专利名称：VECTORING TRANSITION DUCT FOR
TURBINE ENGINE
发明人：ROBERGE, Gary D.申请号：EP04822617.9申请日：20041201公开号：EP1825126A2公开日：20070829
摘要：A transition duct (112) is provided at the outlet of a turbine engine. Thetransition duct transitions the outlet of the tip turbine engine (10) from round to
rectangular. The transition duct also provides a plurality of variable vanes at the outlet ofthe transition duct. The transition duct incorporates a perimeter slot (124) providingcooling to the duct outer wall and attached components. The variable vanes (120) areinstalled to vector the exhaust gases. This allows the aircraft to decelerate, hover oraccelerate in the forward direction by commanding the position of the variable vanes .One potential application of the tip turbine engine is for vertical installations in aircraft.
申请人：UNITED TECHNOLOGIES CORPORATION
地址：One Financial Plaza Hartford CT 06101 US
国籍：US
代理机构：Leckey, David Herbert
更多信息请下载全文后查看
因篇幅问题不能全部显示，请点此查看更多更全内容