发明名称 ENGINE MID-TURBINE FRAME DISTRIBUTIVE COOLANT FLOW
摘要 A turbine engine includes a frame assembly including an outer cavity and an inner cavity with the outer cavity including at least one opening configured and adapted to communicate cooling air to the turbine case. A baffle within the outer cavity includes a plurality of openings for directing cooling airflow into the outer cavity for preventing impingement on a radially inner wall of the outer cavity for maintaining a desired temperature of the cooling air within the outer cavity.
申请公布号 US2016245114(A1) 申请公布日期 2016.08.25
申请号 US201514607102 申请日期 2015.01.28
申请人 United Technologies Corporation 发明人 Wang Cheng-Zhang
分类号 F01D25/14;F01D9/04;F01D25/12 主分类号 F01D25/14
代理机构 代理人
主权项 1. A turbine engine, comprising: a turbine section including a turbine case disposed about an axis; a frame assembly defining an outer cavity, wherein the outer cavity includes radially outer wall, a radially inner wall and at least one opening configured and adapted to communicate cooling air to the turbine case; and a baffle configured to receive cooling air through the radially outer wall and direct cooling airflow within the outer cavity to prevent impingement on the inner wall.
地址 Hartford CT US