发明名称 Jet exhaust simulator
摘要 A jet exhaust simulator provides a multichamber jet fuel burner in which the fuel supplies to the chambers may be remotely and independently controlled, and in which a pilot flame chamber with squib igniter provides a reliable source of combustion. Primary, secondary, and tertiary fuel nozzles are provided, with the tertiary nozzles using straight venturis to inject large fuel drops into a burning fuel/air mixture in order to produce an exhaust plume closely simulating the length and infrared light emissions characteristics of a jet aircraft engine. The exhaust simulator is particularly adapted for use in a towable aerial target for the testing of infrared seeker guided shells or missles.
申请公布号 US4607849(A) 申请公布日期 1986.08.26
申请号 US19850709092 申请日期 1985.03.07
申请人 SOUTHWEST AEROSPACE CORPORATION 发明人 SMITH, DAVID H.;BRUM, ROGER D.
分类号 F23R3/34;F41J2/02;F41J9/10;(IPC1-7):F41J9/10 主分类号 F23R3/34
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