Bearing structure

US2016160910A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016160910-A1
Application numberUS-201514961027-A
CountryUS
Kind codeA1
Filing dateDec 7, 2015
Priority dateDec 9, 2014
Publication dateJun 9, 2016
Grant date

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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.

Bearing structure including a first bearing, surrounded by a housing, having a first inner and outer race and first set of rolling elements between the inner and outer races and a second bearing having a second inner and outer race and second set of rolling elements between the second inner and outer races. A first compliant element is connected to the first outer race. A rigid diaphragm is connected to the first outer race between the compliant element and outer race, and is connected to the housing at its outer end. The first compliant element, outer race and rigid diaphragm at least partly define a pressure chamber. The first outer race is axially slidable relative to the second such that a pressure increase in the chamber changes the axial spacing between the first and second outer races, inducing additional axial load on the bearings which helps balance thrust load sharing.

First claim

Opening claim text (preview).

1 . A bearing structure comprising: a first bearing having a first inner race, a first outer race and a first set of rolling elements housed between the first inner race and the first outer race; a second bearing having a second inner race, a second outer race and a second set of rolling elements housed between the second inner race and the second outer race; a housing surrounding the first bearing; a first compliant element, the first compliant element fixedly connected to the first outer race, a rigid diaphragm having a radially inner end fixedly connected to the first outer race at a position spaced from the connection between the first compliant element and the first outer race, and a radially outer end flexibly connected to the housing, wherein the first compliant element, first outer race and rigid diaphragm at least partly define a pressure chamber; and wherein the first outer race is axially slidable relative to the second outer race such that an increase in pressure in the pressure chamber causes a change in axial spacing between the first and second outer races. 2 . A bearing structure according to claim 1 wherein the rigid diaphragm is flexibly connected to the housing at its radially outer end through a flexible element. 3 . A bearing structure according to claim 2 wherein the flexible element is a flexible diaphragm or bellows. 4 . A bearing structure according to claim 1 wherein the first outer race comprises a radially extending flange and the radially inner end of the rigid diaphragm is fixedly connected to the flange. 5 . A bearing structure according to claim 1 wherein the housing further comprises a first radially extending casing and the first compliant element is fixedly connected between the first radially extending casing and the first outer race. 6 . A bearing structure according to claim 1 wherein the first compliant element is connected to an axial end of the first outer race. 7 . A bearing structure according to claim 1 further comprising a second compliant element fixedly connected to the first outer race. 8 . A bearing structure according to claim 7 wherein the first compliant element is connected at an axial end of the first outer race and the second compliant element is connected at the opposing axial end. 9 . A bearing structure according to claim 8 wherein the rigid diaphragm is interposed between the first and second compliant elements such that the pressure chamber is divided into a first pressure chamber defined at least partly by the first compliant element, rigid diaphragm and first outer race and a second pressure chamber defined at least partly by the second compliant element, rigid diaphragm and first outer race. 10 . A bearing structure according to claim 9 wherein the rigid diaphragm is provided midway between the two compliant elements such that the pressure chambers are substantially the same size. 11 . A bearing structure according to claim 7 wherein the housing further comprises a second radially extending casing and the second compliant element is fixedly connected between the second radially extending casing and the first outer race. 12 . A bearing structure according to claim 1 wherein the first and/or second compliant element is a flexible bellows. 13 . A bearing structure according to claim 1 further comprising a valved pressure inlet or a respective valved pressure inlet to provide fluid communication from a pressure source to the respective pressure chamber. 14 . A bearing structure according to claim 1 further comprising a valved pressure outlet or a respective valved pressure outlet to allow venting of pressure from within the or the respective pressure chamber. 15 . A bearing structure according to claim 1 further comprising at least one load sensor associated with each of the first bearing and the second bearing. 16 . A bearing structure according to claim 15 , further comprising an electronic control module, the at least one load sensor being configured to monitor axial loads on the first bearing and the second bearing to provide feedback to the electronic control module. 17 . A bearing structure according to claim 16 , wherein the electronic control module is configured to trigger pressurisation of at least the pressure chamber if the axial load on the first bearing or the second bearing is found to be below a predetermined minimum. 18 . A bearing structure according to claim 16 , wherein the at least one load sensor and the electronic control module are configured to trigger venting of the pressure chamber. 19 . A bearing structure as claimed in claim 16 , wherein the at least one load sensor and the electronic control module are configured to continually or regularly adjust the pressure within the pressure chamber to maintain the axial loading on the first bearing and the second bearing above a predetermined minimum. 20 . A gas turbine engine comprising a bearing structure according to claim 1 .

Assignees

Inventors

Classifications

  • with a single row or balls · CPC title

  • F16C19/54Primary

    Systems consisting of a plurality of bearings with rolling friction (spindle bearings F16C35/08) · CPC title

  • Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title

  • related to load on the bearing, e.g. bearings with load sensors or means to protect the bearing against overload · CPC title

  • Radial bearings · CPC title

Patent family

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Frequently asked questions

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What does patent US2016160910A1 cover?
Bearing structure including a first bearing, surrounded by a housing, having a first inner and outer race and first set of rolling elements between the inner and outer races and a second bearing having a second inner and outer race and second set of rolling elements between the second inner and outer races. A first compliant element is connected to the first outer race. A rigid diaphragm is con…
Who is the assignee on this patent?
Rolls Royce Plc
What technology area does this patent fall under?
Primary CPC classification F16C19/54. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jun 09 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).