Aircraft armrest rail roller linkage apparatus
09845156 ยท 2017-12-19
Assignee
Inventors
Cpc classification
International classification
F16M13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D11/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
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.
Claims
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.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Features, aspects and advantages of the present invention are understood when the following detailed description of the invention is read with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION OF THE INVENTION
Prior Art FIGS. 1, 1A, 2, and 2A
(19) Referring to the prior art figures,
Preferred Embodiment and Best Mode FIGS. 3-12
(20) The present invention will now be described more fully hereinafter with reference to the accompanying drawings in which exemplary embodiments of the invention are shown. However, the invention may be embodied in many different forms and should not be construed as limited to the representative embodiments set forth herein. The exemplary embodiments are provided so that this disclosure will be both thorough and complete, and will fully convey the scope of the invention and enable one of ordinary skill in the art to make, use and practice the invention. Like reference numbers refer to like elements throughout the various drawings.
(21) Referring to the
(22) As shown in
(23) As shown in
(24) As shown in exploded
(25) As shown in
(26) As shown in
(27) Combining result of above is turning of roller adjustment screw 50 in direction 56 brings all rollers 40 towards rail 20 and it is directly proportional. More turns in direction 56 applies more force of rollers 40 on rail 20. The reverse of this procedure applies less force.
(28) Compression spring 52 is also acting as anti-rotation force on roller adjustment screw 50 by applying constant pressure on both adjustment cylinders 26, 28 and avoids backing-off of roller adjustment screw 50 due to any vibration during normal mechanism operation.
(29) An aircraft armrest rail roller linkage 10 according to the invention has been described with reference to specific embodiments and examples. Various details of the invention may be changed without departing from the scope of the invention. Furthermore, the foregoing description of the preferred embodiments of the invention and best mode for practicing the invention are provided for the purpose of illustration only and not for the purpose of limitation, the invention being defined by the claims. It is envisioned that other embodiments may perform similar functions and/or achieve similar results. Any and all such equivalent embodiments and examples are within the scope of the present invention and are intended to be covered by the appended claims.