IP Library Granted Patent US 10,106,260
Granted Patent B2
US 10,106,260 · App. 15/690,745 · Granted Oct 23, 2018

Exit row table for an aircraft

Inventors: Pierre Gagnon (Vaudreuil, CA); Jordan Roy (Saint-Constant, CA); Tom Deka (Ste-Catherine, CA); Christian Mageau (Saint-Joseph-du-Lac, CA); Michele Monardo (Montreal, CA); Stefan Huber (Ort im Innkreis, AT); Christoph Haselberger (Ort imm Innkreis, AT)
Assignee: BOMBARDIER, INC.
B64D11/0638B64D11/06B64D11/0605
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Quick Facts
Patent No.
US 10,106,260
App. No.
15/690,745
Granted
Oct 23, 2018
Kind
B2
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.

Claims (10)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 30, 2017
From: GAGNON, PIERRE; ROY, JORDAN; DEKA, TOM; MAGEAU, CHRISTIAN; MONARDO, MICHELE; HUBER, STEFAN; HASELBERGER, CHRISTOPH
To: BOMBARDIER INC.
Reel/Frame 043448/0119 →
Continuity (3)
Continuation 14890960
Provisional Application 61823567 · May 15, 2013
Related Publication 20170361934A1 · Dec 21, 2017
Cited By (1)
US 12,654,858