Aircraft passenger suite privacy screen control apparatus and method

Patent metadata

Field	Value
Publication number	US-10562633-B2
Application number	US-201615294014-A
Country	US
Kind code	B2
Filing date	Oct 14, 2016
Priority date	Oct 14, 2015
Publication date	Feb 18, 2020
Grant date	Feb 18, 2020

Abstract

A control assembly for a pocket-style screen or door. Top and bottom guide rollers carried by the screen travel along adjustable guide rails mounted in the pocket. A magnet assembly includes a stationary magnet mounted in the pocket wall arranged to attract a moveable magnet carried on a cable to facilitate final opening and closing the screen. A damper cooperates with the magnet assembly to decrease the velocity of the screen as it moves into stowed and deployed positions.

First claim

What is claimed is:

1. A screen control apparatus, comprising:
a screen movable between a stowed position within a pocket and a deployed position outside of the pocket;
at least one guide roller carried on the screen arranged to travel along at least one guide rail mounted in the pocket;
a cable routed around a plurality of pulleys rotatably mounted within the pocket, the cable secured to the screen;
a magnet assembly including a stationary magnet mounted within the pocket and a moveable magnet carried on the cable, the moveable magnet movable into and out of magnetic attraction with the stationary magnet as the screen moves between the stowed and deployed positions, the moveable magnet shaped to engage the stationary magnet with increasing magnetic attraction as the moveable magnet further engages the stationary magnet, the stationary magnet being a female conical-shaped magnet and the moveable magnet being a male conical-shaped magnet mounted on the cable, and the stationary magnet being mounted in a tubular guide through which the cable passes; and
a damper assembly mounted within the pocket operable for controlling cable velocity.

2. The screen control apparatus according to claim 1 , wherein the pocket is located within a wall of an aircraft passenger suite, the pocket having a vertical opening facing across an entrance to the passenger suite.

3. The screen control apparatus according to claim 1 , wherein the at least one guide roller comprises a top roller rotatably mounted proximate a top of the screen and a bottom roller rotatably mounted proximate a bottom of the screen, the top roller arranged to travel along a top guide mounted within the pocket above the screen, and the bottom roller arranged to travel along a bottom guide mounted within the pocket below the screen.

4. The screen control apparatus according to claim 3 , wherein the at least one guide roller further comprises a middle roller rotatably mounted proximate a face of the screen, the middle roller arranged to travel along a middle guide mounted within the pocket between the top and bottom guides.

5. The screen control apparatus according to claim 1 , wherein the at least one guide rail is an elongate linear member adjustable at one or both ends to adjust at least one of screen position and trajectory.

6. The screen control apparatus according to claim 1 , further comprising a top cable block securing the cable to the screen proximate a top of the screen, and a bottom cable block securing the cable to the screen proximate a bottom of the screen, the top and bottom cable blocks moveable with the screen.

7. The screen control apparatus according to claim 1 , further comprising a glide sheet arranged between the stationary magnet and the moveable magnet, the glide sheet having a wear surface controlling a distance between the moveable magnet and the stationary magnet.

8. The screen control apparatus according to claim 1 , wherein the cable comprises an in-line turnbuckle for adjusting cable tension.

9. The screen control apparatus according to claim 1 , wherein the damper assembly comprises a plurality of pulleys around which the cable is routed along a non-linear pathway.

10. The screen control apparatus according to claim 1 , wherein the screen is a door, shade, window, or any other rigid or flexible structure adapted to slide between stowed and deployed positions.

11. An aircraft passenger suite, comprising:
a plurality of walls;
an entrance located between spaced ones of the plurality of walls;
a pocket located within one of the plurality of walls, the pocket having a vertical opening facing across the entrance;
a screen movable between a stowed position within the pocket and a deployed position outside of the pocket;
at least one guide roller carried on the screen arranged to travel along at least one guide rail mounted in the pocket;
a cable routed around a plurality of pulleys rotatably mounted within the pocket, the cable secured to the screen;
a magnet assembly including a stationary magnet mounted within the pocket and a moveable magnet carried on the cable, the moveable magnet movable into and out of magnetic attraction with the stationary magnet as the screen moves between the stowed and deployed positions, the moveable magnet shaped to engage the stationary magnet with increasing magnetic attraction as the moveable magnet further engages the stationary magnet, the stationary magnet being a female conical-shaped magnet and the moveable magnet being a male conical-shaped magnet mounted on the cable, and the stationary magnet being mounted in a tubular guide through which the cable passes; and
a damper assembly mounted within the pocket operable for controlling cable velocity.

12. The aircraft passenger suite according to claim 11 , wherein the at least one guide roller comprises a top roller rotatably mounted proximate a top of the screen and a bottom roller rotatably mounted proximate a bottom of the screen, the top roller arranged to travel along a top guide mounted within the pocket above the screen, and the bottom roller arranged to travel along a bottom guide mounted within the pocket below the screen.

13. The aircraft passenger suite according to claim 12 , wherein the at least one guide roller further comprises a middle roller rotatably mounted proximate a face of the screen, the middle roller arranged to travel along a middle guide mounted within the pocket between the top and bottom guides.

14. The aircraft passenger suite according to claim 11 , wherein the at least one guide rail is an elongate linear member adjustable at one or both ends to adjust at least one of screen position and trajectory.

15. The aircraft passenger suite according to claim 11 , further comprising a top cable block securing the cable to the screen proximate a top of the screen, and a bottom cable block securing the cable to the screen proximate a bottom of the screen, the top and bottom cable blocks moveable with the screen.

16. The aircraft passenger suite according to claim 11 , further comprising a glide sheet arranged between the stationary magnet and the moveable magnet, the glide sheet having a wear surface controlling a distance between the moveable magnet and the stationary magnet.

17. The aircraft passenger suite according to claim 11 , wherein the cable comprises an in-line turnbuckle for adjusting cable tension.

18. The aircraft passenger suite according to claim 11 , wherein the damper assembly comprises a plurality of pulleys around which the cable is routed along a non-linear pathway.

Assignees

• Be Aerospace Inc

Inventors

• Kuyper John
• Frost Ian L

Classifications

• B64D11/0602

  Seat modules, i.e. seat systems including furniture separate from the seat itself · CPC title

• B64D11/0604

  including a bed, e.g. cocoon type passenger seat modules · CPC title

• B64D11/0606 Primary

  with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title