panel includes a material that is different from titanium.

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