发明名称 PROXIMITY FUSE
摘要 <p>PURPOSE:To eliminate operation except at a target by providing a second discriminator for deciding to output a high level when a distance value indicated by a distance signal becomes a predetermined value or less, and an ignition driver for operating an ignition when both the outputs of first and second discriminators become high levels. CONSTITUTION:A distance signal A to be supplied from a guiding device placed in a missile is input to a discriminator 4b. When the missile approaches a target and the signal A indicates a value for a predetermined distance, the discriminator 4b outputs a high level to an AND gate of a driver 4. Both discriminators 4a, 4b output high levels and a 2-input AND gate of a driver 5 satisfies an AND condition, the driver 5 outputs a drive signal to an ignition circuit 6 based on the output of the gate to ignite powder. The amplitude of a reception signal level for sending a high level output and distance of the discriminators 4a, 4b are previously set based on performance of the missile. An operation except at a target can be remarkably suppressed.</p>
申请公布号 JPH04158199(A) 申请公布日期 1992.06.01
申请号 JP19900282244 申请日期 1990.10.19
申请人 NEC CORP 发明人 SHIROMA TAKENORI;ODA OSAMU
分类号 F42C13/04;G01S13/88 主分类号 F42C13/04
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