发明名称 |
FLOOR SYSTEM FOR A FUSELAGE SECTION OF AN AIRCRAFT |
摘要 |
A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as primary structure. Consequent to the free or self-supporting design of the floor system in the fuselage cell, the layout of the floor system along an aircraft axis can be matched to customer specifications in a simple manner without reference to structural boundary conditions of the fuselage structure. A floor surface for the floor system is formed from a number of floor elements which can be fitted with functional elements, wherein filling of empty spaces or cavities can be achieved with a number of floor equalization elements. As the floor elements have a relatively large support or fixing surface the loads induced by the functional elements are introduced into the floor system distributed over a large area such that the structural components thereof can be of a structurally lighter and thus weight-saving size. |
申请公布号 |
EP2240364(A2) |
申请公布日期 |
2010.10.20 |
申请号 |
EP20090708578 |
申请日期 |
2009.01.07 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
HAACK, CORD;SCHUMACHER, MARKUS;MUIN, ANDREW;SCOLEY, IAN |
分类号 |
B64C1/18 |
主分类号 |
B64C1/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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