发明名称 |
AIRCRAFT COCKPIT, IN PARTICULAR THE FRONT PORTION OF AN AIRCRAFT COCKPIT |
摘要 |
A device for mixing at least two separate streams of components which, when mixed, form a combined fluid stream. The device comprises a conduit with at least two separate passageways leading to exit openings at an end face of the conduit. Each passageway communicates with a separate component stream and is arranged to direct the separate component stream in a downstream direction. The exit openings each have a predetermined cross-sectional flow area. A separate channel is located at a downstream end of each passageway exit opening. The channels are arranged to redirect the flow from each passageway to an axial direction. A single mixing chamber communicates with all of the separate channels, the mixing chamber being arranged to receive each of the component streams at an upstream end thereof and to permit a mixing of the component streams. An outlet is arranged downstream of the mixing chamber through which the combined fluid stream is dispensed. |
申请公布号 |
US2014209740(A1) |
申请公布日期 |
2014.07.31 |
申请号 |
US201414230074 |
申请日期 |
2014.03.31 |
申请人 |
Airbus Operations SAS |
发明人 |
Guering Bernard;Depeige Alain |
分类号 |
B60R11/02;B64D11/06;B64D45/00 |
主分类号 |
B60R11/02 |
代理机构 |
|
代理人 |
|
主权项 |
1. An aircraft cockpit display device comprising a screen and a support, wherein the screen is mounted on its support rotatable about a first, substantially horizontal pin, and wherein the support provides height adjustment of the screen. |
地址 |
Toulouse FR |