Integrated side ledge for an aircraft having a working surface supported by a first gear rack and second gear rack
An integrated side ledge table for an aircraft includes a mounting system with panels and brackets which mount directly to an aircraft structure. The panels are arranged to form a pocket which conceals gear racks configured to support a working surface such as a table. The table mounted to a pivot plate which is configured to track along the opposed gear racks and move the table to stowed and deployed positions when the lid, which provides access to the pocket, is opened or closed.
1 . An integrated side ledge for an aircraft, the integrated side ledge comprising:
a working surface, wherein the working surface is supported in between a first gear rack and a second gear rack, the first gear rack and the second gear rack each mounted inside a pocket and on opposing sides;
the pocket being mounted onto a mounting bracket, wherein the mounting bracket is mountable to an aircraft structure;
a pivot plate mounted to an underneath surface of the working surface and includes a first pivot mount on one side edge and a second pivot mount on an opposite side edge;
the working surface being configured to move from a stowed position inside the pocket to a fully deployed position when removed from the pocket.
2 . The integrated side ledge of claim 1 , wherein the first pivot mount is configured to track along the first gear rack and the second pivot mount is configured to track along the second gear rack.
3 . The integrated side ledge of claim 1 , wherein the pocket includes a front panel, a back panel, a first side panel, a second side panel, and a top panel wherein a lid hingedly mounts to the integrated side ledge.
4 . The integrated side ledge of claim 3 , wherein the first gear rack fastens to the first side panel and the second gear rack fastens to the second side panel.
5 . The integrated side ledge of claim 3 , wherein the lid pivots such that the working surface moves between the stowed position and the fully deployed position.
6 . The integrated side ledge of claim 1 , wherein the pocket conceals the working surface when the working surface is in the stowed position.
7 . An integrated side ledge for an aircraft, the integrated side ledge comprising:
mounting system, wherein the mounting system is configured to be secured to an aircraft structure;
a pocket including a rear panel, wherein the rear panel is configured to be fastened to the mounting system;
a working surface, wherein the working surface is supported on opposite sides by a first gear rack and a second gear rack and is configured to track in a single plane aligned with the first gear rack and the second gear rack;
the first gear rack and the second gear rack being mounted to opposing walls forming the pocket; and
a pivot plate mounted to an underside of the working surface.
8 . The integrated side ledge of claim 7 , wherein the first and second gear racks include siding, wherein the siding wraps around an upper rotating member and a lower rotating member forming the sides of a channel.
9 . The integrated side ledge of claim 8 , wherein the siding includes gear teeth, wherein the gear teeth interact with gear teeth configured on the upper rotating member and lower rotating member.
10 . The integrated side ledge of claim 7 , wherein the pivot plate includes pivot mounts positioned on opposing outer edges configured to track in between the siding of the first gear rack and the second gear rack.
11 . The integrated side ledge of claim 10 , wherein the pivot mounts each include gear teeth configured to interact with the siding to allow the working surface to be tracked.
12 . The integrated side ledge of claim 7 , further comprising a lid hingedly mounted to a top panel to provide access to the pocket when the lid is pivoted to an open position.
13 . The integrated side ledge of claim 12 , wherein pivoting the lid to a past open position deploys the working surface from the pocket.
14 . The integrated side ledge of claim 12 , wherein the working surface includes at least one groove configured to track along at least one guide rail.
15 . The integrated side ledge of claim 14 , wherein the guide rail is aligned in a single plane in a vertical direction within the pocket.
16 . The integrated side ledge of claim 14 , wherein the guide rail includes an upper edge configured to support the working surface in a deployed position.
17 . The integrated side ledge of claim 7 , wherein the opposing walls are each mounted to opposing ends of the rear panel.
18 . An integrated side ledge for an aircraft, the integrated side ledge comprising:
a table, wherein the table is mounted to a pivot plate and the pivot plate is supported on opposing ends by a first gear rack and a second gear rack and is configured to track in between the first and second gear racks;
the first gear rack and the second gear rack being mounted to opposing side panels, wherein each opposing side panel mounts to a rear panel, wherein the rear panel, the opposing side panels, and a front panel are arranged to form a pocket;
a mounting system, wherein the rear panel mounts directly to the mounting system and the mounting system mounts directly to an aircraft structure.