| 发明名称 |
DEVICE FOR PRECOOLING AND PURIFYING ENGINE BLEED AIR |
| 摘要 |
A cooling device for the cooling of bleed air in an aircraft comprises an inlet opening for letting in bleed air, and an outlet opening for letting out bleed air. Furthermore, the cooling device comprises a heat exchanger with a first surface, along which the bleed air can be led from the inlet opening to the outlet opening, and with a second surface, along which a cooling medium can be led. The first surface comprises a catalytic element and is designed to carry out a catalytic reduction of bleed air impurities. The heat exchanger is a rib plate heat exchanger, and the first surface is at least in part formed by a first rib. |
| 申请公布号 |
US2015360786(A1) |
申请公布日期 |
2015.12.17 |
| 申请号 |
US201514737629 |
申请日期 |
2015.06.12 |
| 申请人 |
Airbus Defence and Space GmbH |
发明人 |
OBERPRILLER Korbinian;OBERPRILLER Helmut |
| 分类号 |
B64D13/08 |
主分类号 |
B64D13/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A cooling device for the cooling of bleed air in an aircraft, comprising:
an inlet opening for letting in bleed air, and an outlet opening for letting out bleed air; a heat exchanger with a first surface, along which the bleed air can be led from the inlet opening to the outlet opening, and with a second surface, along which a cooling medium can be led; wherein the first surface comprises a catalytic element and is designed to carry out a catalytic reduction of bleed air impurities; wherein the heat exchanger is a rib plate heat exchanger, and the first surface is at least in part formed by a first rib. |
| 地址 |
Ottobrunn DE |
