Aircraft seat employing dual actuators for seat translaton and seat recline

• US 9,227,729 B2
• Filed: 04/08/2014
• Issued: 01/05/2016
• Est. Priority Date: 04/08/2013
• Status: Active Grant

• Current Assignee: B/E Aerospace, Inc. (Rtx Corporation)
• Original Assignee: B/E Aerospace, Inc. (Rtx Corporation)
• Inventors: Udriste, Daniel, De La Garza, Javier Valdes, Beroth, Michael
• Primary Examiner(s): Plummer, Elizabeth A
• Application Number:
  US14/247,745
• Publication Number:
  US 20140300162A1
• Time in Patent Office: 637 Days
• Field of Search: 297/317, 297/320, 297/322, 297/354.13
• US Class Current: 1/1
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/06395 characterised by the arrangement of electric motors for adjustment
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats

Abstract

An aircraft passenger seat including a seat base frame, a seatback and a seat bottom configured to horizontally translate relative to the seat base frame, a first actuator arranged to drive seat translation, and a second actuator arranged to drive seatback recline, the dual actuators working in parallel to increase the speed of horizontal translation and combine the recline function into one continuous motion.

Claims

1. An aircraft passenger seat configured to recline, comprising:

a fixed base frame;

a seatback pivotally connected to a seat bottom;

a first actuator arranged to drive horizontal translation of a first rail relative to the fixed base frame to horizontally translate the seatback and the seat bottom relative to the fixed base frame independent of seat recline; and

a second actuator arranged to drive horizontal translation of a second rail relative to the first rail to drive seat recline including both seatback and seat bottom angular adjustment;

wherein the first and second actuators are arranged in parallel to drive seatback and seat bottom horizontal translation and seat recline in one continuous motion.

2. The aircraft passenger seat of claim 1, wherein the first rail defines a non-linear guide path for guiding movement of the seat bottom engaged therein, and the second rail is arranged to move the seat bottom along the non-linear guide path.

3. The aircraft passenger seat of claim 2, wherein the seat bottom moves from a rearward end of the non-linear guide path when the second actuator is retracted and the seatback is upright, to a forward end of the non-linear guide path when the second actuator is fully extended and the seatback fully reclined.

4. The aircraft passenger seat of claim 1, wherein the seatback and the seat bottom are pivotally attached, and the seatback is attached to the first rail through a rotating link.

5. The aircraft passenger seat of claim 4, wherein the second actuator is attached to a forward end of the seat bottom such that extending the second actuator moves the seat bottom forward, thereby pulling the seatback along therewith such that the rotating link rotates to recline the seatback.

6. The aircraft passenger seat of claim 1, wherein the fixed base frame comprises spaced legs and transverse forward and rear beam tubes.

7. An aircraft passenger seat configured to recline and horizontally translate, comprising:

a seat base frame;

a seatback and a seat bottom configured to horizontally translate relative to the seat base frame;

a first actuator arranged to drive a first rail to drive seatback and seat bottom horizontal translation relative to the seat base frame independent of seat recline; and

a second actuator arranged to drive a second rail to drive seat recline, the second rail arranged to horizontally translate relative to the first rail to angularly adjust both the seatback and the seat bottom;

the first and second actuators working in parallel to increase the speed of horizontal translation and combine seat recline into one continuous motion.

8. The aircraft passenger seat of claim 7, wherein the first rail defines a non-linear guide path for guiding movement of the seat bottom engaged therein, and the second rail is arranged to move the seat bottom along the non-linear guide path.

9. The aircraft passenger seat of claim 8, wherein the seat bottom travels from one end of the non-linear guide path to the other as the seatback moves from a fully upright to a fully reclined sitting position.

10. The aircraft passenger seat of claim 7, wherein the seatback and the seat bottom are pivotally attached, and the seatback is attached to the first rail through a rotating link.

11. The aircraft passenger seat of claim 10, wherein the second actuator is attached to a forward end of the seat bottom such that extending the second actuator moves the seat bottom forward, thereby pulling the seatback along therewith such that the rotating link rotates to recline the seatback.

12. The aircraft passenger seat of claim 7, wherein the first and second actuators operate together to speed seatback translation and recline.

13. The aircraft passenger seat of claim 7, wherein the seat base frame is fixed and comprises spaced legs interconnected through transverse forward and rear beam tubes.