发明名称 Seal fitting method, for sealing missile in launch tube, involves measuring and display device for indicating deformation of seal caused by its compression
摘要 Method has a cylindrical device inserted in the launch tube (1) until it abuts the annular end face of the seal (5), with a drive acting between the cylindrical device and the device which supports it relative to the launch tube, for pressing the seal into the gap between the missile and the launch tube. Cylindrical device is provided with a measuring and display device (7) for indicating the deformation of the seal caused by its compression. An Independent claim for a device for fitting a seal between a missile and a launch tube is also included.
申请公布号 DE10064480(C1) 申请公布日期 2002.04.04
申请号 DE20001064480 申请日期 2000.12.22
申请人 EADS DEUTSCHLAND GMBH 发明人 SPENGLER, HANS
分类号 F41F3/042;(IPC1-7):F41F3/042 主分类号 F41F3/042
代理机构 代理人
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