发明名称 Device for locating missile in firing barrel - has forward and rear adjustable and sprung locating points and at least two fixed locating points
摘要 At least one adjustable and sprung locating point (11,31) and two fixed locating points (11,12,31,32) are arranged, and serves simultaneously for alignment of the firing barrel (6) in the firing container (1), in which parts of the locating points fill out a gap between the firing barrel and the firing container. Adjustment screws for the adjustable and sprung locating points (11,31) support on transverse frames (3,4) of the firing container (1). At the front and at the rear two adjustable and sprung bearing points (11,31) and two fixed bearing points (12,32) are arranged, whereby the front bearing points (11,12) locate against support pins (10) on the missile (8). The rear bearing points (31,32) support on slide ribs (35) fitted on locations (33) for vanes (34) on the missile (8). USE/ADVANTAGE - A tolerance-free, adjustable missile location which obviates rattling vibrations.
申请公布号 DE4304563(C1) 申请公布日期 1994.04.28
申请号 DE19934304563 申请日期 1993.02.16
申请人 DEUTSCHE AEROSPACE AG, 80804 MUENCHEN, DE 发明人 HUETTER, HORST, 8180 TEGERNSEE, DE;PUTTINGER, DIETMAR, ING.(GRAD.), 8000 MUENCHEN, DE
分类号 F41F3/052;(IPC1-7):F41F3/042;B64D7/08;F41F3/06 主分类号 F41F3/052
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