Stowable elevated footstep for an aircraft galley

US9975621B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9975621-B2
Application numberUS-201615081700-A
CountryUS
Kind codeB2
Filing dateMar 25, 2016
Priority dateApr 1, 2015
Publication dateMay 22, 2018
Grant dateMay 22, 2018

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  1. Title

    What the patent document calls the invention.

  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

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present invention is an improved footstep for an aircraft galley or similar monument that is retractable into the galley when not in use. The overall size of the footstep is significantly reduced by the use of a spring loaded detent mechanism. The present invention is designed to allow the footstep to remain in the deployed, horizontal position by means of a spring and plunger that cooperate to create a detent or over-center position. Further, the present invention permits the footstep to automatically return to the stowed position by virtue of the spring and plunger detent system.

First claim

Opening claim text (preview).

I claim: 1. A pivoting step assembly adapted to be mounted within a recess of a wall structure having a substantially vertical, planar presentation, the pivoting step assembly comprising: a step having spaced apart retainer plates at a first end, the retainer plates each having a circular profile along a first surface and a central bore therethrough; a base having a lug plate that is disposed between the retainer plates of the step, and first and second circular shoulders for receiving the spaced apart retainer plates, and an aperture in the lug plate aligned with the central bores in the retainer plates; a pin passing through the retainer plates and the lug plate at the central bores and aperture, respectively, such that the step is configured to pivot about the pin between a stowed vertical position adapted to be within the wall structure and a deployed horizontal position adapted to extend from the wall structure; a restoring system for urging the step to move from the deployed horizontal position to the stowed vertical position, the restoring system comprising a spring member disposed in a bore of the step, a lever pinned to the base and partially extending into the bore of the step, and a ball disposed between an unpinned end of the lever and one end of the spring member, where the spring is adapted to be compressed by the ball as the step rotates from the stowed vertical position to the deployed horizontal position. 2. The pivoting step assembly of claim 1 , wherein the step includes a toe at a second end adapted to extend from the wall structure when the step is in the stowed vertical position. 3. The pivoting step assembly of claim 1 , further comprising at least one magnet incorporated into the base adapted to maintain the step in the stowed vertical position when not in use. 4. The pivoting step assembly of claim 1 , wherein the lever resides at least partially in an open slot along a front surface of the lug plate. 5. The pivoting step assembly of claim 1 , where the wall structure is an aircraft galley. 6. The pivoting step assembly of claim 1 , where the restoring system is neutralized when the step is in the deployed horizontal position. 7. The pivoting step assembly of claim 1 , wherein the step has an arched first surface and a substantially planar second surface, the second surface bearing against the base when the step is in the stowed vertical position. 8. The pivoting step assembly of claim 1 , wherein the base includes a stop that bears against a ledge of the step when the step is in the deployed horizontal position to prevent further rotation of the step relative to the base. 9. The pivoting step assembly of claim 1 , wherein the step has first and second cavities that extend substantially a length of the step on respective first and second sides. 10. The pivoting step assembly of claim 1 , further comprising first and second stabilizing members disposed in annular recesses of the lug plate about the aperture, the first and second stabilizing members seated between the retainer plates and the lug plate.

Assignees

Inventors

Classifications

  • in the form of climbing irons or the like {(built-in climbing irons for poles A63B27/00; built-in climbing devices as construction element E04F11/00)} · CPC title

  • having tip-up steps · CPC title

  • Ladders in use as furniture or ladders in relation to furniture, e.g. in cupboards (step-stools, chairs or benches requiring conversion between the step and seat functions A47C12/02) · CPC title

  • Galleys · CPC title

  • B64C1/24Primary

    Steps mounted on, and retractable within, fuselages · CPC title

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Frequently asked questions

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What does patent US9975621B2 cover?
The present invention is an improved footstep for an aircraft galley or similar monument that is retractable into the galley when not in use. The overall size of the footstep is significantly reduced by the use of a spring loaded detent mechanism. The present invention is designed to allow the footstep to remain in the deployed, horizontal position by means of a spring and plunger that cooperat…
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification B64C1/24. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue May 22 2018 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).