Low loss bearing drain

US9695714B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9695714-B2
Application numberUS-201414785103-A
CountryUS
Kind codeB2
Filing dateApr 21, 2014
Priority dateApr 22, 2013
Publication dateJul 4, 2017
Grant dateJul 4, 2017

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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 turbine module comprises a turbine shaft, a rotor assembly secured to the shaft, a bearing assembly rotatably supporting the turbine shaft, and a bearing housing containing the bearing assembly. The bearing housing includes a gutter at least partially circumscribing the bearing assembly, and a drain disposed proximate a base of the gutter. The gutter includes a first sloped floor portion circumferentially adjacent to the drain.

First claim

Opening claim text (preview).

The invention claimed is: 1. A turbine module comprising: a turbine shaft rotatable about a center line of the turbine module; a rotor assembly secured to the turbine shaft, the rotor assembly including a plurality of airfoils circumferentially distributed around a rotor disk; a first bearing assembly including a first plurality of bearings rotatably supporting the turbine shaft; a bearing housing containing the first bearing assembly, the bearing housing including a first gutter recessed into an inner surface of the bearing housing, and at least partially circumscribing the first plurality of bearings radially outward therefrom, and a drain disposed proximate a base of the gutter, the first gutter including a first sloped floor portion circumferentially adjacent to the drain; and a bearing compartment retaining the bearing housing, the bearing compartment including a longitudinal exit duct in communication with the drain; wherein the exit duct comprises an open longitudinal pathway between the drain and a lubricant return line disposed at an axial end of the turbine module. 2. The turbine module of claim 1 , wherein the first sloped floor portion is tangential to an upper floor portion at a clockwise or counterclockwise angular location relative to a center of the drain. 3. The turbine module of claim 2 , wherein the first gutter also includes a second sloped floor portion circumferentially adjacent to the drain. 4. The turbine module of claim 3 , wherein the second sloped floor portion is tangential to the upper floor portion at an opposite angular location from the first sloped floor portion with respect to the center of the drain. 5. The turbine module of claim 2 , wherein the upper floor portion is generally circular and circumscribes the first bearing assembly between the clockwise angular location and the counterclockwise angular location. 6. The turbine module of claim 2 , wherein at least one of the clockwise angular location and the counterclockwise angular location is spaced more than 40°, and less than about 50°, from the center of the drain. 7. The turbine module of claim 1 , further comprising: a plurality of bearing assemblies, including the first bearing assembly contained in the bearing housing, each of the plurality of bearing assemblies including a plurality of bearings, including the first plurality of bearings rotatably supporting the turbine shaft; and a plurality of gutters, including the first gutter, recessed into the bearing housing inner surface, each of the plurality of gutters at least partially circumscribing corresponding ones of the plurality of bearing assemblies and each gutter including a first sloped floor portion circumferentially adjacent to a drain disposed proximate a base of each gutter. 8. The turbine module of claim 1 , wherein an outer diameter of the bearing housing proximate the first bearing assembly measures at least about 1.0 m (39 inches). 9. The turbine module of claim 8 , wherein a lubricant flow rate capacity of the first bearing assembly is at least about 3.8 liters/second (about 1.0 gal/second). 10. A turbomachine bearing system comprising: a bearing housing including at least one portion adapted to be in communication with a lubricant supply passage; a drain disposed at a base of the bearing housing; a first gutter in communication with the drain, recessed into an inner surface of the bearing housing, and at least partially circumscribing the at least one portion of the bearing housing, the gutter including a floor with at least one sloped portion in communication with, and circumferentially adjacent to the drain; and a bearing compartment retaining the bearing housing, the bearing compartment including a longitudinal exit duct in communication with the drain; wherein the exit duct comprises an open longitudinal pathway between the drain and a lubricant return line disposed below the bearing housing. 11. The turbomachine bearing system of claim 10 , wherein the first gutter includes a first sloped floor portion extending between the drain and a first angular location of the gutter relative to a center of the drain. 12. The turbomachine bearing system of claim 11 , wherein the first gutter also includes a second sloped floor portion extending between the drain and a second angular location of the gutter relative to the center of the drain. 13. The turbomachine bearing system of claim 12 , wherein the first sloped floor portion and the second sloped floor portion are each tangential to an upper floor portion of the first gutter. 14. The turbomachine bearing system of claim 13 , wherein the upper floor portion is generally circular and circumscribes the at least one portion of the bearing housing between the first angular location and the second angular location. 15. The turbomachine bearing system of claim 12 , wherein at least one of the first angular location and the second angular location is spaced more than 40°, and less than about 50°, from the center of the drain. 16. The turbomachine bearing system of claim 10 , further comprising: a plurality of bearing assemblies contained in the bearing housing; and a plurality of gutters at least partially circumscribing corresponding ones of the plurality of bearing assemblies, and each gutter including a first sloped floor portion circumferentially adjacent to a corresponding plurality of drains disposed proximate a base of each gutter.

Assignees

Inventors

Classifications

  • Bearing supports · CPC title

  • Details of collecting or draining, e.g. returning the liquid to a sump · CPC title

  • F01D25/32Primary

    Collecting of condensation water; Drainage {; Removing solid particles} · CPC title

  • Drainage · CPC title

  • Radial bearings · CPC title

Patent family

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Frequently asked questions

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What does patent US9695714B2 cover?
A turbine module comprises a turbine shaft, a rotor assembly secured to the shaft, a bearing assembly rotatably supporting the turbine shaft, and a bearing housing containing the bearing assembly. The bearing housing includes a gutter at least partially circumscribing the bearing assembly, and a drain disposed proximate a base of the gutter. The gutter includes a first sloped floor portion circ…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D25/32. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jul 04 2017 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).