Aircraft armrest rail roller linkage apparatus

US9845156B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9845156-B2
Application numberUS-201615148531-A
CountryUS
Kind codeB2
Filing dateMay 6, 2016
Priority dateMay 11, 2015
Publication dateDec 19, 2017
Grant dateDec 19, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

An aircraft armrest may incorporate a rail roller linkage. The roller linkage may include an armrest plate, a rail attached to an aircraft seat assembly, a top roller link, and a bottom roller link. The top roller link may have a threaded upper adjustment cylinder, a pivot joint, and a pair of grooved rollers diagonally disposed on either side of the pivot. The bottom roller link may have an unthreaded lower adjustment cylinder, a pivot joint, and a pair of grooved rollers diagonally disposed on either side of the pivot. The grooved rollers may mesh with the rail. The roller linkage may include a roller adjustment screw, having a threaded portion, and extending through both of the adjustment cylinders. A compression spring may bias the roller link around the rail and may be disposed between the top roller link and the bottom roller link and surrounding the roller adjustment screw.

First claim

Opening claim text (preview).

What is claimed is: 1. An aircraft armrest rail roller linkage apparatus comprising: (a) an armrest plate for attaching to an armrest assembly; (b) a rail attached to an aircraft seat assembly; (c) a top roller link, attached to the armrest plate, having an upper adjustment cylinder that is threaded and also having a pivot joint and a pair of grooved rollers diagonally disposed on either side of the pivot, the grooves meshing with the rail; (d) a bottom roller link attached to the armrest plate, having a lower adjustment cylinder that is unthreaded and also having a pivot joint and a pair of grooved rollers diagonally disposed on either side of the pivot, the grooves meshing with the rail; (e) a roller adjustment screw, having a threaded portion, and extending through both the upper and the lower adjustment cylinders, the threaded portion of the roller adjustment screw meshing with the threaded portion of the upper adjustment cylinder; (f) a compression spring, biasing the top and bottom roller links around the rail, disposed between the top roller link and the bottom roller link and surrounding the roller adjustment screw; and (f) wherein the respective pivot joints of the top roller link and the bottom roller link are positioned on opposite sides of the rail.

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What does patent US9845156B2 cover?
An aircraft armrest may incorporate a rail roller linkage. The roller linkage may include an armrest plate, a rail attached to an aircraft seat assembly, a top roller link, and a bottom roller link. The top roller link may have a threaded upper adjustment cylinder, a pivot joint, and a pair of grooved rollers diagonally disposed on either side of the pivot. The bottom roller link may have an un…
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification B64D11/0644. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 19 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).