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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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