CRADLE RECLINE MECHANISM FOR AIRCRAFT PASSENGER SEAT

• US 20170021930A1
• Filed: 10/08/2016
• Published: 01/26/2017
• Est. Priority Date: 04/02/2014
• Status: Abandoned Application

• 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: HENSHAW, Robert J.
• Application Number:
  US15/289,150
• Publication Number:
  US 20170021930A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats

Abstract

In a preferred embodiment, a cradle recline mechanism for an aircraft passenger seat includes a guide mechanism for guiding a seat bottom of the aircraft passenger seat forward and lower as the seat bottom moves from an upright sitting position to a cradle recline sitting position, where a rear portion of the seat bottom is lowered more than a front portion of the seat bottom, causing the seat bottom to angle upwards from a bottom edge of the seat back. A seat back of the passenger seat may be pivotably connected to the seat bottom such that it is pulled forward and down with the movement of the seat bottom, with the recline angle determined by a rigid support mechanism disposed behind the seat back. Passenger weight may be counterbalanced using a moveable control mechanism such as a locking gas spring.

Claims

1. A cradle recline mechanism for an aircraft passenger seat, comprising:

a means for guiding a seat bottom of the aircraft passenger seat forward and lower as the seat bottom moves from an upright sitting position to a cradle recline sitting position, wherein the means for guiding lowers a rear portion of the seat bottom more than a front portion of the seat bottom, causing the seat bottom to angle upwards from a bottom edge of the seat back;

a pivoting attachment mechanism attaching a seat back of the passenger seat to the seat bottom, such that the seat back moves forward and lower with the seat bottom;

a seat support disposed behind the seat back, wherein the seat support maintains an aftmost position of the seat back during movement of the seat back into the cradle recline sitting position; and

a means for counterbalancing passenger weight to return the passenger seat to the upright sitting position and for preventing over-acceleration into the cradle recline sitting position.

2. The cradle recline mechanism of claim 1, wherein the means for preventing over-acceleration comprises a locking gas spring.

3. The cradle recline mechanism of claim 1, wherein the pivoting attachment mechanism comprises mating hinge segments connected by a pin.

4. The cradle recline mechanism of claim 1, wherein the means for guiding comprises at least a first roller configured to roll along a first arcuate roller rack, the first roller rack having a first end positioned higher than a second end.

5. The cradle recline mechanism of claim 4, wherein the means for guiding comprises an arc pivot.

6. The cradle recline mechanism of claim 5, wherein the arc pivot comprises an arcuate toothed side rail attached to the end of the first roller, and a pinion gear.

7. The cradle recline mechanism of claim 1, wherein the rigid seat support comprises a fixed shell support positioned aft of the seat back.

8. An aircraft passenger seat, comprising:

left and right spreaders;

a seat pan mounted between the left and right spreaders;

a seat back pivotably attached to the seat pan;

a fixed seat back support positioned aft of the seat back; and

a set of rollers configured to roll along roller racks, each roller rack including a first end positioned higher than a second end;

wherein the seat pan is mounted to the left and right spreaders via the set of rollers and the roller racks such that, upon moving from an upright sitting position to a reclined sitting position, the rollers move from the first ends of the roller racks to the second ends of the roller rack to lower the seat pan from an upper position to a lower position, wherein a rear portion of the seat bottom is lower than a front portion of the seat bottom in the reclined sitting position.

9. The aircraft passenger seat of claim 8, wherein, upon moving from an upright sitting position to a reclined sitting position, the seat back angles downward with the rear portion of the seat pan, and the fixed seat back support limits a recline angle of the seat back.

10. The aircraft passenger seat of claim 9, wherein the fixed seat back support comprises a fixed shell positioned behind at least the seat back of the passenger seat.

11. The aircraft passenger seat of claim 8, further comprising a passenger weight counterbalancing mechanism for counterbalancing passenger weight to return the seat pan to the upright sitting position and to prevent over acceleration of the seat pan into the reclined sitting position.

12. The aircraft passenger seat of claim 11, wherein the counterbalancing mechanism comprises a tensioner device having a locking function and an unlocking function to lock and to unlock the travel of a rod along a stroke course.

13. The aircraft passenger seat of claim 12, wherein the counterbalancing mechanism accommodates multiple stages of adjustable sitting positions between the upright sitting position and the reclined sitting position.

14. The aircraft passenger seat of claim 11, wherein the counterbalancing mechanism interoperates with the movement of the set of rollers via an arc pivot.

15. The aircraft passenger seat of claim 14, wherein the arc pivot is a virtual pivot mechanism.

16. The aircraft passenger seat of claim 8, further comprising a leg rest pivotably attached to the front of the seat pan.

17. The aircraft passenger seat of claim 16, wherein the leg rest is configured to extend independently of movement into the reclined sitting position.