Aircraft passenger seat leg rest deployment using path and follower mechanism

Patent metadata

Field	Value
Publication number	US-2022242573-A1
Application number	US-202117161858-A
Country	US
Kind code	A1
Filing date	Jan 29, 2021
Priority date	Jan 29, 2021
Publication date	Aug 4, 2022
Grant date	—

Abstract

A passenger seat incorporating a path and follower mechanism for nonlinear deployment of a passenger leg rest is disclosed. The passenger seat incorporates lightweight tubular members linked to backrest linkages, the backrest linkages driven by a passenger occupying the seat, e.g., via a reclining motion of the seatback. The reclining motion drives the backrest linkages which in turn drive path followers through a curving path such that, as the path follower drives forward or backward, the leg rest deploys at a variable rate between undeployed and fully deployed configurations, consistently providing an optimally relaxing leg position at any point between.

First claim

We claim:

1 . An aircraft passenger seat, comprising:
a seat frame pivotably coupled to a seatback, the seat frame and seatback collectively configured to accommodate at least one passenger; a deployable leg rest configured to accommodate at least one leg of the passenger when not in an undeployed configuration; at least one tubular member extending between a left side and a right side of the passenger seat, the tubular member operatively coupled to the seatback by at least one seatback linkage configured for articulation by a reclining motion of the seatback; at least one path follower operatively coupled to the at least one seatback linkage, the at least one seatback linkage configured to drive the at least one path follower through an arcuate path between a rear endpoint associated with the undeployed configuration of the leg rest and a forward endpoint associated with a fully deployed configuration of the leg rest when the at least one seatback linkage is articulated; and at least one forward mechanism link operatively coupled to the at least one path follower and to the leg rest, the at least one forward mechanism link configured to be driven by the at least one path follower to deploy the leg rest at a variable rate corresponding to the arcuate path.

2 . The passenger seat of claim 1 , wherein the at least one seatback linkage is configured to lock the at least one path follower in one or more intermediate positions between the rear endpoint and the forward endpoint of the arcuate path.

3 . The passenger seat of claim 2 , wherein the one or more intermediate positions include at least one intermediate position associated with a relative minimum of the arcuate path and with a partially deployed configuration of the leg rest.

4 . The passenger seat of claim 1 , wherein the reclining motion of the seatback is manually driven by the passenger.

5 . The passenger seat of claim 1 , further comprising:
at least one motorized actuator operatively coupled to the seatback, wherein the reclining motion of the seatback is driven by the at least one motorized actuator.

6 . The passenger seat of claim 1 , wherein:
the arcuate path includes at least one intermediate point dividing the arcuate path into a first segment and a second segment; and the leg rest is configured for deployment at a first rate corresponding to the first segment and a second rate corresponding to the second segment.

7 . The passenger seat of claim 6 , wherein:
the first rate is an increasing rate of deployment; and the second rate is a decreasing rate of deployment.

Assignees

• Be Aerospace Inc

Inventors

• Bunea Catalin
• Jacob Twinkle V

Classifications

• B64D11/0643 Primary

  Adjustable foot or leg rests · CPC title

• B64D11/064

  Adjustable inclination or position of seats · CPC title

• B64D11/0641

  Seats convertible into beds · CPC title

• Y02T50/40

  Weight reduction · CPC title