发明名称 |
Structural element for an aircraft |
摘要 |
<p>The structural element for the floor in an aircraft fuselage (2) has a passive component (3), as the lateral carrier to support the floor, and active piezo electric ceramics (20-22) to pass controlled forces into the passive component. A control (31), with an electronic measurement and evaluation function, is electrically connected (24-26) to the piezo electric ceramics, to pass voltage signals for them to expand or contract (27-30) according to the forces on the fuselage floor as the aircraft maneuvers in flight.</p> |
申请公布号 |
EP1681236(A1) |
申请公布日期 |
2006.07.19 |
申请号 |
EP20060000910 |
申请日期 |
2006.01.17 |
申请人 |
AIRBUS DEUTSCHLAND GMBH;EADS DEUTSCHLAND GMBH |
发明人 |
FRANKENBERGER, ECKART;KONSTANZER, PETER |
分类号 |
B64C1/00;B64C1/18;B64C1/40 |
主分类号 |
B64C1/00 |
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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