Friction stop device

Patent metadata

Field	Value
Publication number	US-9989191-B2
Application number	US-201414903106-A
Country	US
Kind code	B2
Filing date	Jul 9, 2014
Priority date	Jul 9, 2013
Publication date	Jun 5, 2018
Grant date	Jun 5, 2018

Abstract

Deployment apparatus ( 10 ) including a deployment object ( 12 ), a deployment arm ( 16 ) with a first end ( 22 ) coupled to the deployment object and a second end ( 24 ) having a pivot ( 26 ), and a hinge assembly ( 18 ) rotatably attached to the pivot of the deployment arm. The hinge assembly ( 18 ) includes an enclosure ( 44 ) and a friction stop device ( 82 ) disposed within the enclosure such that the friction stop device includes a friction portion ( 80 ) configured to be pressed against a lateral surface of the pivot ( 26 ) of the deployment arm such that the friction portion provides a predetermined torque. The predetermined torque may be calculated based on maintaining a deployed angle of the deployment arm ( 16 ) such that the deployment object ( 12 ) is held in a raised deployed position.

First claim

That which is claimed is:

1. A deployment apparatus comprising:
a deployment object;
a deployment arm with a first end coupled to the deployment object and a second end having a pivot; and
a hinge assembly rotatably attached to the pivot of the deployment arm, the hinge assembly comprising a deployment arm mount, an enclosure, and a friction stop device disposed within the enclosure, the friction stop device comprising a friction portion configured to be pressed against a lateral surface of the pivot of the deployment arm such that the friction portion provides a predetermined torque,
wherein the deployment arm mount comprises at least two tracks that are slidingly engaged with a plurality of linear bearings on a surface of the enclosure.

2. The deployment apparatus of claim 1 , wherein the predetermined torque is calculated based on maintaining a deployed angle of the deployment arm such that the deployment object is held in a raised deployed position.

3. The deployment apparatus of claim 1 , wherein the friction portion is disposed axially with respect to a rotational axis at the second end of the deployment arm.

4. The deployment apparatus of claim 1 , wherein the friction stop device further comprises a first backing plate bonded to the friction portion.

5. The deployment apparatus of claim 1 , wherein the friction stop device further comprises one or more Belleville washers configured to maintain a compression load on the friction portion.

6. The deployment apparatus of claim 1 , wherein the hinge assembly further comprises one or more set screws configured to change a compression load on the friction portion.

7. The deployment apparatus of claim 1 , wherein the deployment object is selected from the group consisting of a display monitor, a tray table, and a cocktail table.

8. The deployment apparatus of claim 1 , wherein the hinge assembly further comprises a gas spring coupled at one end to the enclosure and coupled at an opposing end to the deployment arm mount.

9. The deployment apparatus of claim 1 , wherein the friction portion comprises a centrally located substantially square hole.

10. The deployment apparatus of claim 1 , wherein the friction portion comprises a cylindrical outer surface except for one or more flat surfaces.

11. The deployment apparatus of claim 1 , wherein the hinge assembly further comprises a mechanical lockout configured to maintain the deployment object in a deployed position.

12. The deployment apparatus of claim 11 , wherein the mechanical lockout comprises a projection configured to engage a notch.

13. A deployment apparatus comprising:
a deployment object;
a deployment arm with a first end coupled to the deployment object; and
a hinge assembly that is rotatably attached to a second end of the deployment arm, the hinge assembly comprising:
an enclosure;
a friction stop device disposed within the enclosure, the friction stop device comprising a friction portion disposed axially with respect to a rotational axis at the second end of the deployment arm;
a first backing plate bonded to the friction portion;
one or more Belleville washers disposed adjacent to the first backing plate and configured to maintain a compression load on the friction portion;
a second backing plate disposed adjacent to the one or more Belleville washers; and
one or more set screws configured to press against the second backing plate to change the compression load on the friction portion,

wherein the friction portion is configured to be pressed against a lateral surface of the second end of the deployment arm such that the friction portion provides a predetermined torque.

14. A passenger seat comprising:
a deployment apparatus comprising:
a deployment object;
a deployment arm with a first end coupled to the deployment object and a second end having a pivot; and
a hinge assembly rotatably attached to the pivot of the deployment arm, the hinge assembly comprising a deployment arm mount, an enclosure, and a friction stop device disposed within the enclosure, the friction stop device comprising a friction portion configured to be pressed against a lateral surface of the pivot of the deployment arm such that the friction portion provides a predetermined torque,

wherein the deployment arm mount comprises at least two tracks that are slidingly engaged with a plurality of linear bearings on a surface of the enclosure.

15. The passenger seat of claim 14 , wherein the predetermined torque is calculated based on maintaining a deployed angle of the deployment arm such that the deployment object is held in a raised deployed position.

16. The passenger seat of claim 14 , wherein the friction portion is disposed axially with respect to a rotational axis at the second end of the deployment arm.

17. The passenger seat of claim 14 , wherein the friction stop device further comprises a first backing plate bonded to the friction portion.

18. The passenger seat of claim 14 , wherein the friction stop device further comprises one or more Belleville washers configured to maintain a compression load on the friction portion.

19. The passenger seat of claim 14 , wherein the hinge assembly further comprises one or more set screws configured to change a compression load on the friction portion.

Assignees

• Zodiac Seats Us Llc

Inventors

• Parker Ty W
• Johnston Jeffrey
• Zemler Matthew K
• Delgadillo Sebastian S
• Jones Matt

Classifications

• F16M11/2021

  around a horizontal axis (F16M11/2035 takes precedence) · CPC title

• F16M11/126

  for tilting and panning (F16M11/14 takes precedence) · CPC title

• B64D11/00151

  Permanently mounted seat back monitors · CPC title

• B60R2011/0085

  with adjustment by rotation in their operational position · CPC title

• F16M11/18

  with mechanism for moving the apparatus relatively to the stand · CPC title