发明名称 |
METHOD OF DE-ICING THE LEADING EDGE OF AN AERODYNAMIC SURFACE AND AIRCRAFT IMPLEMENTING SUCH A METHOD |
摘要 |
<p>According to the invention, on at least one of the faces (1E, 1I) of said leading edge (1), forward of the partition (3), an action is exerted on the fluid flow (EF) so as to cause the latter to switch from the laminar state (EFL) to the turbulent state (EFT) in order to increase the thermal exchanges and minimize the thermal stresses on said leading edge.</p> |
申请公布号 |
WO2007080333(A1) |
申请公布日期 |
2007.07.19 |
申请号 |
WO2007FR00065 |
申请日期 |
2007.01.15 |
申请人 |
AIRBUS FRANCE;BARBARA, OLIVIER;DONJAT, DAVID |
发明人 |
BARBARA, OLIVIER;DONJAT, DAVID |
分类号 |
B64D15/04;B64C21/10 |
主分类号 |
B64D15/04 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|