Passenger positioning devices for aircraft seats for regulatory compliance

Patent metadata

Field	Value
Publication number	US-12054263-B2
Application number	US-202217576653-A
Country	US
Kind code	B2
Filing date	Jan 14, 2022
Priority date	Jan 14, 2022
Publication date	Aug 6, 2024
Grant date	Aug 6, 2024

Abstract

An aircraft passenger seat installable in an aircraft cabin at an angle relative to an aircraft longitudinal axis. The passenger seat includes movable or shape changing seat elements for temporarily re-indexing the passenger orientation according to at least one predetermined flight condition such that the seat assembly meets predefined regulatory certification criteria in at least one of the predetermined flight conditions. A method for effecting a temporary change in position of a seated passenger relative to the aircraft longitudinal axis (i.e., direction of flight) according to at least one predetermined flight condition.

First claim

What is claimed is:

1. An aircraft passenger seat installed in an aircraft cabin at an offset angle relative to a vertical plane along an aircraft longitudinal axis, the aircraft passenger seat comprising:
a backrest comprising a first device configured to effect a change in the backrest to change an angle of a seated passenger relative to the aircraft longitudinal axis, the change in the backrest including movement of one side of a front of the backrest relative to an opposing side of the front of the backrest to change an angle of the front of the backrest relative to the vertical plane along the aircraft longitudinal axis;
a seat bottom including a second device configured to effect a change in the seat bottom to change an angle of the seated passenger relative to the aircraft longitudinal axis, the change in the seat bottom including movement of one side of a forward end of the seat bottom relative to an opposing side of the forward end of the seat bottom to change an angle of the forward end of the seat bottom relative to the vertical plane along the aircraft longitudinal axis; and
a controller communicatively coupled to each of the first and second devices, the controller configured to actuate the first and second devices according to at least one aircraft flight condition.

2. The aircraft passenger seat according to claim 1 , wherein:
in a taxi, takeoff, and landing (TTOL) aircraft flight condition, the backrest and the seat bottom are shaped to position the seated passenger at a first angle relative to the vertical plane along the aircraft longitudinal axis; and
in a non-TTOL aircraft flight condition, the controller is configured to actuate each of the first and second devices to effect the change in the respective backrest and the seat bottom to position the seated passenger at a second angle relative to the vertical plane along the aircraft longitudinal axis;
wherein the second angle is greater than the first angle.

3. The aircraft passenger seat according to claim 2 , wherein:
the first device is a first air bladder, incorporated within or positioned in relation to the backrest, configured to be inflated to change the shape of the backrest to position the seated passenger at the first angle, and configured to be deflated to change the shape of the backrest to position the seated passenger at the second angle;
the second device is a second air bladder, incorporated within or positioned in relation to the seat bottom, configured to be inflated to change the shape of the seat bottom to position the seated passenger at the first angle, and configured to be deflated to change the shape of the seat bottom to position the seated passenger at the second angle; and
the controller is configured to cause each of the first and second air bladders to be inflated in preparation for or responsive to the TTOL aircraft flight condition and each of the bladders to be deflated in preparation for or responsive to the non- TTOL flight condition.

4. The aircraft passenger seat according to claim 3 , wherein:
inflating the first air bladder causes forward movement of one side of the backrest; and
inflating the second air bladder causes forward movement of one side of the forward end of the seat bottom.

5. The aircraft passenger seat according to claim 3 , wherein each of the first and second air bladders are wedge-shaped such that inflation causes re-indexing of the seated passenger for TTOL and deflation causes re-indexing of the seated passenger for flight.

6. The aircraft passenger seat according to claim 2 , wherein:
the first device is a first actuator, positioned in relation to the backrest, configured to move one side of the backrest forward to position the seated passenger at the first angle, and configured to move the one side of the backrest rearward to position the seated passenger at the second angle; and
the second device is a second actuator, positioned in relation to the seat bottom, configured to move one side of a forward end of the bottom forward to position the seated passenger at the first angle, and configured to move the one side of the forward end rearward to position the seated passenger at the second angle.

7. The aircraft passenger seat according to claim 1 , wherein:
a first condition of the aircraft passenger seat corresponds to a TTOL-compliant seat angle in which the angle of the seated passenger, determined by the backrest and the seat bottom, is 45° or relative to the vertical plane along the aircraft longitudinal axis; and
a second condition of the aircraft passenger seat corresponds to a TTOL-non-compliant seat angle in which the angle of the seated passenger, determined by the backrest and the seat bottom, is greater than 45° relative to the vertical plane along the aircraft longitudinal axis.

8. The aircraft passenger seat according to claim 1 , wherein:
actuation of the first and second devices is coordinated by the controller;
a first condition of each of the first and second devices corresponds to a taxi, takeoff and landing (TTOL) condition of the aircraft passenger seat; and
a second condition of each of the first and second devices corresponds to a flight condition of the aircraft passenger seat.

9. The aircraft passenger seat according to claim 1 , wherein:
the first device is coupled to the backrest and extends in a vertical direction of the backrest, wherein rotation of the first device effects rotational movement of the backrest to decrease the angle of the backrest relative to the vertical plane along the aircraft longitudinal axis;
the second device is coupled to the seat bottom and is rotatable about a vertical axis such that rotation of the second device effects rotational movement of the seat bottom to decrease an angle of a forward end of the seat bottom relative to the vertical plane along the aircraft longitudinal axis; and
rotation of the first and second devices is coordinated.

10. The aircraft passenger seat according to claim 1 , further comprising a passenger restraint including first and second attachment points asymmetrically positioned on opposite sides of the seat bottom.

11. The aircraft passenger seat according to claim 1 , further comprising a frame supporting each of the backrest and the seat bottom, wherein the frame is rotationally fixed about a vertical axis of the frame.

12. A method for effecting a temporary position change of a seated passenger relative to a vertical plane along an aircraft longitudinal axis, comprising the steps of:
providing a seat assembly comprising:
a backrest comprising a first device configured to effect a change in the backrest to change an angle of a seated passenger relative to the aircraft longitudinal axis, the change in the backrest including movement of one side of a front of the backrest relative to an opposing side of the front of the backrest to change an angle of the front of the backrest relative to the vertical plane along the aircraft longitudinal axis;

a seat bottom including a second device configured to effect a change in the seat bottom to change an angle of the seated passenger relative to the aircraft longitudinal axis, the change in the seat bottom including movement of one side of a forward end of the seat bottom relative to an opposing side of the forward end of the seat bottom to change an angle of the forward end of the seat bottom relative to the vertical plane along the aircraft longitudinal axis; and
a controller communicatively coupled to each of the first and second devices, the controller configured to actuate the first and second devices according to at least one aircraft flight condition;
positioning the seat assembly in an aircraft

Assignees

• Be Aerospace Inc

Inventors

• Dowty Mark B
• Pence Tracy N
• Wyss Alen

Classifications

• B64D11/0639

  with features for adjustment or converting of seats · CPC title

• B64D11/0601 Primary

  Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight · CPC title

• B60N2/14

  rotatable, e.g. to permit easy access (B60N2/10 {, B60N2/2869} take precedence) · CPC title

• B64D11/064 Primary

  Adjustable inclination or position of seats · CPC title