公开(公告)号：US20180335077A1

公开(公告)日：2018-11-22

申请号：US15982082

申请日：2018-05-17

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Ruediger OESSENICH ,  Magdalena HERRADOR MORENO ,  Thomas ERNSTBERGER ,  Jan EULITZ

IPC分类号： F16C3/02

CPC分类号： F16C3/026 ,  B29C65/64 ,  B29C66/534 ,  B29C70/462 ,  B29C70/86 ,  B29L2031/75 ,  F05D2240/61 ,  F05D2300/6034 ,  F05D2300/614 ,  F16C2360/23 ,  F16D1/027 ,  F16D1/101

摘要： A shaft, especially a radial shaft of an aircraft engine, with a hollow shaft made of a fibre composite material in a first multilayered arrangement and connection areas at the respective ends of the shaft for a respective connection element, wherein the connection of shaft and the connection elements is positive locking. The connection areas include a second multilayered arrangement made of fibre composite material, whose layers are arranged on the first multilayered arrangement of the shaft.