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 |