Material and processes for additively manufacturing one or more parts

Abstract

Material is provided for forming a part using a manufacturing system. The material includes a plurality of discrete particles. Each of the particles includes a metal powder core encapsulated by a non-metal coating. At least the cores of the particles are adapted to be solidified together by the manufacturing system to form the part.

Claims

1. A process for forming a part using an additive manufacturing system, the process comprising: providing a plurality of discrete particles, each of the particles including a metal powder core encapsulated by a non-metal coating, wherein the non-metal coating comprises at least one of the following materials: alkoxysilane, aminosilane, organic phospholic acid, triazol, or alkylphosphonic acid; and solidifying at least some of the cores together using the additive manufacturing system to form at least a portion of the part.

2. A process for forming a part using an additive manufacturing system, the process comprising: providing a plurality of discrete particles, each of the particles including a metal powder core encapsulated by a non-metal coating, wherein the non-metal coating of one of the particles comprises at least one of the following materials: alkoxysilane, aminosilane, organic phospholic acid, triazol, or alkylphosphonic acid; and solidifying at least some of the cores together using the additive manufacturing system to form at least a portion of the part.

3. The process of claim 2, wherein the metal powder core of one of the particles comprises a degassed metal powder core.

4. The process of claim 2, wherein the coating of one of the particles is adapted to prevent the core from adsorbing moisture.

5. The process of claim 2, further comprising removing the coatings from at least some of the particles to expose the cores of the respective particles.

6. The process of claim 2, wherein the core of one of the particles includes one or more metal particles.

7. The process of claim 2, wherein the core of one of the particles comprises at least one of the following materials: aluminum, copper, titanium, nickel or steel.

8. The process of claim 2, wherein the additive manufacturing system comprises a cold spray device.

9. The process of claim 2, wherein the additive manufacturing system comprises one of a laser or an electron beam energy source.

10. The process of claim 2, wherein the non-metal coating of one of the particles comprises at least one of the following materials: the alkoxysilane, or the aminosilane.

11. The process of claim 2, wherein the non-metal coating of one of the particles comprises the triazol.

12. The process of claim 2, wherein the non-metal coating of one of the particles comprises the organic phospholic acid.

13. The process of claim 2, wherein the non-metal coating of one of the particles comprises the alkylphosphonic acid.

14. A process for forming a part using an additive manufacturing system that includes a material applicator, the process comprising: providing a plurality of discrete particles, each of the particles including a metal powder core encapsulated by a non-metal coating, wherein the non-metal coating comprises at least one of the following materials: alkoxysilane, aminosilane, organic phospholic acid, triazol, or alkylphosphonic acid; providing a plurality of exposed cores by removing the non-metal coating from each of the particles such that the respective core is exposed; providing the exposed cores to the material applicator; and forming at least a portion of the part using at least the material applicator, the forming comprising solidifying at least some of the exposed cores together.

15. The process of claim 14, wherein the core of one of the particles includes one or more metal particles.

16. The process of claim 14, wherein the core of one of the particles comprises at least one of the following materials: aluminum, copper, titanium, nickel or steel.

17. The process of claim 14, wherein the additive manufacturing system comprises a cold spray device.

18. The process of claim 14, wherein the additive manufacturing system comprises one of a laser or an electron beam energy source.

19. The process of claim 14, wherein the coating of one of the particles is adapted to volatize to expose the core.

20. The process of claim 14, wherein the non-metal coating comprises a polymer-ceramic coating.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is cross-sectional illustration of an additive manufacturing particle;

(2) FIG. 2 is a block diagram of a system for additively manufacturing one or more parts; and

(3) FIG. 3 is a flow diagram of a process for forming one or more parts using the additive manufacturing system of FIG. 2 and material including the additive manufacturing particle of FIG. 1.

DETAILED DESCRIPTION OF THE INVENTION

(4) Material is described below for additively manufacturing one or more parts. This additive manufacturing material includes a plurality of discrete particles that collectively form powder. An exemplary of one of these additive manufacturing particles 10 is illustrated in FIG. 1 and described below. It is worth noting, however, that one or more of the additive manufacturing particles included in the additive manufacturing material may alternatively have different configurations and/or compositions than that described below and illustrated in FIG. 1.

(5) The additive manufacturing particle 10 of FIG. 1 includes a metal powder core 12 covered and/or encapsulated by a coating 14. The core 12 may include one or more metal particles. Each of these metal particles may be composed from one or more of the following core materials: aluminum (Al), copper (Cu), titanium (Ti), nickel (Ni), steel, and/or alloys thereof. One or more of the metal particles, of course, may also or alternatively be composed from one or more core materials other than those described above.

(6) The core 12 may be a degassed metal powder core. For example, before being encapsulated within the coating 14, the core 12 may be degassed to remove entrained gas, adsorbates and/or moisture therefrom. Various degassing processes are known in the art and therefore are not described in further detail.

(7) The core 12 may have a size (e.g., an average diameter) of between about five micrometers (5 μm) and about five-hundred micrometers (500 μm); e.g., between about twenty micrometers (20 μm) and about sixty micrometers (60 μm). The present invention, however, is not limited to the foregoing exemplary core sizes.

(8) The coating 14 is adapted to substantially reduce or prevent the core 12 from adsorbing moisture. The coating 14 therefore may enable the additive manufacturing particle 10 to be stored outside of a controlled additive manufacturing environment (e.g., a vacuum or noble gas environment) without compromising the core material for subsequent additive manufacturing. In contrast, a metal particle without such a coating may adsorb moisture during the storage and/or transportation thereof. This moisture may subsequently cause surface defects and/or porosity defects in a part formed from the now non-degassed metal particle.

(9) Referring again to FIG. 1, the coating 14 may also be adapted to partially or substantially completely decompose and/or volatize in order to partially or substantially completely expose the core 12 for subsequent additive manufacturing. In this manner, the coating 14 may be removed from the core 12 prior to formation of the part(s), which reduces the likelihood of or substantially prevents the coating material from altering the mechanical properties and/or the intended chemical composition of the part(s).

(10) The coating 14 may be a non-metal coating such as, for example, a polymer coating, a ceramic coating, a polymer-ceramic coating, or any other type of coating that does not include a metal component and is adapted as described above. The coating 14, for example, may be composed from one or more of the coating materials listed below in Table I. The coating 14, however, may also or alternatively be composed of one or more coating materials other than those described above and listed in Table I.

(11) TABLE-US-00001 TABLE I Core Repre- sentative Coating Metal Core Representative Non-Metal Material Chemical Class(es) Coating Material(s) Aluminum Alkoxysilane Triethoxy silane Aminosilane Aminopropyldimethylethoxysilane Organic phospholic Pentanephosphonic acid acid Nitride Nitrogen (e.g., N.sub.2) Fluoride Fluorocarbon Epoxy Organic vapor coating Paralene, cyanoacrylate Copper Thiol, disulphide, Organic thiol thiolate Triazol Benzenetriazole (BTA) Organic vapor coating Paralene, cyanoacrylate Inorganic vapor Silane coating Titanium Inorganic vapor Titanium nitride coating Chemisorption Fluorinated polymers Nickel Chemisorption Alkylphosphonic acids Steel Electropolymerization Polypyrrol/polyaniline

(12) The coating material may be deposited on the core 12 to form the coating 14 through one or more of the following processes: chemical adsorption, physical adsorption and/or covalent bonding. Various chemical adsorption, physical adsorption and covalent bonding processes are known in the art and therefore are not described in further detail. The coating material, of course, may also or alternatively be deposited on the core 12 using one or more processes other than those described above.

(13) FIG. 2 illustrates a system 16 for additively manufacturing a part 18 (or parts) from the additive manufacturing material (e.g., powder) describe above. This additive manufacturing system 16 includes a support 20, an additive manufacturing device 22 and a controller 24. The additive manufacturing system 16 also includes a housing 26, such as a sealed enclosure or pressure vessel, in which the support 20 and at least a portion of the additive manufacturing device 22 are located.

(14) The support 20 includes a support surface 28. This support surface 28 is configured to support the additive manufacturing material and/or at least a portion of the part 18 (or parts) during the formation of the part 18 (or parts). The support surface 28, for example, may be substantially horizontal relative to gravity. The support surface 28 may also have a generally planar geometry.

(15) The additive manufacturing device 22 may be configured as a cold spray device, a laser sintering device, or an electron beam melting device. Various cold spray devices, laser sintering devices and electron beam melting devices are known in the art and therefore are not described in further detail. In addition, various other types and configurations of additive manufacturing devices are known in the art and the present invention is not limited to any particular ones thereof.

(16) The controller 24 is in signal communication (e.g., hardwired and/or wirelessly coupled) with the additive manufacturing device 22. The controller 24 is adapted to signal the additive manufacturing device 22 to perform at least a portion of the process described below. The controller 24 is implemented with a combination of hardware and software. The hardware includes memory and a processing device (or system), which includes one or more single-core and/or multi-core processors. The memory may be a non-transitory computer readable medium, and configured to store software (e.g., program instructions) for execution by the processing device. The hardware may also or alternatively include analog and/or digital circuitry other than that described above.

(17) FIG. 3 is a flow diagram of a process for forming a part 18 (or parts) using the additive manufacturing material and the additive manufacturing system 16. An example of a part that may be formed with the additive manufacturing system 16 is a rotor blade for a turbine engine; e.g., a turbine blade, a compressor blade or a fan blade. Other examples of a part that may be formed with the additive manufacturing system 16 include a stator blade for a turbine engine, a guide vane for a turbine engine, a gas path wall for a turbine engine as well as various other components included in a turbine engine. The process of FIG. 3 and the additive manufacturing system 16, of course, may also or alternatively form parts other than those included in a turbine engine.

(18) Prior to the formation of the part 18 (or parts), the additive manufacturing material may be stored in an ambient environment outside of the additively manufacturing system 16. Alternatively, the additive manufacturing material may be stored in a controlled environment (e.g., a vacuum or noble gas environment) and/or in a reservoir 30 (e.g., a hopper) of the additive manufacturing system 16.

(19) In step 300, the additive manufacturing material is loaded into the additive manufacturing system 16. The additive manufacturing material, for example, may be poured out or otherwise directed from its storage container into the reservoir 30, which may selectively feed the material to the additive manufacturing device 22.

(20) In step 302, the coating 14 is removed from at least some of the additive manufacturing particles (e.g., particle 10) to expose the core material; e.g., the degassed metal powder cores. For example, a conduit and/or a chamber 32 configured with the additive manufacturing device 22 may be heated with a heater to or above an elevated (e.g., above ambient) temperature at which the coating material decomposes and/or volatizes. This conduit and/or chamber 32 may be connected upstream of a material applicator 34 (e.g., a powder bed nozzle or a cold spray nozzle) of the additive manufacturing device 22. The material applicator 34 therefore may receive the exposed core material (e.g., the degassed metal powder cores) from the conduit and/or chamber 32.

(21) In step 304, at least some of the exposed core material is formed into at least a portion of the part 18 (or parts). The material applicator 34, for example, may cold spray the exposed core material onto the support surface 28 to build up a base layer. The material applicator 34 may subsequently cold spray one or more additional layers of the exposed core material onto the base layer to accumulatively form the part 18 (or parts). As each layer of material is cold sprayed, it may fuse to a previously sprayed layer thereby solidifying at least some of the metal powder cores 12 together to form the part 18 (or parts).

(22) In another example, the material applicator 34 may deposit a uniform and compacted layer of the exposed core material onto the support surface 28. A laser or electron beam energy source 36 may subsequently solidify (e.g., sinter or otherwise melt) some or all of the metal powder cores 12 in the layer together to form a base layer of the part 18 (or parts). The material applicator 34 may subsequently deposit one or more additional uniform and compacted layers of the exposed core material onto the base layer, and the laser or electron beam energy source 36 may respectively solidify some or all of the metal powder cores 12 in the additional layer(s) to form additional layers of the part 18 (or parts). Of course, the process of FIG. 3 is not limited to the foregoing exemplary material buildup techniques or devices.

(23) One or more of the process steps of FIG. 3 may be omitted, re-arranged and/or combined. For example, in some embodiments, the additive manufacturing material may be stored with the additive manufacturing system 16. In some embodiments, the coating 14 may be removed within the material applicator 34 and/or as the additive manufacturing particles (e.g., particle 10) are directed from the material applicator 34 towards the support surface 28. In some embodiments, the coating material may not be removed from the particles (e.g., particle 10) where, for example, the coating material does not substantially affect the chemical composition and/or mechanical properties of the part 18 (or parts) formed therefrom.

(24) The process of FIG. 3 may include one or more additional steps other than those described above. For example, in some embodiments, the part 18 (or parts) may undergo additional manufacturing processes during and/or after the material buildup step 304. Examples of such additional manufacturing processes may include, but are not limited to, machining, surface finishing, coating, etc. In some embodiments, the part 18 (or parts) may also or alternatively undergo additional manufacturing processes before the material buildup step 304 where, for example, the additive manufacturing material is built up upon an existing part or portion of a part (or parts); e.g., to repair a part, etc.

(25) While the material disclosed herein is described above with reference to additive manufacturing, this material may also or alternatively be used for other manufacturing processes. The material, for example, may be solidified together by a manufacturing system during casting, hot pressing, extruding, etc. The present invention therefore is not limited to any particular manufacturing processes or systems.

(26) While various embodiments of the present invention have been disclosed, it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible within the scope of the invention. For example, the present invention as described herein includes several aspects and embodiments that include particular features. Although these features may be described individually, it is within the scope of the present invention that some or all of these features may be combined within any one of the aspects and remain within the scope of the invention. Accordingly, the present invention is not to be restricted except in light of the attached claims and their equivalents.