发明名称 FAN EXHAUST NOZZLE FOR TURBOFAN ENGINE
摘要 The cross sectional flow area of a fan discharge nozzle on one side of a central plane of an associated gas turbine engine power plant is greater than the corresponding flow area of the fan discharge nozzle on an opposite side of the central plane to compensate for the blockage of fan airflow by a pylon.
申请公布号 US2011014045(A1) 申请公布日期 2011.01.20
申请号 US20100893042 申请日期 2010.09.29
申请人 MCCALL JOHN 发明人 MCCALL JOHN
分类号 F01D5/04 主分类号 F01D5/04
代理机构 代理人
主权项
地址