Device for selectively connecting a gearmotor to an aircraft wheel to enable the wheel to be driven selectively by the gearmotor

US9291240B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9291240-B2
Application numberUS-201213712125-A
CountryUS
Kind codeB2
Filing dateDec 12, 2012
Priority dateDec 15, 2011
Publication dateMar 22, 2016
Grant dateMar 22, 2016

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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.

A device, which connects a gearmotor to an aircraft wheel, comprising: a casing rotatably carrying a shaft driven by the gearmotor, the shaft having a fluted portion on which a gearwheel is mounted to slide along a longitudinal axis of the shaft without rotating relative to the shaft; a toothed ring for constraining to rotate with the aircraft wheel; and structure for moving the gearwheel axially between a retracted position (disengaged from the toothed ring) and an engaged position (gearwheel meshes with the toothed ring). The structure for moving the gearwheel comprises a hollow screw-and-nut assembly extending around the shaft. One element of the assembly is axially secured to the gearwheel but prevented from rotating by an anti-rotation member. The other element of the assembly is rotatably mounted inside the casing to be driven selectively by an electric motor so that rotating the electric motor causes the gearwheel to move axially.

First claim

Opening claim text (preview).

What is claimed is: 1. A device for connecting a gearmotor to an aircraft wheel, the device comprising: a casing rotatably carrying a shaft that is to be driven by a gearmotor, the shaft having a fluted portion on which a gearwheel is mounted to slide along a longitudinal axis of the shaft without rotating relative to the shaft; a toothed ring for constraining to rotate with an aircraft wheel; and a structure for moving the gearwheel axially between a retracted position in which it is disengaged from the toothed ring and an engaged position in which the gearwheel meshes with the toothed ring; wherein the structure for moving the gearwheel axially comprise a hollow screw-and-nut assembly extending around the shaft, one of the elements of the screw-and-nut assembly being axially secured to the gearwheel but prevented from rotating by an anti-rotation member, and the other element of the screw-and-nut assembly being rotatably mounted inside the casing to be driven selectively by an electric motor so that rotating the electric motor causes the gearwheel to move axially, and wherein the device further includes a brake for selectively blocking rotation of the element of the screw-and-nut assembly that is driven in rotation by the electric motor. 2. The device according to claim 1 , wherein the connection between the screw and the nut of the screw-and-nut assembly is reversible and resilient return means are installed between the shaft and the gearwheel in order to urge the gearwheel towards the retracted position. 3. The device according to claim 1 , wherein the gearwheel and the structure for moving the gearwheel axially extend between two bearings of the shaft that are carried by the casing.

Assignees

Inventors

Classifications

  • Brakes; Rotational locks · CPC title

  • F16H1/02Primary

    without gears having orbital motion · CPC title

  • B64C25/405Primary

    Powered wheels, e.g. for taxing · CPC title

  • Disconnecting means · CPC title

  • with clutching members movable only axially · CPC title

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Frequently asked questions

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What does patent US9291240B2 cover?
A device, which connects a gearmotor to an aircraft wheel, comprising: a casing rotatably carrying a shaft driven by the gearmotor, the shaft having a fluted portion on which a gearwheel is mounted to slide along a longitudinal axis of the shaft without rotating relative to the shaft; a toothed ring for constraining to rotate with the aircraft wheel; and structure for moving the gearwheel axial…
Who is the assignee on this patent?
Messier Bugatti Dowty
What technology area does this patent fall under?
Primary CPC classification F16H1/02. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 22 2016 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).