Method for removing and/or installing a turbine bearing and a device for carrying out the method

US9512723B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9512723-B2
Application numberUS-201214368744-A
CountryUS
Kind codeB2
Filing dateNov 29, 2012
Priority dateDec 30, 2011
Publication dateDec 6, 2016
Grant dateDec 6, 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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  7. Citations and related patents

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Abstract

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A method and a device are provided for removing a turbine bearing or a bearing segment of a preferably stationary turbo engine, having a housing that may preferably be split in half while the housing is closed. The method includes: supporting the rotor to relieve the turbine bearing of the weight of the rotor, fastening a support plate to a turbine bearing housing, attaching two parallel, rail-like supports to the support plate and fastening a cross-beam to ends of supports, fastening a counter-bearing plate having at least two push/pull rods to the turbine bearing housing, and fastening the push/pull rods to the turbine bearing and detaching the fastening of the turbine bearing from the turbine bearing housing and pulling the turbine bearing located in the operating position thereof out of the turbine bearing housing with the aid of the push/pull rods.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for removing or installing a turbine bearing, or one of its constituent parts, of a static turbomachine when a housing of the static turbomachine is closed, the method comprising: a) supporting a rotor and/or holding the rotor in order to free the turbine bearing from the weight of the rotor, b) fastening a support plate to an end face of a turbine bearing housing, attaching to the support plate two mutually parallel rail-like beams so that the beams extend into and out of the turbine bearing housing, and fastening a cross beam to those ends of the beams which are opposite the support plate, c) positioning the turbine bearing on the beams so that the beams act as a cantilevered support under the turbine bearing, and d) moving the turbine bearing on the beams from a first position to a second position. 2. The method as claimed in claim 1 , wherein the method is for installing the turbine bearing, wherein step c) comprises placing the turbine bearing to be installed on the beams and moving the turbine bearing into the first position that is an intermediate position, and wherein step d) comprises moving the turbine bearing, or one of its constituent parts, from the intermediate position into the second position that is its installation position. 3. The method as claimed in claim 2 , wherein, before step c), for each beam a sliding element is fastened to the turbine bearing. 4. The method as claimed in claim 2 , wherein, before or after step b), an abutment plate having at least two movable push/pull rods is fastened to the turbine bearing housing and the push/pull rods are fastened to the turbine bearing and the movement is performed by the push/pull rods. 5. The method as claimed in claim 1 , wherein the method is for removing the turbine bearing, wherein step c) comprises releasing a fastening of the turbine bearing from the turbine bearing housing and wherein step d) comprises extracting the turbine bearing, or one of its constituent parts, from the turbine bearing housing. 6. The method as claimed in claim 5 , wherein, before step d), for each beam a sliding element is fastened to the turbine bearing. 7. The method as claimed in claim 5 , wherein, before or after step b), an abutment plate having at least two push/pull rods is fastened to the turbine bearing housing and the push/pull rods are fastened to the turbine bearing and the extraction is performed with the aid of the push/pull rods. 8. The method as claimed in claim 1 , further comprising braking movement of the turbine bearing along the beams via a locking element that is secured to a pivotable securing bracket that is arranged on at least one of the beams. 9. The method as claimed in claim 1 , wherein the beams are in each case configured as a roller track and the rolling planes thereof are inclined with respect to one another. 10. A device for installing or removing a turbine bearing, or one of its constituent parts, of a static turbomachine when a housing of the static turbomachine is closed, comprising: a support plate for fastening to a turbine bearing housing of the turbine bearing, at least two mutually parallel rail-like beams which are fastened perpendicularly to the support plate, a cross beam which is fastened to beam ends, a pivotable securing bracket arranged on at least one beam, and a locking element which brakes the movement, along the beams, of the turbine bearing to be removed/installed, being articulated on this bracket via at least one joint. 11. The device as claimed in claim 10 , further comprising: an abutment plate provided for fastening to the turbine bearing housing and having at least two push/pull rods which can be moved thereon and which are provided for fastening to the component to be removed or installed. 12. The device as claimed in claim 10 , wherein the beams are in each case configured as a roller track and rolling planes thereof are inclined with respect to one another. 13. A method, comprising: a) supporting a rotor and/or holding the rotor using the device of claim 10 in order to free a turbine bearing from the weight of the rotor, b) fastening the support plate of the device to the turbine bearing housing, attaching to the support plate of the device the at least two mutually parallel rail-like beams of the device and fastening the cross beam of the device to those ends of the beams which are opposite the support plate, c) positioning the turbine bearing on the beams and d) moving the turbine bearing on the beams from a first position to a second position. 14. A device for installing or removing a turbine bearing, or one of its constituent parts, of a static turbomachine when a housing of the static turbomachine is closed, comprising: a support plate configured to be secured to an end side of an annular bearing housing, at least two mutually parallel rail-like beams which are fastened perpendicularly to the support plate and which are configured to extend into and out of the annular bearing housing, wherein an end of the beams extending out of the annular bearing housing is configured to act as a cantilevered support under the turbine bearing, and a cross beam which is fastened to beam ends. 15. The device of claim 14 , wherein the beams are in each case configured as a roller track and rolling planes thereof are inclined with respect to one another.

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What does patent US9512723B2 cover?
A method and a device are provided for removing a turbine bearing or a bearing segment of a preferably stationary turbo engine, having a housing that may preferably be split in half while the housing is closed. The method includes: supporting the rotor to relieve the turbine bearing of the weight of the rotor, fastening a support plate to a turbine bearing housing, attaching two parallel, rail-…
Who is the assignee on this patent?
Siemens Ag
What technology area does this patent fall under?
Primary CPC classification B25B27/06. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 06 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).