Aircraft cockpit, in particular the front portion of an aircraft cockpit
AssigneeAirbus Operations GmbH
InventorsBernard Guering, Alain Depeige
Life of this patent
Estimating the term…
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AssigneeAirbus Operations GmbH
InventorsBernard Guering, Alain Depeige
Estimating the term…
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.
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.
An aircraft cockpit comprising:
A glare shield of an aircraft cockpit, comprising:
An aircraft cockpit comprising:
Dependencies are inferred from the claim text.