发明名称 Flame position ultrasonic interferometer
摘要 A sensitive instrument system for determining the position of the burn front in a rocket motor is disclosed. Separate adjacent transmitter and receiver elements are attached to the rocket motor casing to form an ultrasonic interference system. An ultrasound beam is transmitted to the motor's interior and the reflected beam from the propellant gas burn front is captured by the receiver. The received signal is processed to determine the distance to the propellant-gas interface.
申请公布号 US5272908(A) 申请公布日期 1993.12.28
申请号 US19900474695 申请日期 1990.02.06
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 SOSS, DAVID A.
分类号 G01N29/024;G01N33/22;(IPC1-7):G01N33/22 主分类号 G01N29/024
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