发明名称 Radial bearing assembly for rudder shafts of pair of turning rudder blades of guided missile has each rudder shaft extending upto central longitudinal axis of missile structure whereby one of two tubular shafts surrounds other shaft
摘要 <p>Radial bearing assembly has rudder shafts (17,21) of a pair of turning rudder blades (13,20). Each rudder shaft extends upto the central longitudinal axis (16) of the missile structure (12). One of the two tubular rudder shafts surrounds the other rudder shaft. Rudder shafts are supported near the ends of the missile structure, facing the rudder blades, as well as at the ends away from the rudder blades.</p>
申请公布号 DE102004037204(A1) 申请公布日期 2006.03.23
申请号 DE20041037204 申请日期 2004.07.30
申请人 DIEHL BGT DEFENCE GMBH & CO. KG 发明人 BAER, KLAUS
分类号 F42B10/62 主分类号 F42B10/62
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