发明名称 |
BYPASS TURBOJET ENGINE AIR INTAKE |
摘要 |
FIELD: transport. ^ SUBSTANCE: bypass turbojet engine cowling air intake with front suction branch pipe comprises top and bottom parts, inner (closer to fuselage) lateral side (115int) and outer lateral side (115ext) that define front edge (115) between cowling outer wall (111) and inner wall (113) that forms engine air feed channel. Front edge of external lateral wall (115ext) is arranged behind relative to front edge of inner lateral side (115int). Bypass turbojet engine may be equipped with such air intake. ^ EFFECT: reduced noise. ^ 7 cl, 4 dwg |
申请公布号 |
RU2413657(C2) |
申请公布日期 |
2011.03.10 |
申请号 |
RU20070103248 |
申请日期 |
2007.01.26 |
申请人 |
SNEKMA |
发明人 |
SHANE FILIPP ZHERAR;LOEHAK P'ER FILIPP MARI |
分类号 |
B64D33/02;F02C7/045;F02K3/06 |
主分类号 |
B64D33/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|