发明名称 Guide cage for sub-calibre, flight stabilised projectile - has longitudinal slits terminating short of the rear end, leaving points of intentional weakness
摘要 <p>Drive cage (1) for a sub-calibre wing-stabilised missile is joined to the latter by the central thread and is made e.g. of aluminium or titanium. It is divided by three slots at a 120 deg.C spacing, produced by a slitting cutter (58) to a depth which leaves remanents of metal (20,50) at each end, bridging the slits. To prevent leakage of the propellant gases, the slits are filled during the presence in the barrel by shims shaped exactly to suit the contours of the slit; they are held in position by clips (with intentionally weak spot) in the groove (37). On leaving the barrel, the drive cage breaks up on three parts.</p>
申请公布号 DE3051030(C2) 申请公布日期 1987.04.23
申请号 DE19803051030 申请日期 1980.09.03
申请人 RHEINMETALL GMBH, 4000 DUESSELDORF, DE;L'ETAT FRANCAIS REPRESENTE PAR LE DELEGUE GENERAL POUR L'ARMEMENT, PARIS, FR 发明人 MONTIER, PATRICK;MOREAU, PIERRE ANDRE, BOURGES, FR;SAUVESTRE, JEAN-CLAUDE, ST. DOULCHARD, FR;SIMON, WALTER, 5100 AACHEN, DE;BISPING, BERNHARD, DIPL.-ING., 4030 RATINGEN, DE;WALLOW, PETER, DIPL.-ING., 4000 DUESSELDORF, DE;GERSBACH, KLAUS, 4156 WILLICH, DE
分类号 F42B14/06;(IPC1-7):F42B13/16 主分类号 F42B14/06
代理机构 代理人
主权项
地址