发明名称 Gas turbine engine having a device for bleeding turbine flow into the fan bypass duct
摘要 <p>The gas-turbine engine has a fan (1), a fan housing (3) and a fan duct (4) and high pressure and low pressure turbines (15,16) are arranged one behind the other in the housing of the engine in the flow direction. A unit (17) is provided in the fan duct in the flow direction of the air stream (20) for discharging a part of the air stream before the low pressure-turbine in radial direction. The air stream comes out from the high pressure turbine.</p>
申请公布号 EP2119900(A2) 申请公布日期 2009.11.18
申请号 EP20090158579 申请日期 2009.04.23
申请人 ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 发明人 VENTER, GIDEON
分类号 F02K3/075;F02C9/18 主分类号 F02K3/075
代理机构 代理人
主权项
地址