Console assembly including stowable support surface

Patent metadata

Field	Value
Publication number	US-9878801-B2
Application number	US-201514866164-A
Country	US
Kind code	B2
Filing date	Sep 25, 2015
Priority date	Oct 13, 2014
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

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.

First claim

What is claimed is:

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.

Assignees

• Gulfstream Aerospace Corp
• C&D Aerospace Canada Co

Inventors

• Flynn Tristan
• Loar Todd
• Long Eric
• Strelzyk Conrad
• Clarke Bryan

Classifications

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title