Movable ottoman for an aircraft seat

Patent metadata

Field	Value
Publication number	US-11066174-B2
Application number	US-202016797119-A
Country	US
Kind code	B2
Filing date	Feb 21, 2020
Priority date	Apr 9, 2018
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

An aircraft seating unit includes a base, a seat coupled to the base, a housing coupled to the base and enclosing frame elements of at least one of the base or the seat, and an ottoman. The housing defines a recess at a location below and to a rear of the seat. The ottoman is disposed within the recess. The ottoman includes a guide coupled to at least one of the frame elements, a slide translatable along the guide, a foot platform coupled to the slide, and an actuator positioned to facilitate selectively translating the slide along the guide to reposition the foot platform between a stowed position and a deployed position. The guide defines a translation axis that is angled relative to a vertical axis such that the foot platform moves both vertically and horizontally as the slide translates along the guide.

First claim

The invention claimed is:

1. An aircraft seating unit comprising:
a base configured to couple to a deck of an aircraft;
a seat coupled to the base;
a housing coupled to the base and enclosing frame elements of at least one of the base or the seat, wherein the housing defines a recess at a location below and to a rear of the seat; and
an ottoman disposed within the recess, the ottoman including:
a guide coupled to at least one of the frame elements;
a slide translatable along the guide;
a foot platform coupled to the slide, the foot platform including a flat surface defining a horizontal plane;
an actuator positioned to facilitate selectively translating the slide along the guide to reposition the foot platform between a stowed position and a deployed position;
wherein the guide defines a translation axis; and
wherein the translation axis is angled relative to a vertical axis that is perpendicular to the horizontal plane such that the foot platform moves both vertically and horizontally as the slide translates along the guide, wherein the ottoman includes an arm defining a first interface pivotally coupled to the slide, a second interface pivotally coupled to the actuator, and a third interface pivotally coupled to at least one of the frame elements, and wherein engagement of the actuator causes the arm to pivot about the third interface and move the slide along the guide, wherein each of the first, second, and third interfaces remain in a common plane during translation, wherein the common plane is perpendicular to the horizontal plane.

2. The aircraft seating unit of claim 1 , wherein the ottoman includes a bracket having a first plate and a second plate extending from the first plate, and wherein the first plate is coupled to the foot platform and the second plate is coupled to the slide and the first interface of the arm.

3. The aircraft seating unit of claim 1 , wherein the first interface, the second interface, and the third interface are positioned at fixed distances from each other.

4. The aircraft seating unit of claim 1 , wherein an angle between the translation axis and the vertical axis is at most ten degrees.

5. The aircraft seating unit of claim 1 , wherein an angle between the translation axis and the vertical axis is at least ten degrees.

6. The aircraft seating unit of claim 1 , wherein the foot platform includes an angled portion extending downward from the flat surface at an angle.

7. The aircraft seating unit of claim 6 , wherein the flat surface and the angled portion are separate components coupled together by a support.

8. The ottoman of claim 1 , wherein the foot platform is selectively repositionable to any position between the stowed position and a fully-deployed position.

9. The aircraft seating unit of claim 1 , wherein the seat is a first seat, the recess is a first recess, the ottoman is a first ottoman, and the foot platform is a first foot platform, and wherein the housing defines a second recess, further comprising a second seat coupled to the base and a second ottoman disposed within the second recess, the second ottoman including a second foot platform that is selectively deployable from the second recess.

10. A seating unit comprising:
a base;
a seat coupled to the base;
a housing coupled to the base and enclosing frame elements of at least one of the base or the seat, wherein the housing defines a recess; and
an ottoman disposed within the recess, the ottoman including:
a guide coupled to at least one of the frame elements;
a slide translatable along the guide;
a foot platform coupled to the slide;
an actuator; and
an arm having a unitary structure, the arm defining a first interface pivotally coupled to the slide, a second interface pivotally coupled to the actuator, and a third interface pivotally coupled to at least one of the frame elements;
wherein engagement of the actuator causes the arm to pivot about the third interface and move the slide along the guide, wherein the ottoman includes an arm defining a first interface pivotally coupled to the slide, a second interface pivotally coupled to the actuator, and a third interface pivotally coupled to at least one of the frame elements, and wherein engagement of the actuator causes the arm to pivot about the third interface and move the slide along the guide, wherein each of the first, second, and third interfaces remain in a common plane during translation, wherein the common plane is perpendicular to the horizontal plane.

11. The seating unit of claim 10 , wherein the recess is at a location below and to a rear of the seat.

12. A seating unit comprising:
a base;
a seat coupled to the base;
a housing coupled to the base and enclosing frame elements of at least one of the base or the seat, wherein the housing defines a recess at a location below and to a rear of the seat; and
an ottoman disposed within the recess, the ottoman including a foot platform that is selectively deployable from a stowed position to a deployed position, wherein the ottoman further includes:
a guide coupled to at least one of the frame elements;
a slide translatable along the guide, wherein the foot platform is coupled to the slide; and
an actuator positioned to facilitate selectively translating the slide along the guide to reposition the foot platform between the stowed position and the deployed position,
an arm having a unitary structure, the arm defining a first interface pivotally coupled to the slide, a second interface pivotally coupled to the actuator, and a third interface pivotally coupled to at least one of the frame elements, and wherein engagement of the actuator causes the arm to pivot about the third interface and move the slide along the guide, wherein each of the first, second, and third interfaces remain in a common plane during translation, wherein the common plane is perpendicular to the horizontal plane.

13. The seating unit of claim 12 , wherein the ottoman further includes a bracket having a first plate and a second plate extending from the first plate, and wherein the first plate is coupled to the foot platform and the second plate is coupled to the slide and the first interface of the arm.

14. The seating unit of claim 12 , wherein the foot platform includes a horizontal portion and an angled portion extending downward from the horizontal portion at an angle.

15. The seating unit of claim 12 , wherein the foot platform moves both vertically and horizontally along an angled translation path between the stowed position and the deployed position.

16. The seating unit of claim 12 , wherein the seat is a first seat, the recess is a first recess, the ottoman is a first ottoman, and the foot platform is a first foot platform, and wherein the housing defines a second recess, further comprising a second seat coupled to the base and a second ottoman disposed within the second recess, the second ottoman including a second foot platform that is selectively deployable from the second recess.

17. The seating unit of claim 16 , wherein the first foot platform has a first size and the second foot platform has a second size different than the first size.

Assignees

• Be Aerospace Inc

Inventors

• Suhre Ryan J
• Schmid Michael J

Classifications

• B60N3/063

  with adjustment systems · CPC title

• B64D11/0643 Primary

  Adjustable foot or leg rests · CPC title