发明名称 Multi-axis vectorable exhaust nozzle
摘要 A convergent-divergent exhaust nozzle is mounted to an exhaust duct of a jet aircraft engine by a circumferentially-spaced set of hydraulic cylinders. The cylinders are interconnected in captured flow via hydraulic circuits which allow the cylinders to function as a gimbal mounting. This mounting allows the entire nozzle to vector the exhaust without additionally loading the divergent flaps with vectored exhaust so that cool, low pressure ram air can be channeled directly to the divergent flaps for efficient cooling.
申请公布号 US5351888(A) 申请公布日期 1994.10.04
申请号 US19930061398 申请日期 1993.05.14
申请人 GENERAL ELECTRIC COMPANY 发明人 TAYLOR, JOHN B.;NASH, DUDLEY O.
分类号 B64D33/08;F02K1/00;F02K1/12;(IPC1-7):B64D33/08;B05B1/12 主分类号 B64D33/08
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