发明名称 OPTIMIZATION OF DOWNSTREAM OPEN FAN PROPELLER POSITION
摘要 <p>A method and apparatus for controlling a propeller of a contra-rotation open fan (CROF) engine of an aircraft. A diameter of the propeller is set to be at a first diameter during at least a portion of a first flight condition of the aircraft. The diameter of the propeller is set to be at a second diameter, different from the first diameter, during at least a portion of a second flight condition of the aircraft.</p>
申请公布号 EP2516262(A1) 申请公布日期 2012.10.31
申请号 EP20100782158 申请日期 2010.11.18
申请人 THE BOEING COMPANY 发明人 MOORE, MATTHEW D.;BOREN, KELLY L.;LANGTRY, ROBIN B.
分类号 B64C11/00;B64C11/48 主分类号 B64C11/00
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