发明申请
US20160185449A1 FLUID-VECTORING SYSTEM 有权
流体传感系统

FLUID-VECTORING SYSTEM
摘要:
A jet aircraft includes an aircraft integrated, fluid vectoring, exhaust nozzle system. Implementation of this disclosure may eliminate or reduce the size of the aircraft vertical stabilizer and rudder assembly, thereby potentially improving aircraft survivability and increasing aircraft thrust-to-weight ratio.
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