Method and apparatus for shortening the rotor blades of a turbomachine

US9616543B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9616543-B2
Application numberUS-201414518296-A
CountryUS
Kind codeB2
Filing dateOct 20, 2014
Priority dateOct 24, 2013
Publication dateApr 11, 2017
Grant dateApr 11, 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 for shortening one or more rotor blade(s) ( 2 ) of a turbomachine ( 3 ) by removal of material at the blade tip, and apparatus ( 1; 19 ) for carrying out the method: a belt grinding apparatus ( 1; 19 ) shortens the rotor blades ( 2 ) and a contour of the blade tip is generated by a relative movement of the blade tip along the static belt grinding apparatus.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for shortening at least one rotor blade of a turbomachine by removal of material at a tip of the blade, the method comprising: providing a belt grinding apparatus including a tip grinding belt, and the apparatus and the belt thereof being configured for grinding the blade tips for shortening the rotor blade; providing the rotor blades installed in a casing of the turbomachine during the shortening; removing part of the casing to at least partially expose the rotor blades to be machined and to expose a parting joint of the casing; attaching the belt grinding apparatus to the casing at the parting joint, in the region of the rotor blades to be machined; orienting the belt grinding apparatus relative to the rotor blades to be shortened in a manner selected to enable the removal by the belt of the material at the blade tips; rotating the at least one rotor blade past the belt; and shortening the rotor blades by operating the belt grinding apparatus and the belt for grinding the blade tips while the rotor on which the at least one blade is supported is continuously rotating. 2. The method as claimed in claim 1 , wherein at least one of the rotor blades has cooling air bores, and the method further comprises sealing or covering the cooling air bores before the grinding. 3. The method as claimed in claim 1 , further comprising continuously rotating the rotor using an auxiliary rotor rotating device for rotating the rotor during the shortening so that the blade tips rotate past the belt for grinding by the belt. 4. The method as claimed in claim 1 , further comprising extracting grinding dust produced during the grinding.

Assignees

Inventors

Classifications

  • B24B21/165Primary

    for vanes or blades of turbines, propellers, impellers, compressors and the like · CPC title

  • by sucking · CPC title

  • Hollow blades, {i.e. blades with cooling or heating channels or cavities (structure of hollow blades in general F01D5/147)}; Heating, heat-insulating or cooling means on blades · CPC title

  • specially designed for portable grinding machines, e.g. hand-guided · CPC title

  • with belt-like tools · CPC title

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Frequently asked questions

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What does patent US9616543B2 cover?
A method for shortening one or more rotor blade(s) ( 2 ) of a turbomachine ( 3 ) by removal of material at the blade tip, and apparatus ( 1; 19 ) for carrying out the method: a belt grinding apparatus ( 1; 19 ) shortens the rotor blades ( 2 ) and a contour of the blade tip is generated by a relative movement of the blade tip along the static belt grinding apparatus.
Who is the assignee on this patent?
Siemens Ag
What technology area does this patent fall under?
Primary CPC classification B24B21/165. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 11 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).