Bearing arrangement

US11441603B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11441603-B2
Application numberUS-202016793556-A
CountryUS
Kind codeB2
Filing dateFeb 18, 2020
Priority dateFeb 21, 2019
Publication dateSep 13, 2022
Grant dateSep 13, 2022

How to read this patent

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  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.

A bearing arrangement having: a first element having an inner race and a first bearing surface; a second element, pivotable relative to the first element about a first axis, and having an outer race and a second bearing surface that cooperates with the first bearing surface to form a plain bearing. The bearing arrangement also includes a roller element disposed between the inner and outer races to form a rolling bearing. The inner and outer races are arcuate and subtend an angle of less than 360° about the first axis.

First claim

Opening claim text (preview).

The invention claimed is: 1. An aircraft landing gear comprising: a bogie beam; a shock strut coupled to the bogie beam by a bogie pivot pin, and a bearing assembly coupled to the bogie beam and the shock strut, the bearing assembly comprising: a first element having: an inner race, and a first bearing surface, a second element, pivotable relative to the first element about a first axis, the second element comprising: an outer race, and a second bearing surface, which is configured to cooperate with the first bearing surface to form a plain bearing, and a roller element disposed between the inner race and the outer race to form a rolling bearing, wherein the inner race and the outer race are arcuate and subtend an angle of less than 360° about the first axis. 2. The bearing arrangement of claim 1 , wherein the inner and outer races subtend an angle of not more than 180° about the axis. 3. The bearing arrangement of claim 1 , wherein the first element is a journal. 4. The bearing arrangement of claim 1 , wherein the second element is a lug. 5. The bearing arrangement of claim 1 , wherein the first bearing surface and the second bearing surface are arcuate. 6. The bearing arrangement of claim 1 , wherein the first bearing surface and the inner race form a continuous surface. 7. The bearing arrangement of claim 1 , wherein the rolling bearing and the plain bearing are offset in a direction along the first axis. 8. The bearing assembly of claim 1 , further comprising a tape coupled to the inner race or to the outer race, and at least partially encircling the roller element. 9. The bearing arrangement of claim 1 , wherein the roller element comprises a toothed gear, arranged to engage a corresponding toothed surface of the inner race and/or the outer race. 10. The bearing arrangement of claim 1 , wherein the roller element is a first roller element and the bearing arrangement further comprises a second roller element coupled to the first roller element by a cage such that the roller elements maintain a fixed spacing. 11. The bearing arrangement of claim 10 , wherein the cage extends from a first cage end to a second cage end, and the inner race and the outer race each subtends an angle at the first axis which is greater than an angle subtended by the first cage end and the second cage end. 12. The bearing arrangement of claim 1 , wherein the inner race and the outer race extend along the first axis further than the first bearing surface and the second bearing surface extend along the first axis. 13. The aircraft landing gear of claim 1 , wherein: the first element is the bogie pivot pin; the second element is a lug of the shock strut; and the inner race is disposed on an upper side of the bogie pivot pin when the landing gear is deployed. 14. The aircraft landing gear of claim 1 , wherein: the first element is the bogie pivot pin; the second element is a lug of the bogie beam; and the inner race is disposed on a lower side of the bogie pivot pin when the landing gear is deployed.

Assignees

Inventors

Classifications

  • F16C21/00Primary

    Combinations of sliding-contact bearings with ball or roller bearings, for exclusively rotary movement (F16C17/24, F16C19/52 take precedence) · CPC title

  • Raceways; Race rings · CPC title

  • Means to synchronise movements · CPC title

  • Aeroplanes; Helicopters · CPC title

  • wheeled type, e.g. multi-wheeled bogies · CPC title

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Frequently asked questions

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What does patent US11441603B2 cover?
A bearing arrangement having: a first element having an inner race and a first bearing surface; a second element, pivotable relative to the first element about a first axis, and having an outer race and a second bearing surface that cooperates with the first bearing surface to form a plain bearing. The bearing arrangement also includes a roller element disposed between the inner and outer races…
Who is the assignee on this patent?
Safran Landing Systems Uk Ltd
What technology area does this patent fall under?
Primary CPC classification F16C21/00. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 13 2022 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).