Method for producing blades from Ni-based alloys and blades produced therefrom

Patent metadata

Field	Value
Publication number	US-11969799-B2
Application number	US-202016744337-A
Country	US
Kind code	B2
Filing date	Jan 16, 2020
Priority date	Jan 18, 2019
Publication date	Apr 30, 2024
Grant date	Apr 30, 2024

Abstract

The present invention relates to a method for producing a component of a turbomachine from a metal alloy as well as a correspondingly produced component, wherein the method includes defining at least one first component region that will have a first property profile, and at least one second component region that will have a second property profile which is different from the first property profile; providing at least one powder of the metal alloy or several different powders of constituents of the metal alloy; additive manufacture of the component from the at least one powder, wherein the powder is melted for cohesive joining of the powder particles to each other and to a substrate or to an already produced part of the component.

First claim

What is claimed is:

1. A method for producing a monolithically formed component of a turbomachine from a metal alloy, which comprises the following steps:
defining at least one first component region within a monolithic component, said first component region having a first property profile that improves a first material characteristic of the at least one first component region, and at least one second component region within said monolithic component, said second component region having a second property profile that improves a second material characteristic of the at least one second component region, the second property profile being different from the first property profile and the second material characteristic being different from the first material characteristic;
providing at least one powder of the metal alloy or several different powders of constituents of the metal alloy;
additive manufacturing of the monolithic component from the at least one powder, wherein the powder is melted for cohesive joining of the powder particles to each other and to a substrate or to an already produced part of the monolithic component, and is additively deposited under such different conditions that different structures of the deposited material are produced in the first component region and in the second component region, wherein the at least one first component region and the at least one second component region have different micro structural formations;
wherein the property profile of the first component region has an improved fatigue strength than that in the second component region and the property profile in the second component region has a higher creep resistance than that in the first component region; and
wherein a fine-grained structure with fine carbide precipitations is formed in the first component region, and a coarse-grained structure with coarse carbide precipitations is formed in the second component region.

2. The method according to claim 1 , wherein during the additive manufacture, the monolithic component is built up layer-by-layer onto a substrate or a previously produced part of the monolithic component, wherein a layer-by-layer construction by layerwise deposition welding or layerwise melting of powder material with an energy-rich beam and layerwise solidifying of the molten powder.

3. The method according to claim 2 , wherein the energy-rich beam is a laser beam or an electron beam.

4. The method according to claim 1 , wherein, prior to the melting, a preheating of the powder material is carried out by radiant heating or inductive heating.

5. The method according to claim 1 , wherein the different conditions for melting the powder comprise at least one item from the following group: different heating energy, different beam energy, different melting temperatures, different melting rates, different preheating times, different holding times in the molten state, different cooling conditions, different cooling rates, different temperature gradients, different ambient pressures, and different deposition rates.

6. The method according to claim 1 , wherein the different powder particles and/or the different conditions for melting the powder during the production of the first and/or the second component region are varied over the corresponding first and/or second component region and/or in the transition region between the first and second component region, so that a gradient of material with varying property profile is deposited in the corresponding first and/or second component region and/or in the transition region.

7. The method according to claim 1 , wherein the monolithic component is a rotating blade of a turbomachine, wherein the first component region comprises the blade root and the second component region comprises the region of an inner and/or outer shroud and/or the region of the blade element and/or the transition region between shroud and blade element.

8. The method according to claim 1 , wherein the monolithic component is formed of an Fe-, Co- or Ni-based superalloy.

9. The method according to claim 1 , wherein the monolithic component is made of an Fe-, Co- or Ni-based superalloy and is fabricated in one piece by additive manufacture.

10. The method according to claim 9 , wherein the monolithic component is a blade of a turbomachine wherein the first component region comprises the blade root and the second component region comprises the region of an inner and/or outer shroud and/or the region of the blade element and/or the transition region between shroud and blade element.

Assignees

• MTU Aero Engines AG

Inventors

• Fried Markus

Classifications

• B22F5/04 Primary

  of turbine blades · CPC title

• B22F10/28

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

• B22F10/32

  of the atmosphere, e.g. composition or pressure in a building chamber · CPC title

• B22F10/36

  of energy beam parameters · CPC title

• B22F10/38

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