Exit row table for an aircraft

Patent metadata

Field	Value
Publication number	US-10106260-B2
Application number	US-201715690745-A
Country	US
Kind code	B2
Filing date	Aug 30, 2017
Priority date	May 15, 2013
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

A table (30) for an aircraft includes a table surface (56) deployable between a retracted position and a deployed position, an arm (50) having a first end and a second end, the arm (50) supporting the table (66) surface at the first end, a support connected to the arm (50) at the second end, the support connecting the arm to a structure interior to the aircraft, a sensor (136) within the aircraft to detect if a seat adjacent to the table surface is occupied, and a mechanism (120) for retracting the table surface to the retracted position if the sensor (136) detects at least one of that the seat is not occupied and that the aircraft flight mode meets predetermined criteria.

First claim

What is claimed is:

1. An exit row table, comprising:
a table surface deployable between a retracted position and a deployed position;
an arm having a first end and a second end, the arm supporting the table surface at the first end, through an arm pivot;
a scissor jack connected to the arm via a slide for deploying the arm and table surface between a first position to a second position;
a support connected to the arm at the second end of the arm, the support being connected to the slide disposed in an aircraft structure interior; and
a rail for guiding travel of the slide connected to the support through a support pivot allowing the support to pivot from a vertical orientation to a horizontal orientation,
wherein the scissor jack is connected at a first end thereof to the slide connected to the support, such that the support moves along the rail and the scissor jack is connectable at a second end thereof to at least one of the rail, a frame disposed in the aircraft structure interior, or a portion of an interior of a sideledge of the aircraft.

2. The exit row table of claim 1 , wherein the first position is within a compartment and the second position is at least partially exterior to the compartment.

3. The exit row table of claim 1 , further comprising an actuator connected to the scissor jack for applying a force on the arm to deploy the arm between the first position and the second position.

4. The exit row table of claim 1 , wherein the scissor jack is responsive to a momentary application of a force to deploy the table surface between the first and second positions.

Assignees

• Bombardier Inc
• Bombardier Inc

Inventors

• Gagnon Pierre
• Roy Jordan
• Deka Tom
• Mageau Christian
• Monardo Michele
• Huber Stefan
• Haselberger Christoph

Classifications

• B64D11/06 Primary

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title

• B64D11/0605

  including tables or desks · CPC title

• B64D11/0638 Primary

  with foldable tables, trays or cup holders · CPC title