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Aircraft passenger seat assembly including backrest reclining device

A technology for aircraft passengers and seats, applied in the field of aircraft "sleeper" seats, can solve problems such as difficulty in adjusting and finding, increasing the total weight and restrictions of aircraft seats

Active Publication Date: 2021-09-10
ROCKWELL COLLINS INC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Actuators and associated components such as motors, circuitry, and cables add to the overall weight of an aircraft seat, which can limit the number of sleeper seats that can be added to an aircraft
Additionally, these traditional seats may rely on multiple articulating elements, such as the seat back, headrest, or legrest, for added passenger comfort, which can make it difficult to adjust and find a comfortable position
For example, in these conventional seats, each hinge element may have to be actuated individually and sequentially one by one

Method used

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  • Aircraft passenger seat assembly including backrest reclining device
  • Aircraft passenger seat assembly including backrest reclining device
  • Aircraft passenger seat assembly including backrest reclining device

Examples

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Embodiment Construction

[0014] The description set forth below in conjunction with the accompanying drawings is intended to describe various illustrative embodiments of the disclosed subject matter. Specific features and functions are described in conjunction with each illustrative embodiment; however, it will be apparent to one skilled in the art that the disclosed embodiments can be practiced without each of those specific features and functions.

[0015] Throughout this specification, reference to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the disclosed subject matter. Thus, appearances of the phrases "in one embodiment" or "in an embodiment" in various places throughout this specification are not necessarily referring to the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any suitable manner in one or ...

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PUM

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Abstract

An aircraft passenger seat has a seat back including a lower portion pivotally mounted to a seat bottom and an upper portion rotatably coupled to the lower portion. During an articulated movement of the seat, the upper part may pivot forward relative to the lower part. An inner diaphragm may be positioned between the head restraint and a set of side frame members of the upper section and rotatably coupled to the upper and lower sections to provide support for the upper back and shoulders of a seated occupant. The actuation assembly provides coordinated articulation of the lower, upper, and inner diaphragms to allow the seat to articulate between an upright taxi takeoff and landing (TTOL) and reclined position and allow for more ergonomic seated occupants pose.

Description

[0001] related application [0002] This application claims priority to U.S. Provisional Patent Application Serial No. 62 / 401,014, filed September 28, 2016, entitled "Passenger Seat Back Reclining Apparatus." This application, in its entirety, incorporates by reference the following prior prior patent application by B / E Airlines relating to hinged aircraft seat back frames: filed September 30, 2016, entitled "Segmented Seat for Achieving a Bed Rest Sitting Position" U.S. Patent Application No. 15 / 282,352, entitled "Aircraft Seat with Simultaneous Articulation of Seat Pan and Seat Back," filed April 8, 2014, U.S. Patent Application No. 14 / 247,850 , now U.S. Patent No. 9,284,055. All of the aforementioned applications are hereby incorporated by reference in their entirety. Background technique [0003] The present disclosure relates to deployable aircraft "sleeper" seats, such as those provided in premium cabins (e.g., first class, business class) in passenger aircraft, which ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B60N2/02B23P11/00A47C1/024B64D11/06
CPCB64D11/06395B64D11/064B64D11/0642B64D11/0643B64D11/0648B60N2/2222B64D11/0644B60N2/23B60N2/995B60N2/34Y02T50/40B60N2/02246B64D11/0641
Inventor 迈克尔·贝罗特
Owner ROCKWELL COLLINS INC
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