发明名称 Turbofan engine
摘要 <p>A propulsive fan system (10) comprises a fan unit (11) comprising a first stage array (12) of rotatable blades (14) upstream of a second stage array (16) of rotatable blades (14). The first stage (12) is coupled to a first drive means (24). The second stage (16) is coupled to a second drive means (26). The first drive means (24) is independently operable of the second drive means (26) during operation of the fan system (10).</p>
申请公布号 EP2270326(A2) 申请公布日期 2011.01.05
申请号 EP20100162389 申请日期 2010.05.10
申请人 ROLLS-ROYCE PLC 发明人 BRADBROOK, STEPHEN JOHN
分类号 F02K3/06 主分类号 F02K3/06
代理机构 代理人
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