| 发明名称 |
MULTI-BYPASS STREAM GAS TURBINE ENGINE WITH ENLARGED BYPASS FLOW AREA |
| 摘要 |
A gas turbine engine comprises a first bypass flow path housing configured within the engine, radially exterior to an engine core housing, and a second bypass flow path housing configured within the engine, radially exterior to the first bypass flow path housing. An axially downstream portion of the first bypass flow path housing includes a stepwise increase in area compared with an axially adjacent upstream portion of the first bypass flow path housing, thereby defining a component placement cavity in the axially downstream portion. |
| 申请公布号 |
US2015152789(A1) |
申请公布日期 |
2015.06.04 |
| 申请号 |
US201414534318 |
申请日期 |
2014.11.06 |
| 申请人 |
United Technologies Corporation |
发明人 |
Thomas Michael R.;Snape Nathan |
| 分类号 |
F02C9/18;F02C3/04 |
主分类号 |
F02C9/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a first bypass flow path housing configured within the engine, radially exterior to an engine core housing, and a second bypass flow path housing configured within the engine, radially exterior to said first bypass flow path housing; and an axially downstream portion of said first bypass flow path housing including a stepwise increase in area compared with an axially adjacent upstream portion of said first bypass flow path housing, thereby defining a component placement cavity in said axially downstream portion. |
| 地址 |
Hartford CT US |
