发明名称 Aircraft including an internal partition
摘要 The aircraft includes a structural portion such as a fuselage, a wing, or a tail, the structural portion including a wall separating the inside from the outside of the portion and including fractions defining between them an inside volume of the portion and at least one structural partition separating zones of the volume, e.g. a front zone and a rear zone, from each other, the partition including at least one flexible diaphragm suitable for deforming and at least two preferably rigid supports supporting the diaphragm in discontinuous manner.
申请公布号 US8777160(B2) 申请公布日期 2014.07.15
申请号 US201013511853 申请日期 2010.11.30
申请人 Airbus Operations (S.A.S.) 发明人 Dazet Francis
分类号 B64C1/00 主分类号 B64C1/00
代理机构 Oliff PLC 代理人 Oliff PLC
主权项 1. An aircraft, including a structural portion such selected from the group comprising a fuselage, a wing, and a tail, the structural portion comprising: a wall separating an inside of the structural portion from an outside of the structural portion and comprising components defining between them an inside volume of the structural portion; and at least one structural partition separating zones of the inside volume from each other, the at least one structural partition comprising at least one flexible and deformable diaphragm and at least two rigid supports supporting the at least one diaphragm in a discontinuous manner, wherein the at least one structural partition is fastened to the structural portion by devices that are separable, the rigid supports include a first beam and a second beam such that the at least one diaphragm is connected to the first beam and the second beam, and the at least one diaphragm is configured to be inverted between the first beam and the second beam.
地址 Toulouse Cedex FR