Spring loaded seat bottom which locks during taxi, take-off and landing

• US 9,926,079 B2
• Filed: 03/17/2016
• Issued: 03/27/2018
• Est. Priority Date: 03/17/2015
• Status: Expired due to Fees

• Current Assignee: B/E Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: B/E Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Baker, Cameron, Darbyshire, Martin
• Primary Examiner(s): Brindley, Timothy J
• Application Number:
  US15/073,115
• Publication Number:
  US 20160272324A1
• Time in Patent Office: 740 Days
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats

Abstract

An aircraft passenger seat having a seat bottom movable between a stationary position for taxi, take-off and landing and a movable position during flight in which at least one of a leading edge and a trailing edge of the seat bottom deflects downward in response to a downward load applied thereto.

Claims

1. An aircraft passenger seat, comprising:

a seat bottom movable between a stationary position for taxi, take-off and landing and a movable position during flight in which at least one of a leading edge and a trailing edge of the seat bottom deflects downward in response to a downward load applied thereto, the seat bottom comprising a seat bottom frame positioned between spaced spreaders; and

a linkage and spring assembly packaged on an inboard side of each of the spaced spreaders, each linkage and spring assembly comprising;

a hinge block attached to the inboard side of the respective spreader;

a link pivotably attached at one end to the hinge block; and

a spring disposed between a free end of the link and a spring seat defined in the respective spreader, the spring arranged to bias the link upward in a direction of the seat bottom.

2. The aircraft passenger seat of claim 1, wherein the seat bottom frame comprises:

spaced frame members;

a front beam, a near front beam, and a rear beam interconnecting the spaced frame members; and

a flexible diaphragm spanning the front beam, the near front beam and the rear beam.

3. The aircraft passenger seat of claim 2, wherein the flexible diaphragm is held in a tensioned state, and wherein the rear beam and the near front beam are spaced apart to allow the flexible diaphragm to deflect downward therebetween and the front beam and the near front beam are positioned close together to prevent the flexible diaphragm from deflecting near a front of the seat bottom frame.

4. The aircraft passenger seat of claim 2, wherein each of the spaced frame members are curved or angled.

5. The aircraft passenger seat of claim 1, wherein the spring is a vertically-oriented helical spring.

6. The aircraft passenger seat of claim 1, wherein the seat bottom frame further comprises a vertically-oriented roller rotatably carried on each of the frame members, the vertically-oriented rollers arranged to travel along a top of the links as the seat bottom moves horizontally between the stationary position and the movable position.

7. The aircraft passenger seat of claim 6, wherein in the stationary position the vertically-oriented rollers are positioned vertically above the hinge blocks such that the downward load does not act on the links, and in the movable position the vertically-oriented rollers travel forward along the top of the links causing the free end of the links to pivot downward in response to the downward load.

8. The aircraft passenger seat of claim 1, wherein the link defines a linear portion along which the vertically-oriented roller travels and the free end of the link is shaped to capture the spring between a bottom of the link and the spring seat.

9. An aircraft passenger seat, comprising:

a reclining seat back;

spaced spreaders;

a seat bottom comprising a seat bottom frame positioned between the spaced spreaders, the seat bottom configured to translate between a first position in which the seat bottom is stationary and a second position in which at least one of a leading edge and a trailing edge of the seat bottom moves downward in response to a downward load applied thereto and recovers upward upon removal of the downward load; and

a linkage and spring assembly packaged on an inboard side of at least one of the spaced spreaders, the linkage and spring assembly comprising;

a hinge block attached to the inboard side of the respective spreader;

a link pivotably attached at one end to the hinge block; and

a biasing member disposed between a free end of the link and a biasing member seat defined in the respective spreader, the biasing member arranged to bias the link upward in a direction of the seat bottom.

10. The aircraft passenger seat of claim 9, wherein the seat bottom frame comprises:

spaced left and right frame members;

a front beam, a near front beam, and a rear beam interconnecting the spaced left and right frame members; and

a flexible diaphragm spanning the front beam, the near front beam and the rear beam.

11. The aircraft passenger seat of claim 10, wherein the flexible diaphragm is held in a tensioned state, and wherein the rear beam and the near front beam are spaced apart to allow the flexible diaphragm to deflect downward therebetween and the front beam and the near front beam are positioned close together to prevent the flexible diaphragm from deflecting near a front of the seat bottom frame.

12. The aircraft passenger seat of claim 10, wherein each of the spaced left and right frame members are curved or angled.

13. The aircraft passenger seat of claim 9, wherein the biasing member is a vertically-oriented helical spring.

14. The aircraft passenger seat of claim 9, wherein the seat bottom frame further comprises a vertically-oriented roller rotatably carried on one of the frame members, the vertically-oriented roller arranged to travel along a top of the link as the seat bottom translates between the first position and the second position, the first position for use during aircraft taxi, take-off and landing and the second position for use during flight.

15. The aircraft passenger seat of claim 14, wherein in the first position the vertically-oriented roller is positioned vertically above the hinge block such that the downward load does not act on the link, and in the second position the vertically-oriented roller travels forward along the top of the link thereby causing the free end of the link to pivot downward in response to the downward load.

16. The aircraft passenger seat of claim 9, wherein the link defines a linear portion along which the vertically-oriented roller travels and the free end of the link is shaped to capture the biasing member between a bottom of the link and the biasing member seat.