Fuselage structure and method for manufacturing a fuselage structure
US10486789B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Jul 7, 2016 |
| Grant date | Nov 26, 2019 |
| Priority date | — |
| Expiry date | Oct 1, 2037 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C1/064
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A fuselage structure includes a pressure bulkhead and a frame being arranged behind the pressure bulkhead. The fuselage structure includes a first beam element with a first cantilever and a second cantilever, while the first beam element extends in a vertical direction of the fuselage structure. The first cantilever and the second cantilever protrude from the first beam element in a first direction toward the frame. The first direction of both cantilevers is inclined at a first angle with respect to a longitudinal direction of the fuselage structure. An aircraft with a fuselage structure and a method for manufacturing a fuselage structure are also described.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.