发明名称 Lateral force joint
摘要 A lateral force joint, with which a plate-like spar can be fastened to a fuselage strap mounted on an airplane fuselage. The plate-like spar has a through bore, into which a fastening cylinder mounted on the flange can be inserted for connecting both components. In order to allow for the location of the spar to be adjusted with respect to the fuselage strap, a bearing bush of the spar is eccentrically fitted into the through bore. Correspondingly, the fastening cylinder of the fuselage strap is mounted eccentrically on a bearing bush so that a rotation of the bearing bushes allows the lateral force joint to be adjusted.
申请公布号 US8104709(B2) 申请公布日期 2012.01.31
申请号 US20060989350 申请日期 2006.05.11
申请人 MAENZ CHRISTIAN;AIRBUS DEUTSCHLAND GMBH 发明人 MAENZ CHRISTIAN
分类号 B64C9/00;B64C1/06;B64C3/00;B64C9/02 主分类号 B64C9/00
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