180 materials
3D Systems LaserForm CoCrF75 (A) is a cobalt-chromium-molybdenum alloy grade printed by laser powder bed fusion, here in the annealed condition. Laser melting leaves this alloy with a very fine cellular structure, high residual stress, some anisotropy between build directions and a rough surface, and parts need supports that are cut or machined off. Annealing relieves the residual stress and homogenizes the as-built structure, giving up some strength for greater ductility. Printed parts are used for dental frameworks, medical device components and wear- and corrosion-resistant industrial parts of complex shape. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm CoCrF75 (A) is a cobalt-chromium-molybdenum alloy grade made by laser powder bed fusion, here in the hot isostatically pressed condition. As built, the alloy has a fine cellular solidification structure, residual stress from layerwise melting, some anisotropy between build directions and a rough, support-marked surface. Hot isostatic pressing closes internal porosity, relieves residual stress and homogenizes the microstructure, giving more consistent ductility and fatigue behaviour. Surface roughness and surface-connected pores remain, so parts still need machining or polishing. Parts in this condition are used for orthopaedic and dental components, wear surfaces and high-temperature industrial parts. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive CoCrMo in the as-built condition is the maker's cobalt-chromium-molybdenum grade printed by laser powder bed fusion, with no heat treatment after the build. Rapid solidification gives a fine cellular structure with columnar grains along the build direction, so strength is high, ductility is limited and properties differ between build directions. Parts carry residual stress, need supports and have rough surfaces, so stress relief, support removal and finishing usually follow. The grade is used for dental frameworks, orthopaedic components and wear- and corrosion-resistant industrial parts. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive CoCrMo in the HIP condition is that maker's cobalt-chromium-molybdenum grade, printed by laser powder bed fusion and then hot isostatically pressed. As built, it has a fine cellular structure with grains elongated along the build direction, residual stress and some internal porosity. HIP closes internal pores not connected to the surface, relieves residual stress and recrystallizes the structure, reducing anisotropy and improving ductility and fatigue resistance at some cost in strength. Supports still have to be removed, and the rough printed surface is unchanged and needs machining or polishing. Parts are used for wear- and corrosion-resistant orthopaedic and dental components and high-temperature aerospace parts. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS CobaltChrome MP1 is a cobalt-chromium-molybdenum alloy powder grade processed by laser powder bed fusion, in which a laser melts thin layers of the powder to build dense metal parts. Rapid solidification gives a very fine cellular microstructure in the as-built state, along with high residual stresses that call for a stress-relief heat treatment, usually before parts are cut from the build plate. Overhangs need supports, and the rough as-built surface is commonly blasted, machined or polished where fit or finish matters. Printed parts in this grade are used for dental crown and bridge frameworks, medical device components, and wear- and heat-resistant parts for turbines and engines. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS CobaltChrome MP1 is a cobalt-chromium-molybdenum alloy powder grade printed by laser powder bed fusion, here in the as-built state without heat treatment. Rapid melt-pool solidification gives a very fine cellular microstructure, largely metastable face-centred cubic, with high strength, limited ductility and some anisotropy between build directions. Parts carry residual stress, need supports on overhangs and have a rough surface, so they are usually stress relieved before removal from the plate and finished by blasting, machining or polishing. Typical uses are dental crown and bridge frameworks, medical device components and wear- or heat-loaded engine parts. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS CobaltChrome MP1 is a cobalt-chromium-molybdenum powder grade processed by laser powder bed fusion, here in the heat-treated condition. As built, it has a very fine cellular solidification structure, largely metastable face-centred cubic, with high residual stress and some anisotropy between build directions. Heat treatment, usually done before parts are cut from the build plate, relieves these stresses and homogenizes the microstructure, limiting distortion and directional differences. Supports must still be removed and functional surfaces machined or polished. Typical uses are dental frameworks, implant-type components and wear- or heat-resistant engine parts. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw CoCr-0404 is a cobalt-chromium alloy powder grade from Renishaw, processed by laser powder bed fusion. Rapid solidification of the melt pool gives the as-built alloy a fine cellular-dendritic microstructure, retained largely as metastable face-centred cubic phase, with higher strength than cast material. Parts carry significant residual stress, so they need supports and a stress-relief heat treatment before removal from the build plate. The as-built surface is rough, and functional surfaces are usually machined or polished. Printed parts are used for dental crown, bridge and partial denture frameworks, medical device components, and wear- and heat-resistant parts. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw CoCr-0404 printed by laser powder bed fusion and solution-treated is a cobalt-chromium-molybdenum alloy grade given a high-temperature solution heat treatment after printing. As built, rapid solidification leaves a fine cellular structure with segregation at cell boundaries, grains elongated along the build direction and high residual stress, so parts need supports and stress relief before removal from the plate. Solution treatment homogenises this structure, relieves stress and reduces anisotropy, trading some as-built strength for ductility. Rough surfaces still need machining or polishing. It is used for dental frameworks, orthopaedic components and wear-resistant industrial parts. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
CP Titanium Grade 2 printed by laser powder bed fusion is unalloyed titanium made by fully melting fine powder layer by layer under inert gas. Rapid solidification gives a fine acicular alpha-prime microstructure with columnar grains growing across layers, so properties can differ between build directions. Residual stress is significant, so parts are usually stress relieved before removal from the build plate, and rough as-built surfaces are machined or polished where it matters. Printed parts are used for patient-specific implants, lightweight lattice structures and corrosion-resistant fluid-handling hardware with complex internal channels.
EOS Titanium TiCP Grade 2 is a commercially pure Grade 2 titanium powder grade processed by laser powder bed fusion under argon. Rapid solidification gives a fine acicular alpha microstructure, so as-built parts are stronger and less ductile than annealed wrought material, with residual stress and a rough surface. Parts are usually stress relieved before removal from the build plate and supports, and may be hot isostatically pressed and machined or blasted. Typical uses are corrosion-resistant fluid-handling and chemical processing components, heat exchangers and lightweight parts with complex internal channels. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS Titanium TiCP Grade 2 is a commercially pure Grade 2 titanium powder for laser powder bed fusion, here in the as-built condition without heat treatment. Rapid melt-pool cooling gives a fine acicular alpha structure in columnar prior-beta grains, so as-built parts are generally stronger and less ductile than annealed wrought Grade 2. Parts carry residual stress, need supports and removal from the build plate, and have a rough layered surface, so stress relief and machining or finishing usually follow. Printed parts are used for corrosion-resistant fluid-handling and chemical-processing components, heat exchangers and lightweight lattice structures. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS Titanium TiCP Grade 2 in the heat-treated condition is commercially pure titanium Grade 2 printed by laser powder bed fusion from the maker's powder and heat treated after the build. As built, rapid melt-pool solidification gives a fine acicular alpha structure with high residual stress, and higher strength but lower ductility than annealed wrought material. Heat treatment relieves these stresses and coarsens the structure, recovering ductility and limiting distortion on removal from the plate. Parts still need support removal and machining or blasting of the rough surface. Uses include corrosion-resistant fluid-handling parts, heat exchangers and lattice structures where unalloyed titanium suits better than stronger alloys. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Hastelloy X printed by laser powder bed fusion is a solid-solution-strengthened nickel-chromium-iron-molybdenum superalloy built layer by layer from gas-atomized powder. Rapid solidification gives a fine cellular structure with columnar grains along the build direction, so properties differ between vertical and horizontal builds. The alloy is prone to microcracking and parts retain high residual stress, so they need supports, stress relief before removal from the plate, and machining of rough surfaces. Hot isostatic pressing and solution annealing are commonly applied to close porosity. Typical parts are combustor components, fuel nozzles and ducting for gas turbines.
Colibrium Additive Nickel X is the maker's Hastelloy X grade, a nickel-chromium-iron-molybdenum alloy, printed by laser powder bed fusion and left as built, before any heat treatment. As built, it has a fine cellular solidification structure in columnar grains elongated along the build direction. This gives anisotropic properties, high residual stress and rough supported and down-facing surfaces. Parts are normally stress relieved before removal from the plate, then usually hot isostatically pressed or solution annealed. It is used for gas turbine hot-section parts such as combustor components, fuel nozzles and compact heat exchangers. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive Nickel X is a Hastelloy X grade made by laser powder bed fusion, here in the solution-treated condition. As built, it has a fine cellular solidification structure, columnar grains along the build direction, anisotropic properties and high residual stress, so parts need supports and stress relief before removal from the plate. Solution treatment relieves these stresses, dissolves the cellular segregation and recrystallizes much of the structure, which reduces anisotropy and improves ductility. Printed parts serve in gas turbine hot sections, such as combustor components, fuel nozzles and heat shields with intricate cooling passages. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy HX is a grade of Hastelloy X, a solid-solution-strengthened nickel-chromium-iron-molybdenum alloy, made by laser powder bed fusion. As printed it has a fine cellular-dendritic structure with columnar grains along the build direction, so its properties differ between orientations, and it carries residual stress and a rough surface. Parts are usually stress relieved before removal from the plate and supports, and are often hot isostatically pressed or solution annealed to recrystallise the structure and close porosity. They are used for gas turbine combustor parts, fuel nozzles and heat exchangers that need oxidation resistance at high temperature. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy HX in the as-built condition is a Hastelloy X powder grade printed by laser powder bed fusion and not heat treated after the build. Fast melt-pool solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, so properties differ between build orientations. Parts carry high residual stress, rough downskin surfaces and supports, and the alloy is prone to solidification cracking. It is therefore usually stress relieved or solution annealed, often with hot isostatic pressing, before service. Typical uses are gas turbine combustor and burner parts and other hot-section components with internal cooling channels. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Hastelloy X is the nickel-chromium-iron-molybdenum alloy Hastelloy X, printed by laser powder bed fusion on the maker's own systems with its own process parameters. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, giving anisotropy between build directions, plus high residual stress and rough downskin surfaces. Parts are usually stress relieved on the plate, then solution annealed or hot isostatically pressed to recrystallize the structure and close porosity, with critical surfaces machined. Typical printed parts are gas turbine combustor liners, fuel nozzles, hot-section ducting and heat exchangers with internal passages. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Hastelloy X is the maker's grade of the nickel-chromium-iron-molybdenum alloy Hastelloy X made by laser powder bed fusion, here in the annealed condition. As built, it has a fine cellular structure with columnar grains along the build direction and high residual stress. It is also prone to solidification cracking, which the powder chemistry and process parameters are chosen to limit. Annealing relieves residual stress and partly recrystallizes the as-built structure, trading some strength for ductility and reducing anisotropy between build directions. Parts include gas turbine combustor hardware, fuel nozzles and heat exchangers with internal passages. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Hastelloy X in the as-built condition is this maker's grade of the nickel-chromium-iron-molybdenum alloy Hastelloy X, made by laser powder bed fusion and not heat treated after printing. Rapid solidification gives a fine cellular substructure within columnar grains elongated along the build direction, so properties vary with build orientation, and strength is higher but ductility lower than in wrought material. Parts carry high residual stress and a rough surface, and are usually stress-relieved, removed from supports, then hot isostatically pressed or solution annealed. Printed parts serve as gas turbine combustor components, fuel nozzles and heat exchangers. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Hastelloy X is the maker's grade of Hastelloy X, a nickel-chromium-iron-molybdenum alloy, printed by laser powder bed fusion and hot isostatically pressed. As printed, it has a fine cellular structure with grains elongated along the build direction, high residual stress and a tendency to solidification microcracking, giving direction-dependent properties. Hot isostatic pressing closes internal pores and cracks and recrystallizes the structure, reducing anisotropy and improving ductility and fatigue behaviour. Supports and rough surfaces still need removal and finishing. Parts are used for combustor liners, fuel nozzles, heat exchangers and other hot-section gas turbine components. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 625 made by bound metal deposition is the nickel-chromium-molybdenum-niobium alloy printed from metal-filled polymer filament, then debound and sintered into a metal part. The green part is printed oversize to allow for sintering shrinkage, and the sintered part keeps layer lines, a rougher surface than machined stock, and some porosity. Sagging during sintering limits long unsupported spans, so supports or setters are often needed, and properties can vary with build direction. Typical uses are corrosion-resistant fixtures, housings and fluid-handling parts, and low-volume components for marine, chemical and aerospace service.
Desktop Metal Nickel Alloy IN625 (Studio System 2) is the maker's grade of Inconel 625 printed by bound metal deposition, here in the sintered condition. Alloy powder held in a polymer and wax binder is extruded layer by layer, then debound and furnace-sintered, shrinking substantially, so parts are printed oversized to reach final dimensions. Sintering gives an equiaxed grain structure without the melt-pool texture of laser processes, but leaves some residual porosity, visible layer lines and a rough surface, so functional faces are usually machined. Parts serve as low-volume corrosion- and heat-resistant brackets, fittings, fixtures and prototypes for chemical, marine and energy equipment. Every value on this page is read from Desktop Metal's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Markforged Inconel 625 is the maker's grade of the nickel-chromium-molybdenum alloy printed by bound metal deposition, extruded as a metal-powder-filled polymer filament. The green part is debound and furnace-sintered, shrinking as it densifies, so it is printed oversize. It ends with a sintered grain structure and some closed residual porosity, without the melt-pool structure and residual stress of laser-fused parts. Surfaces show layer lines, and critical features are usually machined. Parts are used for corrosion- and heat-resistant fixtures, tooling, manifolds and low-volume replacement parts in chemical processing, marine and energy equipment. Every value on this page is read from Markforged's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Markforged Inconel 625 is the maker's grade of the nickel-chromium-molybdenum-niobium alloy printed by bound metal deposition, here as a part in the sintered condition. The part is extruded oversized from polymer-bound powder filament, debound to remove the binder and furnace-sintered, shrinking as the powder densifies into a near-dense metal with a sintered grain structure rather than a melt-pool structure. Some residual porosity remains, and layer lines leave a rough surface, so critical faces and holes are usually machined. Printed parts are used for corrosion- and heat-resistant fixtures, tooling, brackets and low-volume functional components in chemical, marine and industrial equipment. Every value on this page is read from Markforged's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 625 printed by laser powder bed fusion is the nickel-chromium-molybdenum-niobium alloy built layer by layer from fine gas-atomized powder. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, so properties can differ between vertical and horizontal builds. Parts have high residual stress and a rough as-built surface, need supports for overhangs, and are usually stress relieved on the plate, then often heat treated, hot isostatically pressed or machined. Printed parts serve as corrosion- and heat-resistant aerospace ducting, combustor components, heat exchangers and chemical-process hardware with complex internal passages.
3D Systems LaserForm Ni625 (A) is a grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, made by laser powder bed fusion. As printed, it has a fine cellular solidification structure with columnar grains along the build direction, so its properties differ between build directions. Parts carry residual stress and need supports, so they are usually stress relieved on the build plate, often hot isostatically pressed or solution annealed, and machined where the rough surface matters. Typical parts are corrosion- and heat-resistant heat exchangers, manifolds, combustion hardware and chemical processing components with internal channels. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni625 (A) is that maker's grade of Inconel 625 made by laser powder bed fusion, here in the annealed condition. As printed, the alloy has a fine cellular structure with niobium and molybdenum segregated at cell boundaries, columnar grains along the build direction and high residual stress. Annealing relieves that stress and homogenizes the structure, lowering strength, raising ductility and reducing anisotropy compared with the as-built state, while supports still need removing and functional surfaces machining. It is used for corrosion- and heat-resistant parts with complex internal passages, such as manifolds, heat exchangers and combustion hardware. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni625 (A) is a grade of Inconel 625 printed by laser powder bed fusion, here in the as-built condition without heat treatment. Rapid solidification gives a fine cellular-dendritic structure with niobium and molybdenum segregated to the cell boundaries, inside columnar grains elongated along the build direction, so properties vary with build orientation. Parts carry high residual stress, need supports and have rough surfaces, so printing is usually followed by stress relief, support removal and often machining. Typical uses are heat- and corrosion-resistant parts with internal channels, such as heat exchangers, manifolds and combustion hardware. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni625 (A) is Inconel 625 printed by laser powder bed fusion from that maker's powder grade and then stress-relieved. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, giving some anisotropy, and high residual stress. Stress relief, usually done on the build plate, lowers that stress and distortion on removal while largely keeping the as-built grain structure. Overhangs need supports, and the rough surface is often machined where sealing or fatigue matters. Typical parts are complex corrosion- and heat-resistant components such as heat exchangers, manifolds, ducting and exhaust parts. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 625 in the as-built condition is the nickel-chromium-molybdenum-niobium alloy exactly as it leaves the L-PBF machine, before stress relief, hot isostatic pressing or solution treatment. Rapid solidification gives fine cellular-dendritic grains, often elongated along the build direction, with niobium and molybdenum segregated between cells, so properties can vary with orientation. High residual stress can distort parts once they are cut from the plate, and surfaces are rough with supports to remove. The state is mainly a starting point for heat treatment and machining of parts for corrosion- and heat-exposed service, such as ducting and heat exchangers.
Colibrium Additive Nickel 625 is the maker's Inconel 625 grade for laser powder bed fusion, here as-built, without post-print heat treatment. Rapid melt-pool solidification gives a fine cellular-dendritic structure, columnar grains along the build direction and niobium and molybdenum segregation at cell boundaries, making properties orientation-dependent. Parts carry high residual stress, are anchored to the plate by supports and have rough down-facing surfaces, so stress relief, plate removal and often hot isostatic pressing or solution annealing and machining follow. Printed parts serve as heat- and corrosion-resistant components with internal channels, such as heat exchangers and combustion hardware. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive Nickel 625 is the maker's laser powder bed fusion grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625, here in the stress-relieved condition. Printing gives a fine cellular-dendritic structure with columnar grains along the build direction, interdendritic segregation of molybdenum and niobium, and high residual stress. Stress relief, usually done before parts are cut from the build plate, reduces distortion but largely keeps the as-built structure and its anisotropy between build directions. Supports must still be removed and rough surfaces machined or finished. Typical parts are heat- and corrosion-resistant components with internal passages, such as heat exchangers and manifolds. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN625 is a maker's grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, processed by laser powder bed fusion. As built it is near fully dense, with a fine cellular-dendritic structure and columnar grains along the build direction that make properties differ between orientations. Rapid solidification leaves residual stress and niobium segregation, so parts are stress-relieved before removal from the plate and often solution annealed or hot isostatically pressed. Overhangs need supports, and the rough surface is usually machined or polished. Parts serve as corrosion- and heat-resistant components with complex geometry, such as aerospace ducting, heat exchangers and chemical-processing hardware. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN625 is one maker's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 printed by laser powder bed fusion, here in the as-built condition. As built, it has a fine cellular-dendritic structure with columnar grains along the build direction and niobium and molybdenum segregated at cell boundaries. This makes it stronger but less ductile than annealed wrought alloy and gives it properties that differ between build directions. Parts carry high residual stress and a rough surface, need supports on overhangs, and are usually stress relieved before removal from the plate. They are used for corrosion- and heat-resistant manifolds, heat exchangers, ducting and combustion hardware. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN625 is a maker's powder grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625, printed by laser powder bed fusion and then heat-treated. As built, it has a fine cellular structure with niobium and molybdenum segregated to cell boundaries, columnar grains along the build direction and high residual stress. Heat treatment relieves that stress before parts are cut from the plate and can homogenize the structure, reducing anisotropy, though supports must still be removed and the rough surface usually machined. Typical parts are heat exchangers, combustion and exhaust hardware, ducting and fluid-handling components for aerospace, energy and chemical processing. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Nikon SLM Solutions IN625 is that maker's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 for laser powder bed fusion. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, so its properties differ between build orientations. Residual stress calls for stress relief before parts are cut from the plate. This is often followed by solution annealing or hot isostatic pressing, and by machining of the rough surface. Printed parts serve as heat exchangers, combustor and exhaust hardware, and chemical-processing or marine components with intricate internal channels. Every value on this page is read from Nikon SLM Solutions' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Nikon SLM Solutions IN625 is that maker's grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, for laser powder bed fusion, here annealed. As printed it has a fine cellular structure with niobium and molybdenum segregated to cell boundaries, grains elongated along the build direction and high residual stress, so parts need supports and stress relief before removal from the plate. Annealing relieves that stress and dissolves much of the segregation, lowering strength but raising ductility and reducing anisotropy. Parts serve as heat exchangers, combustor and exhaust hardware, manifolds and corrosion-resistant chemical and marine components with internal channels. Every value on this page is read from Nikon SLM Solutions' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Nikon SLM Solutions IN625 is that maker's grade of Inconel 625 for laser powder bed fusion, here in the as-built condition without heat treatment. Rapid solidification gives a fine cellular-dendritic structure, with niobium and molybdenum segregated to cell boundaries and columnar grains along the build direction. As a result, strength is high, ductility is below annealed wrought material and properties depend on build direction. Parts carry high residual stress and a rough surface, need supports on overhangs and are usually stress relieved, often also solution annealed or hot isostatically pressed. Typical uses are heat exchangers, combustor and exhaust parts, manifolds and chemical-process hardware with internal passages. Every value on this page is read from Nikon SLM Solutions' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw In625-0402 is that maker's grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, for laser powder bed fusion. Rapid solidification gives a fine cellular structure with niobium and molybdenum segregated to the cell walls, and columnar grains along the build direction make properties differ between orientations. Parts carry high residual stress, so they are stress relieved before removal from the plate and often solution annealed or hot isostatically pressed, then machined where the rough surface matters. Printed parts serve as corrosion- and heat-resistant components with complex internal passages, such as heat exchangers, manifolds and combustion hardware. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw In625-0402 printed by laser powder bed fusion is the maker's grade of the nickel-based alloy Inconel 625 in the as-built state, without heat treatment. Rapid solidification gives a fine cellular-dendritic microstructure with niobium and molybdenum segregated at cell boundaries and columnar grains along the build direction, so properties are anisotropic. Parts carry high residual stress, need supports and have a rough surface. Stress relief, often hot isostatic pressing or solution annealing, and machining usually follow. It is used for corrosion- and heat-resistant parts such as aerospace exhaust and combustion hardware, heat exchangers and chemical-processing components. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw In625-0402 is Renishaw's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 for laser powder bed fusion, here in the heat-treated condition. As printed, it has a fine cellular structure with niobium and molybdenum segregated at cell boundaries, columnar grains along the build direction and high residual stress, giving direction-dependent properties. Heat treatment relieves that stress before parts are removed from the plate and can homogenize and recrystallize the structure, reducing anisotropy; supports still have to be removed and functional surfaces machined. It is used for corrosion- and heat-resistant parts such as heat exchangers, manifolds and combustor and exhaust components. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625 is Velo3D's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 made by laser powder bed fusion. As printed, it has a fine cellular structure with niobium and molybdenum segregated to the cell walls and columnar grains running along the build direction, so its properties vary with build orientation. Residual stress is high, so parts are stress relieved on the build plate and are often hot isostatically pressed or solution annealed, then machined or finished where the rough surface matters. Typical parts are heat exchangers, rocket engine and combustor components, and manifolds with internal channels for hot, corrosive service. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625 as-built is the maker's grade of the nickel-chromium-molybdenum-niobium alloy UNS N06625 printed by laser powder bed fusion, with no heat treatment after printing. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction and niobium and molybdenum segregated to cell boundaries, which makes its properties anisotropic. Parts carry residual stress and a rough surface. They are normally stress relieved before removal from the build plate, often followed by annealing or hot isostatic pressing. Uses include heat exchangers, manifolds and combustion hardware for chemical, marine and aerospace service. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625 in the HIP condition is that maker's grade of the nickel-chromium-molybdenum-niobium alloy, printed by laser powder bed fusion and then hot isostatically pressed. As printed, it has a fine cellular structure with columnar grains along the build direction, niobium and molybdenum segregated to cell boundaries, and residual stress that needs relief before removal from the plate. HIP closes internal porosity and recrystallizes and homogenizes the structure, which reduces anisotropy, but it leaves the rough as-built surface. Parts serve as corrosion- and heat-resistant aerospace ducting, heat exchangers, combustion hardware and chemical-process fittings. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625, solution-treated, is that maker's laser powder bed fusion grade of the nickel-chromium-molybdenum-niobium alloy, heat treated after printing. As printed, it has a fine cellular-dendritic structure with niobium and molybdenum segregated to cell boundaries, columnar grains along the build direction and high residual stress. Parts are therefore stress relieved before removal from the build plate. Solution treatment dissolves the segregation and largely recrystallizes the grains, trading some as-built strength for ductility and more uniform properties across build directions. Typical parts are heat exchangers, manifolds and hot-section hardware needing corrosion and oxidation resistance at temperature. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 718 made by metal binder jetting is the nickel-chromium-iron superalloy formed by binding alloy powder layer by layer, then debinding and sintering the fragile green part. Sintering causes substantial, fairly uniform shrinkage that the design must allow for, and some residual porosity usually remains. With no melt pool, there is little thermal residual stress, less anisotropy than in laser-melted material, and generally no supports, though surfaces are rough. Parts usually need solution treatment and aging, sometimes hot isostatic pressing, and machining of critical features. Typical uses are batches of complex components for high-temperature service, such as turbomachinery and fluid-handling parts.
Desktop Metal Nickel Alloy IN718 (Shop System) in the HIP condition is Inconel 718 printed by metal binder jetting (BJT), sintered and then hot isostatically pressed. Green parts are debound and sintered with substantial shrinkage, giving an equiaxed grain structure without the melt-track texture or residual stress of laser fusion. HIP closes the internal porosity left after sintering, improving ductility and fatigue resistance, though surface-connected pores are not closed. An age-hardening treatment usually follows, and critical surfaces are machined. It is used for complex nickel alloy parts made in batches for high-temperature or corrosive service, such as impellers, nozzles and turbine hardware. Every value on this page is read from Desktop Metal's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 718 printed by laser powder bed fusion is the nickel-chromium-iron superalloy built from fine gas-atomized powder, melted layer by layer under inert gas. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, so as-built properties differ between build orientations, and niobium segregates to cell boundaries. Parts carry high residual stress and a rough surface, so they need stress relief on the plate, support removal, solution and aging treatment, often hot isostatic pressing, and machining of critical surfaces. Typical uses are turbine and combustor components, heat exchangers, manifolds and ducts.
LaserForm Ni718 (A) is the 3D Systems grade of Inconel 718 for laser powder bed fusion, a precipitation-hardening nickel superalloy printed from powder into dense parts. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, niobium segregation and high residual stress, so parts need supports and stress relief before removal from the build plate. Hot isostatic pressing, solution treatment and ageing then close porosity, precipitate the strengthening phases and reduce anisotropy. Printed parts serve in gas turbine and rocket engine hardware such as combustor parts, fuel nozzles, brackets and heat exchangers. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni718 (A) is that maker's grade of Inconel 718 nickel superalloy processed by laser powder bed fusion, in the as-built condition. Rapid solidification gives a fine cellular-dendritic structure in columnar grains along the build direction, with niobium segregated between cells and little age-hardening precipitation, so properties are anisotropic. Parts carry high residual stress and a rough surface, and are usually stress relieved on the plate, then hot isostatically pressed or solution treated and aged before service. They are used for gas turbine and rocket engine hardware such as combustor parts, fuel nozzles, brackets and heat exchangers. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni718 (A) is a heat-treated grade of the nickel superalloy Inconel 718 made by laser powder bed fusion. As built, the alloy has a fine cellular-dendritic structure with niobium segregation, columnar grains along the build direction and high residual stress, so parts need supports and stress relief. Heat treatment relieves that stress and ages the alloy to precipitate its strengthening phases, though grain texture and some anisotropy between build directions can remain. Parts serve in gas turbine and rocket engine hardware, brackets and heat exchangers that need complex geometry and strength at elevated temperature. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 718 printed by laser powder bed fusion in the as-built condition is the nickel-chromium-iron superalloy as it leaves the machine, before any stress relief, hot isostatic pressing or aging. Rapid melting and solidification give cellular-dendritic grains growing in columns along the build direction, with niobium and molybdenum segregated between dendrites, so properties differ between build and in-plane directions. High residual stress remains and can distort parts when they are removed from the build plate, and the surface is rough with support marks. It is used for prototypes, test coupons and parts that will be heat treated and finished afterward, such as turbine and combustor components.
Colibrium Additive Nickel 718 is a laser powder bed fusion grade of the precipitation-hardenable nickel superalloy Inconel 718, here in the aged condition. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, niobium segregation, directional anisotropy and high residual stress, so parts need supports and stress relief before removal from the plate. Aging precipitates the gamma double prime and gamma prime phases that strengthen the alloy, often after solution treatment or hot isostatic pressing. Printed parts serve as turbine and rocket engine components, combustor hardware, manifolds and brackets loaded at elevated temperature. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive Nickel 718 is that maker's grade of Inconel 718 made by laser powder bed fusion, here in the as-built condition without post-build heat treatment. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, interdendritic niobium segregation with Laves phase, and little of the strengthening gamma double prime precipitation. Parts carry high residual stress, differ in properties between build directions and have a rough surface, so they are normally stress relieved, hot isostatically pressed, and solution treated and aged. Printed parts are used for gas turbine and rocket engine hardware such as combustor and fuel system components, brackets and heat exchangers. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive Nickel 718 is the maker's Inconel 718 grade, printed by laser powder bed fusion and hot isostatically pressed. As built, it has fine columnar grains along the build direction, niobium-rich interdendritic segregation, high residual stress and rough downskin surfaces, so parts are stress relieved before support removal. Hot isostatic pressing closes internal pores, reduces segregation and anisotropy, and is usually followed by solution treatment and ageing to precipitate strengthening gamma double prime. Parts serve in gas turbine and rocket engines as combustor hardware, fuel nozzles, brackets and heat exchangers. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN718 is one maker's grade of Inconel 718, a precipitation-hardening nickel superalloy, supplied as powder for laser powder bed fusion. Rapid solidification gives a fine cellular-dendritic structure with niobium segregation and columnar grains along the build direction, so properties differ between build orientations. Parts need supports and a stress relief before removal from the plate. They then usually receive solution treatment and aging, often with hot isostatic pressing, and machining of critical surfaces. Typical uses are gas turbine and rocket engine parts such as combustor components, injectors and heat exchangers with internal channels. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN718 in the as-built condition is Inconel 718 made by laser powder bed fusion from this maker's powder, before any heat treatment. Rapid solidification leaves a fine cellular structure with columnar grains along the build direction and niobium segregation between cells, without the gamma double prime precipitation that age-hardens the alloy. Parts carry high residual stress, differ between build directions, need supports and have rough surfaces, so they are usually stress relieved on the plate, then solution treated and aged, often with hot isostatic pressing. The as-built state is mainly a starting point for turbine and rocket engine parts, brackets and heat exchangers. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN718 is a laser powder bed fusion powder grade of the precipitation-hardening nickel superalloy Inconel 718, here in the heat-treated condition. As built, it has a fine cellular-dendritic structure with niobium segregation, columnar grains along the build direction and high residual stress, so parts are stress-relieved before removal from the plate and supports. Solution treatment and double aging precipitate the gamma double-prime strengthening phase, sometimes after hot isostatic pressing to close porosity, though the columnar texture leaves some anisotropy. Parts serve as turbine and rocket engine components, combustor hardware and heat exchangers, with functional surfaces usually machined. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.