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
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