IP Library Granted Patent US 9,878,801
Granted Patent B2
US 9,878,801 · App. 14/866,164 · Granted Jan 30, 2018

Console assembly including stowable support surface

Inventors: Tristan Flynn (Savannah, GA); Todd Loar (Savannah, GA); Eric Long (Huntington Beach, CA); Conrad Strelzyk (Montreal, CA); Bryan Clarke (Montreal, CA)
Assignees: C&D AEROSPACE CANADA CO.; GULFSTREAM AEROSPACE CORPORATION
B64D43/00
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Quick Facts
Patent No.
US 9,878,801
App. No.
14/866,164
Granted
Jan 30, 2018
Kind
B2
Abstract

A console assembly for use on a flight deck of an aircraft includes, but is not limited to, a console having a recess. The recess has an opening. The console assembly further includes a mounting assembly mounted within the recess. The console assembly further includes a support surface mounted to the mounting assembly. The console assembly further includes a closeout panel that is mounted to the support surface. The support surface fits within the recess. The mounting assembly facilitates movement of the support surface between a retracted and a deployed position. The support surface is disposed within the recess while in the retracted position and outside of the recess while in the deployed position. The closeout panel is disposed at a location on the support surface that causes the closeout panel to close the opening of the recess when the support surface is in the retracted position.

Claims (28)

1. A console assembly for use on a flight deck of an aircraft, the console assembly comprising:

a console configured to be mounted in the flight deck of the aircraft, the console having a recess defined therein, the recess having an opening, the opening facing towards the flight deck when the console is mounted in the flight deck;

a mounting assembly mounted within the recess;

a support surface mounted to the mounting assembly; and a closeout panel mounted to the support surface,

wherein the support surface is configured to fit within the recess, wherein the mounting assembly is configured to facilitate movement of the support surface between a retracted position and a deployed position, wherein the support surface is disposed within the recess when in the retracted position and disposed outside of the recess when in the deployed position, wherein the closeout panel is disposed at a location on the support surface that causes the closeout panel to close the opening of the recess when the support surface is in the retracted position, wherein the support surface includes a first body and a second body, wherein the second body is pivotally attached to the first body, wherein the second body is pivotable from a first position to a second position where the first body and second body form the support surface, wherein when the second body is pivoted to the second position the closeout panel moves with respect to the support surface to a position below the support surface.

2. The console assembly of claim 1 , wherein the support surface is configured to reside in the retracted position within the recess when the second body is folded over the first body in the first position.

3. The console assembly of claim 1 , wherein an entire portion of the mounting assembly remains within the recess when the support surface is disposed in the deployed position.

4. The console assembly of claim 1 , wherein the mounting assembly is configured to permit deflection of the support surface while the support surface is in the deployed position.

5. The console assembly of claim 4 , wherein the mounting assembly permits the support surface to deflect by a predetermined amount while the support surface is disposed in the deployed position.

6. The console assembly of claim 5 , wherein the predetermined amount is fifteen degrees.

7. The console assembly of claim 4 , wherein the mounting assembly includes a release mechanism that permits detachment of the support surface from the mounting assembly.

8. The console assembly of claim 7 , wherein the release mechanism comprises a quick release mechanism.

9. The console assembly of claim 8 , wherein the quick release mechanism is positioned to permit actuation by a thumb of an aircrew member.

10. The console assembly of claim 1 , further including an engagement surface mounted to the support surface, the engagement surface protruding above an upper surface of the support surface.

11. The console assembly of claim 10 , wherein the engagement surface has a higher coefficient of static friction than the upper surface of the support surface.

12. The console assembly of claim 10 , wherein the engagement surface comprises a compressible polymeric material.

13. The console assembly of claim 1 , wherein a first appearance of the closeout panel matches a second appearance of a surface of the console.

14. The console assembly of claim 13 , wherein the closeout panel is adjacent the surface.

15. The console assembly of claim 1 , further including a latch associated with the console, wherein the support surface is retained in the retracted position by the latch when the latch is latched and wherein the support surface is free to move to the deployed position when the latch is unlatched.

16. The console assembly of claim 15 , wherein the latch comprises a push-push latch.

17. A console assembly for use on a flight deck of an aircraft, the console assembly comprising:

a console configured to be mounted in the flight deck of the aircraft, the console having a recess defined therein, the recess having an opening, the opening facing towards the flight deck when the console is mounted in the flight deck;

a mounting assembly mounted within the recess;

a support surface mounted to the mounting assembly;

an engagement surface mounted to the support surface, the engagement surface protruding above an upper surface of the support surface;

a latch associated with the console; and

a closeout panel mounted to the support surface,

wherein the support surface is configured to fit within the recess, wherein the mounting assembly is configured to facilitate movement of the support surface between a retracted position and a deployed position, wherein the support surface is disposed within the recess when the support surface is disposed in the retracted position, wherein the support surface is disposed outside of the recess when the support surface is in the deployed position, wherein the support surface is retained in the retracted position by the latch when the latch is latched, wherein the support surface is free to move to the deployed position when the latch is unlatched, wherein the closeout panel is disposed at a location on the support surface that causes the closeout panel to close the opening of the recess when the support surface is in the retracted position, wherein the support surface includes a first body and a second body, wherein the second body is pivotally attached to the first body, wherein the second body is pivotable from a first position to a second position where the first body and second body form the support surface, wherein when the second body is pivoted to the second position the closeout panel moves with respect to the support surface to a position below the support surface, and wherein the engagement surface has a higher coefficient of static friction than the upper surface of the support surface.

Assignments (5)
CHANGE OF NAME Recorded Mar 31, 2023
From: C&D AEROSPACE CANADA CO.
To: SAFRAN CABIN CANADA CO.
Reel/Frame 063214/0797 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 26, 2017
From: LONG, ERIC
To: C&D AEROSPACE CANADA CO.
Reel/Frame 043962/0906 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 26, 2017
From: STRELZYK, CONRAD
To: C&D AEROSPACE CANADA CO.
Reel/Frame 043962/0957 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 26, 2017
From: CLARKE, BRYAN
To: C&D AEROSPACE CANADA CO.
Reel/Frame 043963/0024 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 25, 2015
From: FLYNN, TRISTAN; LOAR, TODD
To: GULFSTREAM AEROSPACE CORPORATION
Reel/Frame 036661/0189 →
Continuity (2)
Provisional Application 62063391 · Oct 13, 2014
Related Publication 20160101865A1 · Apr 14, 2016