Method for manufacturing or for repairing a component of a rotary machine as well as a component manufactured or repaired using such a method

US11318568B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11318568-B2
Application numberUS-202016944505-A
CountryUS
Kind codeB2
Filing dateJul 31, 2020
Priority dateSep 22, 2016
Publication dateMay 3, 2022
Grant dateMay 3, 2022

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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

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A method for manufacturing a component of a rotary machine, the component extends in an axial direction and a radial direction vertical thereto, and has an inner channel, extending from a first end in a center of the component to a second end at a radial limiting surface of the component and which is partially closed. A blank includes the center of the component and is limited by an outer surface in the radial direction. The maximum dimension of the outer surface in the radial direction is smaller than the dimension of the limiting surface in the radial direction, A first subtractive process step is performed such that a part of the channel is manufactured by a machining process, with the part extending from the first end of the channel to the outer surface of the blank. Afterwards the channel is finished by a build-up process on the blank.

First claim

Opening claim text (preview).

What is claimed: 1. A method for manufacturing a component of a rotary machine, the component extending in an axial direction and a radial direction vertical thereto, and having at least one inner channel extending from a first end in a center of the component to a second end at a radial limiting surface of the component and which is at least partially closed, that the method comprising: providing a blank comprising the center of the component, and the blank being limited by an outer surface in the radial direction, the maximum dimension of the outer surface in the radial direction being smaller than a dimension of the limiting surface in the radial direction; performing a first subtractive process step in which a part of the channel is manufactured by a machining process, with the part extending from the first end of the channel to the outer surface of the blank; and afterwards finishing the channel by a build-up process on the blank by application of at least part of a shapeless or a neutrally shaped material, the build-up process on the blank including building the channel axially adjacent and radially outside of the outer surface of the blank. 2. The method according to claim 1 , wherein the at least one inner channel includes a plurality of inner channels, each of the plurality of inner channels extending from a first end in the center of the component to a second end at the radial limiting surface of the component, adjacent channels are respectively separated by a separating wall, and for each channel, one part of the channel is manufactured in the first subtractive process step, with the part extending from the respective first end of the channel into the outer surface of the blank, and each separating wall and each channel is only finished by the build-up process. 3. The method according to claim 1 , wherein the blank has a central bore before the first subtractive process step, the bore being arranged radially inwardly such, that in the finished state of the component each first end of a channel arranged in the center is separated from the central bore by an annular body. 4. The method according to claim 1 , wherein the first subtractive process step is performed in such a manner, that after finishing the outer surface of the blank, the blank comprises a contiguous annular area covering the confluence of the channel into the outer surface. 5. The method according to claim 1 , wherein the build-up process is performed layer by layer. 6. The method according to claim 1 , wherein the build-up process comprises several additive process steps to successively build up the component. 7. The method according to claim 6 , wherein at least one further subtractive process step is performed between the additive process steps. 8. The method according to claim 6 , wherein in each case one further subtractive process step is performed between two additive process steps. 9. The method according to claim 1 , wherein the component is built up part by part after the first subtractive process step. 10. The method according to claim 1 , wherein the build-up process is performed by a laser. 11. The method according to claim 1 , wherein the component is an impeller, a guide wheel or a diffusor of a rotary machine. 12. The method according to claim 1 , wherein the shapeless or neutrally shaped material is a powder, a band or a wire. 13. The method according to claim 9 , wherein during the build up part all of each separating wall is completed first. 14. The method according to claim 11 , wherein the component is part of a pump, a turbine, a compressor, a compactor or an expander.

Assignees

Inventors

Classifications

  • Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

  • B22F5/009Primary

    of turbine components other than turbine blades (of turbine blades B22F5/04) · CPC title

  • B23P15/04Primary

    turbine or like blades from several pieces · CPC title

  • Construction and assembly (F04D29/2211 takes precedence) · CPC title

  • Form or construction · CPC title

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What does patent US11318568B2 cover?
A method for manufacturing a component of a rotary machine, the component extends in an axial direction and a radial direction vertical thereto, and has an inner channel, extending from a first end in a center of the component to a second end at a radial limiting surface of the component and which is partially closed. A blank includes the center of the component and is limited by an outer surfa…
Who is the assignee on this patent?
Sulzer Management Ag
What technology area does this patent fall under?
Primary CPC classification B22F5/009. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue May 03 2022 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).