| 发明名称 |
ENGINE BYPASS VALVE |
| 摘要 |
Aspects of the disclosure are directed to an engine of an aircraft. The engine may include a first fan configured to output a first air flow, a second fan configured to receive a first portion of the first air flow and output a second air flow, a core configured to receive a first portion of the second air flow and generate a first stream, and at least one valve configured to assume one of at least three states in association with a generation of a second stream and a third stream based on at least one of the first air flow and the second air flow. |
| 申请公布号 |
US2016298550(A1) |
申请公布日期 |
2016.10.13 |
| 申请号 |
US201514685166 |
申请日期 |
2015.04.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Kupratis Daniel B.;Hanlon Christopher J.;Ledwith, JR. Walter A. |
| 分类号 |
F02C9/18;F02C3/13 |
主分类号 |
F02C9/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An engine of an aircraft, comprising:
a first fan configured to output a first air flow; a second fan configured to receive a first portion of the first air flow and output a second air flow; a core configured to receive a first portion of the second air flow and generate a first stream; and at least one valve configured to assume one of at least three states in association with a generation of a second stream and a third stream based on at least one of the first air flow and the second air flow. |
| 地址 |
Hartford CT US |
