发明名称 Axial and or radial bearing in fibre composite shell
摘要 A sleeve (2) between the bearing (1) and the thin-walled shell (3) transmits forces from the bearing to the shell. The shell is divided in the direction of its thickness near the bearing-container. Part of the shell is radially positioned in relation to the sleeve to absorb radial forces. The other part at least partly encloses the end surface of the sleeve for absorbing axial forces. A support ring (4) is positioned between the separated parts of the shell.
申请公布号 DE19713880(A1) 申请公布日期 1998.10.15
申请号 DE1997113880 申请日期 1997.04.04
申请人 ZF LUFTFAHRTTECHNIK GMBH, 34379 CALDEN, DE 发明人 MUELLER, JOSEF, 88682 SALEM, DE
分类号 F16C35/077 主分类号 F16C35/077
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