Flexible lumbar support of aircraft seat

Patent metadata

Field	Value
Publication number	US-9796308-B2
Application number	US-201514704184-A
Country	US
Kind code	B2
Filing date	May 5, 2015
Priority date	May 5, 2015
Publication date	Oct 24, 2017
Grant date	Oct 24, 2017

Abstract

A flexible lumbar support for an aircraft seat includes a frame and flexible seat pad connected thereto for supporting a seat user. At least first and second rods are spaced from each other and the frame, extend across and are secured to the seat pad, and define respectively at least first and second control lines about which the seat pad is rotatable. A third rod is spaced from the seat pad, extends across and is secured to the frame, and defines a third control line. At least a first actuator extends between and is attached to the first and third rods. A second actuator extends between and is attached to the second and third rods. The actuators are movable along the frame and pivotable about the third control line for allowing a change of respective positions of the control lines to generate multiple profiles of the flexible lumbar support.

First claim

What is claimed:

1. A flexible lumbar support for use in a seat of an aircraft, the flexible lumbar support comprising:
a frame;
a flexible seat pad connected to the frame and configured to support a user of the seat;
at least first and second rods spaced from each other and the frame, extending across and secured to the seat pad, and defining respectively at least first and second control lines about which the seat pad is configured to rotate and a third rod spaced from the seat pad, extending across and secured to the frame, and defining a third control line; and
a first actuator extending between and attached to the first and third rods and a second actuator extending between and attached to the second and third rods, the actuators being connected to the third rod at or adjacent a common point of attachment between the first actuator, the second actuator and the third rod, the actuators configured to move along the frame and pivot about the third control line for allowing a change of respective positions of the control lines to generate multiple profiles of the flexible lumbar support.

2. The flexible lumbar support of claim 1 , wherein the flexible lumbar support comprises further a fourth control line extending across an upper portion of the frame and about which a top segment of the seat pad is configured to rotate.

3. The flexible lumbar support of claim 2 , wherein the flexible lumbar support further defines a fifth control line extending across a lower portion of the frame and about which a bottom segment of the seat pad is configured to rotate.

4. The flexible lumbar support of claim 3 , wherein the first actuator fixes a distance between the first and fourth control lines and the second actuator fixes a distance between the second and fifth control lines, a middle segment of the seat pad is free to slide against the top and bottom segments, and a distance between the first and second control lines accommodates generation of multiple profiles of the flexible lumbar support.

5. The flexible lumbar support of claim 1 , wherein each of the actuators comprises at least one of a piston and a cylinder assembly with one or more of spring-loaded cable-crank mechanisms, a ratchet-and-pinion mechanism, and an electrically driven actuator and each of the actuators acts as a corresponding load-carrying member from the seat pad to the frame.

6. The flexible lumbar support of claim 1 , wherein the flexible lumbar support comprises further a rotatable mechanism configured to lock the third rod onto the frame.

7. The flexible lumbar support of claim 1 , wherein the frame includes a vertical section defining a generally rectangular longitudinal cross-section and representing a vertical axis of the frame and a horizontal section defining a generally open-sided rectangular longitudinal cross-section, the vertical section is larger than the horizontal section, and a plane defined by the vertical section is generally perpendicular to a plane defined by the horizontal section.

8. The flexible lumbar support of claim 7 , wherein the seat pad defines a generally rectangular longitudinal cross-section and extends from an upper portion of the vertical section of the frame to an outer portion of the horizontal section of the frame defined opposite the vertical section.

9. A seat of an aircraft comprising:
a flexible lumbar support including:
a frame having a pair of spaced, generally parallel vertical rails, a pair of spaced, generally parallel upper and lower horizontal rails respectively extend between corresponding upper and lower ends of the vertical rails, and a pair of opposed, spaced, generally parallel base rails respectively extending from ends of the lower horizontal rail;
a flexible seat pad having a top segment suspended from the upper horizontal rail, a bottom segment disposed between and connected to the base rails, and a middle segment extending between the top segment and the bottom segment, the middle segment having first and second support pads;
first and second rods spaced from each other and the frame, the first and second rods extending across and secured to the middle segment by the first and second support pads, respectively, and defining respectively at least first and second control lines about which the seat pad is configured to rotate and a third rod spaced from the seat pad, extending across and secured to the vertical rails of the frame, and defining a third control line that is locked onto at least one vertical rail of the frame by a rotatable mechanism; and
a first actuator extending between and attached to the first and third rods and a second actuator extending between and attached to the second and third rods, the actuators being attached to the third rod at or adjacent the rotatable mechanism.

10. The aircraft seat of claim 9 , wherein the flexible lumbar support comprises further a fourth control line extending across an upper portion of the frame and about which the top segment of the seat pad is configured to rotate.

11. The aircraft seat of claim 10 , wherein the flexible lumbar support further defines a fifth control line extending across a lower portion of the frame and about which the bottom segment of the seat pad is configured to rotate.

12. The aircraft seat of claim 11 , wherein the first actuator fixes a distance between the first and fourth control lines and the second actuator fixes a distance between the second and fifth control lines, a middle segment of the seat pad is free to slide against the top and bottom segments, and a distance between the first and second control lines accommodates generation of multiple profiles of the flexible lumbar support.

13. The aircraft seat of claim 9 , wherein each of the actuators comprises at least one of a piston and a cylinder assembly with one or more of spring-loaded cable-crank mechanisms, a ratchet-and-pinion mechanism, and an electrically driven actuator and each of the actuators acts as a corresponding load-carrying member from the seat pad to the frame.

Assignees

• Hamilton Sundstrand Corp
• Ami Ind Inc

Inventors

• Agarwal Ashish Kumar
• Panda Satya Swaroop

Classifications

• B60N2/66 Primary

  Lumbar supports · CPC title

• B64D11/00 Primary

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title

• B64D11/0639

  with features for adjustment or converting of seats · CPC title

• B64D11/0647

  Seats characterised by special upholstery or cushioning features · CPC title

• B64D11/06

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title