发明名称 |
VIRTUAL MULTI-STREAM GAS TURBINE ENGINE |
摘要 |
A gas turbine engine is provided that includes a core flow path to direct a core stream flow. A common flow path is outboard of the core flow path, where the common flow path directs both a second stream flow and a third stream flow. Another gas turbine engine is provided that includes an outer case structure around a central longitudinal engine axis. An intermediate case structure is inboard of the outer case structure, where the intermediate case structure and the outer case structure direct both a third stream flow and a second stream flow. An inner case structure is inboard of the intermediate case structure, where the inner case structure and the intermediate case structure direct a core stream flow. |
申请公布号 |
US2015361819(A1) |
申请公布日期 |
2015.12.17 |
申请号 |
US201514604228 |
申请日期 |
2015.01.23 |
申请人 |
United Technologies Corporation |
发明人 |
Epstein Alan H. |
分类号 |
F01D17/12;F01D9/04;F01D25/24;F01D5/02 |
主分类号 |
F01D17/12 |
代理机构 |
|
代理人 |
|
主权项 |
1. A gas turbine engine, comprising:
a core flow path to direct a core stream flow; and a common flow path outboard of the core flow path, the common flow path to direct both a second stream flow and a third stream flow. |
地址 |
Hartford CT US |