| 发明名称 | Fuselage segment, and method for the production of a fuselage segment | ||
| 摘要 | A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are integrated into the core, as well as a method for manufacturing such a fuselage segment. | ||
| 申请公布号 | US8844870(B2) | 申请公布日期 | 2014.09.30 |
| 申请号 | US201013262246 | 申请日期 | 2010.03.30 |
| 申请人 | Airbus Operations GmbH | 发明人 | Goehlich Robert Alexander |
| 分类号 | B64C1/00;B64C1/12;B32B5/32;B64D11/00;B32B27/04;B64C1/40;B64D13/00;B32B27/02 | 主分类号 | B64C1/00 |
| 代理机构 | Carter, DeLuca, Farrell & Schmidt, LLP | 代理人 | Carter, DeLuca, Farrell & Schmidt, LLP |
| 主权项 | 1. A fuselage segment of an aircraft fuselage, comprising: an inner skin on a cabin side of the aircraft fuselage; and an outer skin of the aircraft fuselage that covers a core, where conduits for system installations are integrated into the core, wherein at least the core consists of a foam material wherein the material hardness of the foam material increases from a center region of the core to the outer skin and from the center region of the core to the inner skin. | ||
| 地址 | Hamburg DE | ||