发明名称 PROPULSIVE ANTI-TORQUE NOZZLE SYSTEM WITH ROTATING THRUST DIRECTOR 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 thrust director is located upstream of the fixed nozzle assembly. The rotating thrust director located 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 WO2012064345(A1) 申请公布日期 2012.05.18
申请号 WO2010US56582 申请日期 2010.11.12
申请人 BELL HELICOPTER TEXTRON INC.;GRONINGA, KIRK, L. 发明人 GRONINGA, KIRK, L.
分类号 B64C27/82 主分类号 B64C27/82
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