Method for treating turbine blades and device therefor

US9403245B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9403245-B2
Application numberUS-201113822739-A
CountryUS
Kind codeB2
Filing dateSep 14, 2011
Priority dateSep 14, 2010
Publication dateAug 2, 2016
Grant dateAug 2, 2016

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A method is provided for treating turbine blades having holes for discharging cooling air. A protective layer is provided and then the holes that are partly or completely closed by the protective layer are opened again. Coordinates concerning the position of the holes are acquired before the protective layer is applied using a laser triangulation sensor using a light source generating a light beam and a light detector. The data obtained is used after application of the protective layer to control a removal device for removing protective layer partly or wholly covering the holes. Each hole is measured by the light beam being shone into the hole in different positions in relation to the longitudinal mid-axis of the latter. The light beam is shone into the respective hole in a plane at at least three different angles to the longitudinal mid-axis thereof.

First claim

Opening claim text (preview).

The invention claimed is: 1. A device for determining the position of cooling air holes in turbine blades, the device comprising: an optical measuring sensor suitable for an optical triangulation method, wherein the optical measuring sensor is fitted to a holder such that the position thereof can be varied, at least one light source generating a light beam, at least one light detector, an evaluation device which is formed in such a way that, on the basis of the signals generated by the light detector when the light beam is shone into a cooling air hole in different positions with relation to a determined longitudinal mid-axis of the cooling air hole, it obtains coordinates of the position of the cooling air holes, wherein the light source is adjustable on the holder in different angular positions in at least one plane, the different angular positions are based upon the determined longitudinal mid-axis, and the maximum angular positions with respect to the determined longitudinal mid-axis, wherein the coordinates of the position of the cooling air holes represent at least three different angular positions of the light beam with respect to the determined longitudinal mid-axis, and wherein the longitudinal axis of each cooling air hole is determined, wherein the optical measuring sensor is a laser triangulation sensor, wherein the light source and light detector are combined to form a single measuring sensor, which is fitted to the holder such that the position thereof is variable. 2. The device as claimed in claim 1 , wherein the holder is a machine tool, or a coordinate measuring machine or a measuring arm. 3. The device as claimed in claim 1 , wherein the light source is adjustable on the holder in a plurality of planes and in each case in different angular positions. 4. The device as claimed in claim 1 , wherein the evaluation device is provided with a multidimensional image processing program for evaluating the signals generated by the light detector. 5. The device as claimed in claim 1 , further comprising a removal device for removing the protective layer in the area of the cooling air holes, wherein the removal device co-operates with the evaluation device in such a way that the removal device is aligned on the basis of the data about the cooling air holes that is prepared in the evaluation device. 6. The device as claimed in claim 5 , wherein the removal device is a laser removal device which generates a laser beam. 7. The device as claimed in claim 5 , wherein the alignment is made such that the laser beam from the laser removal device shines into the respective cooling air hole coaxially or parallel to the longitudinal mid-axis of the latter.

Assignees

Inventors

Classifications

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9403245B2 cover?
A method is provided for treating turbine blades having holes for discharging cooling air. A protective layer is provided and then the holes that are partly or completely closed by the protective layer are opened again. Coordinates concerning the position of the holes are acquired before the protective layer is applied using a laser triangulation sensor using a light source generating a light b…
Who is the assignee on this patent?
Arjakine Nikolai, Melzer-Jokisch Torsten, Thomaidis Dimitrios, and 1 more
What technology area does this patent fall under?
Primary CPC classification F01D5/005. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 02 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).