| 发明名称 | Shell component for an aircraft or spacecraft | ||
| 摘要 | A shell component for an aircraft or spacecraft. The shell component includes a skin panel, a plurality of stringers which are arranged on the skin panel, a former which includes a fiber composite material and is arranged over the stringers so as to cross the stringers, and a former connection structure which includes a ductile material and a plurality of foot portions fixed to the skin panel. The foot portions each transition integrally into a shoulder portion fixed to the former over an associated fixing span, the fixing spans associated with the foot portions extending along the former substantially continuously over the stringers. | ||
| 申请公布号 | US9150299(B2) | 申请公布日期 | 2015.10.06 |
| 申请号 | US200913130257 | 申请日期 | 2009.11.25 |
| 申请人 | Airbus Operations GmbH | 发明人 | Tacke Stefan |
| 分类号 | B64C1/06 | 主分类号 | B64C1/06 |
| 代理机构 | Greer, Burns & Crain Ltd. | 代理人 | Greer, Burns & Crain Ltd. |
| 主权项 | 1. A fuselage shell component for an aircraft or spacecraft, comprising: a skin panel; a plurality of stringers which are arranged on the skin panel; a former which comprises a fibre composite material and is arranged over the stringers; and a former connection structure which comprises a ductile material, which is formed so as to absorb energy upon impact, and a plurality of foot portions fixed to the skin panel, each of which foot portions transitions integrally into a shoulder portion fixed to the former over an associated fixing span for each foot portion, the fixing spans belonging to the foot portions extending along the former substantially continuously over the stringers, wherein the fixing spans overlap one another along the former. | ||
| 地址 | Hamburg DE | ||