IP Library Granted Patent US 9,969,483
Granted Patent B2
US 9,969,483 · App. 14/772,429 · Granted May 15, 2018

Aircraft floor incorporating a ground plane

Inventors: Lody Roborel De Climens (Montreal, CA); Philippe Desy (Prévost, CA); Jean-Guy Gaudreau (St-Bernadin, CA)
Assignee: BOMBARDIER INC.
B64C1/18B64D45/02F16M13/02
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Quick Facts
Patent No.
US 9,969,483
App. No.
14/772,429
Granted
May 15, 2018
Kind
B2
Abstract

A system for shielding of at least one component ( 28 ) within an aircraft ( 10 ) includes a floor panel disposed at least partially between joists ( 38 ) supporting a floor ( 30 ) within the aircraft and a ground plane ( 44 ) connected to a bottom surface of the floor panel. The ground plane extends at least partially between adjacent joists. At least one bracket ( 52 ) electrically connects the ground plane to at least one of the joists.

Claims (19)

1. A system for shielding of at least one component within an aircraft, comprising:

a floor panel disposed at least partially between joists supporting a floor within the aircraft, the floor panel being connected to at least one of the joists;

a ground plane connected to a bottom surface of the floor panel, the ground plane extending at least partially between adjacent joists; and

at least one bracket electrically connecting the ground plane to the at least one joist, the electrical connection between the ground plane and the at least one joist being independent from the connection between the floor panel and the at least one joist.

2. The system of claim 1 , wherein the ground plane shields the at least one component from at least one of electromagnetic and radio frequency interference.

3. The system of claim 1 , wherein the ground plane comprises:

a plate of electrically conductive material; and

at least one hole provided in the plate to lighten the total weight of the plate,

wherein the hole is sized for shielding of the at least one component, accommodating at least one of frequency and wavelength of impingent radiation upon the at least one component.

4. The system of claim 3 , wherein the hole is no more than about 1/10th of the size of a minimum wavelength of the impingent radiation.

5. The system of claim 1 , wherein the bracket comprises:

a body defining a first end and a second end, wherein the first end connects to the ground plane and wherein the second end connects to the joist;

at least one first fastener connecting the first end to the ground plane;

at least one second fastener connecting the second end to the joist;

a spacer connected to the first end, establishing a contact surface between the spacer and the ground plane; and

a seal surrounding the spacer.

6. The system of claim 1 , wherein the bracket comprises a first end defining a first surface for contacting the ground plane and a second end defining a second surface for contacting the at least one joist, the first and second surfaces being non-parallel.

7. The system of claim 6 , wherein the first and second surfaces are substantially perpendicular.

8. The system of claim 1 , comprising a plurality of brackets where each bracket is disposed roughly at a corner of the ground plane.

Assignments (3)
CHANGE OF NAME Recorded Oct 8, 2020
From: C SERIES AIRCRAFT LIMITED PARTNERSHIP
To: AIRBUS CANADA LIMITED PARTNERSHIP
Reel/Frame 054023/0582 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 6, 2018
From: BOMBARDIER INC.
To: C SERIES AIRCRAFT LIMITED PARTNERSHIP
Reel/Frame 046282/0587 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 3, 2015
From: ROBOREL DE CLIMENS, LODY; DESY, PHILIPPE; GAUDREAU, JEAN-GUY
To: BOMBARDIER INC.
Reel/Frame 036485/0518 →
Continuity (2)
Provisional Application 61773441 · Mar 6, 2013
Related Publication 20160009361A1 · Jan 14, 2016