| 发明名称 |
HEAT EXCHANGER FOR A TURBO ENGINE |
| 摘要 |
The invention relates to a heat exchanger of an air circulation channel of a turbomachine, the heat exchanger being configured so as to have fluid to be cooled passing through it and including a plurality of fins protruding from a support surface, the heat exchanger being characterized in that each fin includes a base and a preferably continuous leading face which extends axially from the base in the air circulation direction while tapering from upstream to downstream along an axis parallel with the support surface. |
| 申请公布号 |
US2015260102(A1) |
申请公布日期 |
2015.09.17 |
| 申请号 |
US201414577097 |
申请日期 |
2014.12.19 |
| 申请人 |
SNECMA |
发明人 |
GHAZLANE Imane;Philippart Gabriela |
| 分类号 |
F02C7/18 |
主分类号 |
F02C7/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A heat exchanger of an air circulation channel of a turbomachine, the heat exchanger being configured so that a fluid to be cooled passes through it and includes a plurality of fins protruding from a support surface, the heat exchanger being characterized in that each fin includes a base and a preferably continuous leading face which extends axially from the base, in the air circulation direction while tapering from upstream to downstream along an axis parallel to the support surface. |
| 地址 |
Paris FR |
