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