Porous rotating machine component, combustor and manufacturing method

Patent metadata

Field	Value
Publication number	US-10753609-B2
Application number	US-201515510336-A
Country	US
Kind code	B2
Filing date	Sep 18, 2015
Priority date	Sep 30, 2014
Publication date	Aug 25, 2020
Grant date	Aug 25, 2020

Abstract

A rotating machine component, particularly a gas turbine combustion component, having at least one part built from a porous material with a plurality of pores, wherein at least a subset of the plurality of pores is at least partly filled with a gas with a composition different from air and/or with a powder, wherein the porous material is a laser sintered or laser melted material in which void local regions form the plurality of pores. The component counter-acts vibrations. A rotating machine or gas turbine engine may have such a component.

First claim

The invention claimed is:

1. A rotating machine component, comprising
at least one part built from a porous material comprising a plurality of pores,
wherein at least a subset of the plurality of pores is at least partly filled with a powder,
wherein the powder is selected so that the powder will at least in parts convert to a gaseous state when affected by heat during operation of the rotating machine component, and
wherein neither the powder nor a gas formed when the powder converts to the gaseous state can escape the plurality of pores.

2. The rotating machine component according to claim 1 ,
wherein the porous material comprises a laser sintered or laser melted material in which void local regions form the plurality of pores.

3. The rotating machine component according to claim 1 ,
wherein the porous material comprises metal foam.

4. The rotating machine component according to claim 1 ,
wherein sizes and/or shapes of the plurality of pores and/or a distribution of the plurality of pores over the at least one part are selected to modify Eigen frequencies of the rotating machine component.

5. The rotating machine component according to claim 1 ,
wherein the at least one part comprises at least one cooling channel for guiding cooling fluid through the at least one part to cool the at least one part during operation.

6. The rotating machine component according to claim 1 ,
wherein pores of the plurality of pores comprise argon.

7. The rotating machine component according to claim 1 ,
wherein during operation, at least one of the powder and the gas damp vibrations of the at least one part.

8. The rotating machine component according to claim 1 ,
wherein the rotating machine component comprises a gas turbine combustion component.

9. A combustor, comprising
a part, wherein the part is arranged as a rotating machine component according to claim 1 .

10. The combustor according to claim 9 ,
wherein the combustor comprises a gas turbine engine.

11. The combustor according to claim 9 ,
wherein the part comprises a combustion chamber liner.

12. A manufacturing method of a part of a rotating machine component, comprising:
building-up of the part as a porous structure by solidifying a base material
i) from metal foam which forms a plurality of pores or
ii) via laser sintering or laser melting, wherein the laser sintering or laser melting leaves void local regions to form the plurality of pores; and

providing a powder during building-up of the part such that at least a subset of the plurality of pores is at least partly filled with the powder,
wherein the powder is selected so that the powder will convert to a gaseous state when affected by heat during operation of the rotating machine component, and
wherein neither the powder nor a gas formed when the powder converts to the gaseous state can escape the plurality of pores.

13. The manufacturing method according to claim 12 ,
wherein building-up of the part via laser sintering or laser melting comprises:
generating instructions to a laser positioning control system such that pores of the plurality of pores are generated to comprise random shapes and/or random sizes and/or random distribution.

14. The manufacturing method according to claim 13 ,
wherein the instructions are generated to the laser positioning control system such that the plurality of pores are generated to comprise the random shapes and/or the random sizes and/or the random distribution under evaluation of at least one of the following input parameters as input to the laser positioning control system: a minimum pore size, and a maximum pore size.

15. The manufacturing method according to claim 12 , further comprising:
generating instructions to a powder deposition control system such that a building-up powder is provided from a first source for the laser sintering or the laser melting, and the powder is provided from a second source.

16. The manufacturing method according to claim 12 ,
wherein the rotating machine component comprises a gas turbine combustion component.

Assignees

• Siemens Ag

Inventors

• Graichen Andreas
• Larfeldt Jenny
• Lörstad Daniel
• Munktell Erik

Classifications

• B22F10/38

  to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures · CPC title

• B22F10/28

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

• Y02P10/25

  Process efficiency · CPC title

• B22F5/009

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

• F23R3/002 Primary

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title