发明名称 ANTI-TORQUE NOZZLE SYSTEM WITH INTERNAL SLEEVE VALVE FOR A ROTORCRAFT
摘要 <p>The system of the present application includes a duct for receiving airflow from within a duct portion of a tailboom. The airflow is a mixture of fan driven air and engine exhaust. The system includes a fixed nozzle assembly with an anti-torque nozzle, a pro-torque nozzle and a thrust nozzle. A rotating sleeve valve is located within the fixed nozzle assembly. The rotating sleeve valve located within the fixed nozzle assembly and is configured to selectively redirect airflow into one or more of the anti-torque nozzle, the pro-torque nozzle and the thrust nozzle.</p>
申请公布号 WO2012064344(A1) 申请公布日期 2012.05.18
申请号 WO2010US56571 申请日期 2010.11.12
申请人 BELL HELICOPTER TEXTRON INC.;ROBERTSON, DANIEL, B. 发明人 ROBERTSON, DANIEL, B.
分类号 B64C27/82 主分类号 B64C27/82
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