Method for producing a plate of a turbomachine

US12447544B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12447544-B2
Application numberUS-201917051997-A
CountryUS
Kind codeB2
Filing dateMay 2, 2019
Priority dateMay 2, 2018
Publication dateOct 21, 2025
Grant dateOct 21, 2025

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.

The present invention relates to a method for manufacturing a plate of a turbomachine having a plurality of receiving grooves, which are formed on the cylindrical peripheral surface of the plate in order to receive blade roots of blades of the turbomachine. The receiving grooves extend in a straight line from one face of the plate to the other face of the plate, such that a straight line delimits the receiving groove from each point on the cross section of the receiving groove on one of the faces to the corresponding point on the cross section on the other face. A circular plate is provided and a plurality of receiving grooves are introduced into the plate simultaneously on opposing regions relative to a central axis of rotation of the plate.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for producing a plate or disk of a turbomachine having an axis of rotation and receiving grooves to respectively receive blade roots of the turbomachine, comprising the steps of: providing a circular disk having a cylindrical peripheral surface, a first face and a second face; introducing the receiving grooves into the peripheral surface of the disk by two-step processing, having a first step and a second step; first step processing of pairs of grooves, each of which to extend in a straight line from the first face of the circular disk to the second face of the disk, so that from each point of a cross-section of a receiving groove on the first face to the corresponding point of a cross-section on the second face and wherein a straight line delimits the grooves; and wherein the grooves have a tolerance allowance of 0.1 to 1 mm after the first step of processing; wherein the first step of processing is performed simultaneously for less than all of the of the grooves at a time; wherein less than all of the grooves is a pair of grooves; second step processing of the grooves previously processed in the first processing step using electrochemical material processing with an electrode having a wedge-shaped region and wherein the wedge shape tapers in the direction of the feed direction, the second step processing further fine processes the grooves to a final contour; the wedge shaped region includes an electrode tip and inclined surfaces at the electrode tip; wherein the first step and the second step of processing are carried out by electrochemical material processing and a plurality of grooves are simultaneously introduced into the disk at regions located opposite a central axis of rotation of the disk. 2. The method according to claim 1 , wherein the at least one pair of receiving grooves are introduced into the disk simultaneously in opposing circle sectors relative to the axis of rotation of the disk. 3. The method according to claim 1 , wherein the at least one pair of receiving grooves are introduced into the disk simultaneously, uniformly distributed along the circular, ring-shaped periphery of the disk. 4. The method according to claim 1 , wherein the at least one pair of receiving grooves are introduced simultaneously into the disk and are distributed along the circular, ring-shaped periphery of the disk such that a warping of the disk due to residual stresses is minimized. 5. The method according to claim 1 , wherein all of the at least one pair of receiving grooves are introduced into the disk simultaneously. 6. The method according to claim 1 , wherein the at least one pair of receiving grooves are introduced into the disk at least partially by electrochemical material processing. 7. The method according to claim 1 , wherein during the second step of the processing, only portions of the receiving grooves of the at least one pair of receiving grooves are processed. 8. The method according to claim 1 , wherein at least the first step of the processing takes place simultaneously for all of the receiving grooves and the first step of the processing takes place by electrochemical material processing. 9. The method of according to claim 1 , wherein, in the second step, each groove is separately processed.

Assignees

Inventors

Classifications

  • by electrochemical methods · CPC title

  • Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

  • Electrodes specially adapted therefor or their manufacture (B23H9/00 takes precedence) · CPC title

  • by removing material · CPC title

  • of axial insertion type · CPC title

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 US12447544B2 cover?
The present invention relates to a method for manufacturing a plate of a turbomachine having a plurality of receiving grooves, which are formed on the cylindrical peripheral surface of the plate in order to receive blade roots of blades of the turbomachine. The receiving grooves extend in a straight line from one face of the plate to the other face of the plate, such that a straight line delimi…
Who is the assignee on this patent?
MTU Aero Engines AG
What technology area does this patent fall under?
Primary CPC classification B23H9/10. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Oct 21 2025 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).