An inlet for a ram air turbine. The inlet is positioned forward of a turbine shaft, which is configured to rotate about a portion of an object. The inlet has a fixed geometry that chokes airflow through the inlet to prevent overspeed of the turbine shaft.
申请公布号
WO2012091828(A2)
申请公布日期
2012.07.05
申请号
WO2011US62213
申请日期
2011.11.28
申请人
GENERAL ELECTRIC COMPANY;TERSMETTE, TREVOR, ANDREW;RYAN, CHRISTOPHER, ALLEN
发明人
TERSMETTE, TREVOR, ANDREW;RYAN, CHRISTOPHER, ALLEN
