Method for pulling a bearing body off the rotor of a gas turbine and tubular shaft extension

US9638106B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9638106-B2
Application numberUS-201213983126-A
CountryUS
Kind codeB2
Filing dateJan 5, 2012
Priority dateFeb 9, 2011
Publication dateMay 2, 2017
Grant dateMay 2, 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 method is provided for pulling a bearing body off the rotor of a gas turbine having a casing, while the casing is closed. The method includes fixing a shaft extension on the relevant end of the rotor. In order to free the bearing body of the weight of the rotor, the method involves supporting the rotor and/or holding the rotor. The method further includes fitting sliding elements between the bearing body and the rotor, and moving the bearing body axially along the machine axis onto the shaft extension.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for pulling a bearing body off a rotor of a gas turbine engine, the gas turbine engine having a casing, while the casing is closed, the method comprising: fixing a removable shaft extension on an end of the rotor, and at least one of: supporting the rotor on a turbine exhaust casing, and holding the rotor from above, in order to free the bearing body of the weight of the rotor; fitting sliding elements between the bearing body and the rotor along an axis that is substantially perpendicular to a machine axis such that the bearing body can be moved relative to the machine axis; and moving the bearing body axially along the machine axis off of the rotor onto the shaft extension. 2. The method as claimed in claim 1 , wherein the bearing body is of undivided configuration in the circumferential direction. 3. The method as claimed in claim 1 , further comprising: securing the bearing body against rotation during and after axial movement with the aid of an anti-rotation device. 4. The method as claimed in claim 3 , further comprising: providing at least one guide extending in an axial direction as an anti-rotation device on the shaft extension, the guide limiting the tangential movement of a pin fixed on the bearing body when there is a risk of rotary motion of the bearing body. 5. The method as claimed in claim 4 , wherein the guide is embodied as a U-profile, along an outward-facing web of which the pin can slide with a small clearance. 6. The method as claimed in claim 4 , wherein the guide is embodied as a flat profile, a flat side of which extends perpendicularly to the radius of the shaft extension and parallel to the machine axis. 7. The method as claimed in claim 1 , wherein the shaft extension is screwed onto the end of the rotor. 8. The method as claimed in claim 7 , further comprising: aligning the shaft extension relative to the rotor with the aid of a roller bracket to enable the shaft extension to be screwed onto the rotor without misalignment. 9. The method as claimed in claim 7 , further comprising: positioning and securing the shaft extension which is screwed onto the rotor against rotation with the aid of a locknut. 10. The method as claimed in claim 1 , further comprising: supporting the bearing body on the rotor or the extension of the rotor at two axial positions via the sliding elements. 11. The method as claimed in claim 1 , wherein the gas turbine is a stationary gas turbine. 12. The method as claimed in claim 1 , wherein the casing is configured such that the casing can be divided into halves.

Assignees

Inventors

Classifications

  • B25B27/06Primary

    inserting or withdrawing sleeves or bearing races · CPC title

  • Repairing or disassembling · CPC title

  • Disassembly methods · CPC title

  • F02C7/36Primary

    Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

  • Rigid support of bearing units; Housings, e.g. caps, covers (F16C23/00 takes precedence) · CPC title

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What does patent US9638106B2 cover?
A method is provided for pulling a bearing body off the rotor of a gas turbine having a casing, while the casing is closed. The method includes fixing a shaft extension on the relevant end of the rotor. In order to free the bearing body of the weight of the rotor, the method involves supporting the rotor and/or holding the rotor. The method further includes fitting sliding elements between the …
Who is the assignee on this patent?
MüLLER DIRK, 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 May 02 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).