Aircraft axle insert to mitigate vibration

US9950786B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9950786-B2
Application numberUS-201514977153-A
CountryUS
Kind codeB2
Filing dateDec 21, 2015
Priority dateDec 21, 2015
Publication dateApr 24, 2018
Grant dateApr 24, 2018

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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.

Systems and methods are disclosed for aircraft wheels and brakes systems for use in, for example, an aircraft. In this regard, a damper for an axle may comprise a solid body defined by a cylindrical outside diameter (OD) surface and an elliptical inner surface configured to be inserted into a bore of the axle, the elliptical inner surface defining a void. The damper may comprise a varying thickness between the OD surface and the elliptical inner surface, the varying thickness including a minimum thickness along a major axis of the inner surface and a maximum thickness along a minor axis of the inner surface. The varying thickness may help to decouple a bending mode along the minor axis from the bending mode along the major axis.

First claim

Opening claim text (preview).

What is claimed is: 1. A damper for an axle comprising: a solid body defined by a cylindrical outside diameter (OD) surface and an elliptical inner surface configured to be inserted into a bore of the axle, the elliptical inner surface defining a void concentric with the damper, the elliptical inner surface comprising a major axis and a minor axis, wherein a first length of the major axis is greater than a second length of the minor axis, wherein the damper is configured to rotate…

Assignees

Inventors

Classifications

  • Operations & Transport · mapped topic

  • Cross-Sectional Technologies · mapped topic

  • Operations & Transport · mapped topic

  • Mechanical Engineering · mapped topic

  • B64C25/58Primary

    Operations & Transport · mapped topic

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Frequently asked questions

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What does patent US9950786B2 cover?
Systems and methods are disclosed for aircraft wheels and brakes systems for use in, for example, an aircraft. In this regard, a damper for an axle may comprise a solid body defined by a cylindrical outside diameter (OD) surface and an elliptical inner surface configured to be inserted into a bore of the axle, the elliptical inner surface defining a void. The damper may comprise a varying thick…
Who is the assignee on this patent?
Goodrich Corp
What technology area does this patent fall under?
Primary CPC classification B64C25/58. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 24 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).