发明名称 Variable cycle gas turbine engine
摘要 <p>Gas turbine aero engine provided with core flow bypass (74,66) between the HP and LP turbines, regulation valve (62) and an auxiliary turbine (60). When high trust is required, the valve (62) is open and auxiliary turbine (60) supply extra power to the compressor (32).</p>
申请公布号 EP2472081(A2) 申请公布日期 2012.07.04
申请号 EP20110010294 申请日期 2011.12.29
申请人 ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. 发明人 HEATHCO, CRAIG
分类号 F02C1/00;F02C3/107;F02C3/13;F02C9/18 主分类号 F02C1/00
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