Structure and method for reducing air flow in a wall volume of an aircraft
US10029798B2 · kind B2 · utility
1Cited by
11References
18Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Feb 9, 2015 |
| Grant date | Jul 24, 2018 |
| Priority date | — |
| Expiry date | Mar 13, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/49826
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft including a fuselage defining an upper lobe and a lower lobe, the fuselage including a wall structure that includes an outboard boundary and an inboard boundary spaced from the outboard boundary, wherein the outboard boundary and the inboard boundary define a wall volume therebetween, and a barrier sheeting member extending into the wall volume.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.