Additive manufacturing machines produce 3D objects by building up layers of material. Some additive manufacturing machines are commonly referred to as “3D printers.” 3D printers and other additive manufacturing machines make it possible to convert a CAD (computer aided design) model or other digital representation of an object into the physical object. The model data may be processed into slices each defining that part of a layer or layers of build material to be formed into the object.
In the following detailed description, reference is made to the accompanying drawings which form a part hereof, and in which is shown by way of illustration specific examples in which the disclosure may be practiced. It is to be understood that other examples may be utilized and structural or logical changes may be made without departing from the scope of the present disclosure. The following detailed description, therefore, is not to be taken in a limiting sense, and the scope of the present disclosure is defined by the appended claims. It is to be understood that features of the various examples described herein may be combined, in part or whole, with each other, unless specifically noted otherwise.
In some additive manufacturing processes, thermic energy is used to fuse together the particles in a powdered build material to form a solid object. Thermic energy to fuse the build material may be generated, for example, by applying a liquid fusing agent to a thin layer of powdered build material in a pattern based on the object slice and then exposing the patterned area to fusing energy. Fusing energy absorbing components in the fusing agent absorb fusing energy to help sinter, melt or otherwise fuse the build material. The process is repeated layer by layer and slice by slice to complete the object.
Roller 16 is mounted to carriage 12 and positioned within a radiative heat transfer area 26 generated by thermic source 14, as described further below. Radiative heat transfer area 26 has a view factor between thermic source 14 and roller 16. The view factor is a coefficient scaling radiation exchange between two heat sources determined by geometric factors. Heat flux provided by thermic source 14 and roller 16 can be determined by the view factor, emission spectra, temperature, and power between thermic source 14 and roller 16. Roller 16 within radiative heat transfer area 26 receives localized heat including reflective energy generated by thermic source 14. Radiative heat transfer area 26 includes direct and indirect thermic energy including reflective energy generated by thermic source 14 and reflected from a build surface 28 formed of build material 22 and fusing agent 24, for example, within build zone 18. Excess irradiant energy from thermic source 14 is absorbed by roller 16 along a longitudinal section 30 of an exterior surface 32 of roller 16 extending along a y-axis orthogonal to the x-axis.
Roller 16 is cylindrical and is rotatable around a central longitudinal axis 34 extending in the y-axial direction. Rotating roller 16 while exposing roller 16 to irradiant energy from thermic source 14 uniformly heats exterior surface 32 of roller 16. Roller 16 can be rotated within radiative heat transfer area 26 to provide uniform heating of exterior surface 32 around an entire outer circumference of roller 16. Uniform heating of roller 16 can assist in affecting uniformity in heating of build material 22 at each subsequent spread layer.
With respect to thermic source 14 of fusing system 10, thermic source 14 can include any suitable number and type of thermic sources to heat and irradiate build material. Thermic source 14 can include lower color temperature warming lamps and higher color temperature fusing lamps to provide control for heating and fusing of build material 22. Thermic source 14, illustrated in
With reference to
Second pass 76 is illustrated in
With additional reference to
With continued reference to
Roller 16 includes at least one indexed marker 921-92x to indicate the rotational orientation of roller 16. Indexed markers 92 can be visible, mechanical, or electronic markers that controller 42 can use with techniques to repeatedly align and position index markers 92 in the same phased locations 941-94x across build zone 18 to form substantially uniform build material thicknesses, layer upon layer. Synchronizing the rotational position of roller 16 using index markers 92 to align with phased locations 94 of build zone 18 aids in maintaining and controlling build material 22 layer thickness uniformly.
In one example, controller 42 uses indexed markers 921-92x to align specific surface 32 areas of roller 16 with specific areas of build material 22 build surface 28. In one example, indexed markers 921-92x includes a non-indexed encoder that provides circumferential position and controller 42 determines a circumferential position relative to an initial position from the non-indexed encoder. Controller 42 can determine an absolute roller index position (e.g., 921) during initialization of first pass 72 to coordinate placement of specific areas of exterior surface 32 with specific areas of build surface 28 of build material 22 in build zone 18 (e.g., 941) while spreading. In one example, controller 42 interrupts roller 16 at a specific position (e.g., 921) at termination, or completion, of fusing pass 84 to re-aligned for subsequent spreading pass 72.
Rotation of roller 16 can be timed, paused, and restarted at an integer number of turns (e.g., 921) as indicated with index markers 92. For example, rotation of roller 16 can be paused after fusing to end at a specific rotational, or indexed, position. Techniques can be used to rotate roller 16 a fixed amount in order that indexed markers 921-92x are positioned in the original position to begin the next spreading pass in the appropriate phased locations 941-94x aligned with build zone 18. At the conclusion of fusing and before spreading a subsequent layer, roller 16 stops at a predetermined specific position using index marker 92 to synchronize with phased location 94 across build zone 18 to control layer thickness uniformity. Synchronization of roller 16 across build zone 18 from pass to pass at each build layer provides that roller 16 can be phased along build zone 18, regardless of direction of travel.
Roller 16 is rotated across build zone 18 to evenly spread build material 22. Rotating roller 16 while roller 16 is lifted, or raised above build zone 18 and not in contact with build material 22 or fusing agent 24 on build zone 18 during fusing passes continues to evenly heat roller 16. The uniformly heated roller 16 provides a more uniform spread powder temperature. Roller 16 can be continuously rotated during passing over build zone 18 as well as when off build zone 18 to maintain uniform heating of roller 16. When not spreading build material 22, roller 16 does not perform a function; continuing rotation of roller 16 outside of the spreading function maintains a uniformly heated exterior surface 32 of roller 16. The passing of roller 16 over build zone 18 can be timed to synchronize the rotational orientation of roller 16 to match previous rotational orientation contact locations of build zone 18. Roller 16 can be rotated clockwise or counter-clockwise, depending on the direction of travel across build zone 18.
Although specific examples have been illustrated and described herein, a variety of alternate and/or equivalent implementations may be substituted for the specific examples shown and described without departing from the scope of the present disclosure. This application is intended to cover any adaptations or variations of the specific examples discussed herein. Therefore, it is intended that this disclosure be limited only by the claims and the equivalents thereof.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2017/028990 | 4/21/2017 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2018/194688 | 10/25/2018 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4752352 | Feygin | Jun 1988 | A |
5876550 | Feygin | Mar 1999 | A |
5943235 | Earl | Aug 1999 | A |
6030199 | Tseng | Feb 2000 | A |
6169605 | Penn | Jan 2001 | B1 |
6357855 | Kerekes | Mar 2002 | B1 |
6896839 | Kubo | May 2005 | B2 |
7008209 | Iskra et al. | Mar 2006 | B2 |
7073442 | Fedor | Jul 2006 | B2 |
8636494 | Gothait | Jan 2014 | B2 |
8646877 | Thompson et al. | Feb 2014 | B2 |
9492956 | Horiuchi | Nov 2016 | B2 |
9931785 | Cullen | Apr 2018 | B2 |
10300548 | Fisser | May 2019 | B2 |
10391754 | Hakkaku | Aug 2019 | B2 |
10639853 | Ohi | May 2020 | B2 |
10843409 | Kobayashi | Nov 2020 | B2 |
10981331 | Barnes | Apr 2021 | B2 |
11072123 | Hartman | Jul 2021 | B2 |
20020104973 | Kerekes | Aug 2002 | A1 |
20050104241 | Kritchman | May 2005 | A1 |
20050242473 | Newell et al. | Nov 2005 | A1 |
20140255666 | Stucker et al. | Sep 2014 | A1 |
20140265045 | Cullen | Sep 2014 | A1 |
20140314613 | Hopkinson et al. | Oct 2014 | A1 |
20150136318 | Tiefel | May 2015 | A1 |
20150165681 | Fish et al. | Jun 2015 | A1 |
20160039152 | Hara | Feb 2016 | A1 |
20160059482 | Hakkaku | Mar 2016 | A1 |
20160067929 | Park | Mar 2016 | A1 |
20160311164 | Miyano | Oct 2016 | A1 |
20170021419 | Ng et al. | Jan 2017 | A1 |
20170100896 | Hakkaku | Apr 2017 | A1 |
20180194060 | Hara | Jul 2018 | A1 |
20180250871 | Mugishima | Sep 2018 | A1 |
Number | Date | Country |
---|---|---|
106270877 | Jan 2017 | CN |
3053730 | Aug 2016 | EP |
08137325 | May 1996 | JP |
WO-2014144482 | Sep 2014 | WO |
WO-2015056230 | Apr 2015 | WO |
WO-2016048348 | Mar 2016 | WO |
WO-2016119898 | Aug 2016 | WO |
Entry |
---|
King, W.E. et al., Laser powder bed fusion additive manufacturing of metals; physics, computational, and materials challenges, Applied Physics Reviews 2, 041304, 2015. |
Roy, N.K., μ-SLS of Metals: Design of the powder spreader, powder bed actuators and optics for the system, 2015 < https://sffsymposium.engr.utexas.edu/sites/default/files/2015/2015-11-Roy.pdf >. |
Wimpenny, Selective Infrared Sintering of Polymeric Powders using Radiant IR Heating & Ink Jet Printing, DeMontfort University, Sep. 14, 2006, pp. 789-799. |
Number | Date | Country | |
---|---|---|---|
20210197452 A1 | Jul 2021 | US |