发明名称 |
Flexible coupling for drive shaft of aircraft wing slat and flap |
摘要 |
An aircraft wing has a flexible union between sections of shaft, moving either the leading edge slats or the trailing edge flaps. The end of each shaft section which is to be joined has a flange. Each flange is joined to the adjacent flange by a flexible disc and bolts which pass between both flanges and the disc. The load is transferred between the adjacent shaft sections primarily by the bolts, or by a bolt linkage incorporating mechanical play which discharges the function of a flexible disc. |
申请公布号 |
DE19724772(A1) |
申请公布日期 |
1998.12.24 |
申请号 |
DE1997124772 |
申请日期 |
1997.06.12 |
申请人 |
DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG, DE |
发明人 |
MARTENS, WILHELM, DIPL.-ING., 27751 DELMENHORST, DE |
分类号 |
F16D3/78;F16D3/79;(IPC1-7):F16D3/64;B64C9/12 |
主分类号 |
F16D3/78 |
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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