发明名称 Air target fuze
摘要 1. An improved air target fuze for use on a missile, said fuze comprising in combination: an oscillator, a modulator connected to frequency modulate said oscillator with a modulating waveform chosen so that the carrier frequency of said oscillator is changed from its initial value at approximately a t2/3 rate, where t represents time, until a predetermned frequency is reached, the wave then decreasing at a -t2/3 rate until the carrier frequency returns to its initial value, the above cycle then repeating periodically, a sidewise looking transmitting antenna to which the frequency modulated output of said oscillator is fed, a sidewise looking receiving antenna for receiving a reflected wave from a target, a mixer to which the received wave and a portion of the transmitted wave are fed, a narrow band amplifier having a center frequency fo to which the output of said mixer is fed, said modulating waveform further being chosen so that at the fuze-to-target cut-off distance beyond which the fuze is not to respond the difference frequency between the transmitted and received waves when the transmitted wave has a frequency corresponding to said predetermined point is substantially equal to the center frequency fo of said amplifier, a detonator, and means connected to the output of said narrow band amplifier for functioning said detonator in response to the receipt of a signal from said amplifier.
申请公布号 US4040357(A) 申请公布日期 1977.08.09
申请号 US19590797310 申请日期 1959.03.04
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 SAUNDERS, WILLIAM K.
分类号 F42C13/04;(IPC1-7):F42C13/04 主分类号 F42C13/04
代理机构 代理人
主权项
地址