The present application is a National Phase of International Application Number PCT/GB2014/052256, filed Jul. 24, 2014, which claims priority from Great Britain Application Number 1314030.6, filed Aug. 6, 2013.
The present invention relates to an extrusion-based additive manufacturing system, and a method of manufacturing an object.
An extrusion-based additive manufacturing system is described in WO2012/037329. The system uses a filament as consumable feedstock. The filament has a core portion and a shell portion with different peak crystallization temperatures. Both the core and the shell portions are melted in an extrusion head, and after they have been deposited the portion with the higher crystallization temperature crystallizes before the other portion.
The present invention provides a method of manufacturing an object, the method comprising: extruding material from an extrusion head onto a tool, the extrusion head having an extrusion axis along which the material flows as it exits the extrusion head; generating a relative movement between the extrusion head and the tool as the material is deposited so that the material is deposited as a series of layers, wherein the material cures on or after deposition so that the layers are fused together, and controlling the extrusion of the material and the relative movement so that the series of layers are shaped in accordance with a stored three-dimensional model of the object. At least some of the layers are non-planar layers, and the relative movement during the deposition of each non-planar layer includes at least an element of rotation which causes an orientation between the extrusion axis and the tool to change at the same time as the material is extruded.
Forming some of the layers as non-planar layers enables the object to have improved structural properties. For instance the non-planar layers can be designed to follow lines of stress (such as hoop stress) in the object.
The extrusion axis meets the non-planar layer at a tilt angle which may remain constant or may change as the non-planar layer is deposited. Causing an orientation between the extrusion axis and the tool to change at the same time as the material is deposited enables this tilt angle to be controlled—for instance so that it does not change. An advantage of maintaining a tilt angle which remains constant as the non-planar layer is deposited is that it maintains a stable flow dynamic from the extrusion head to the non-planar layer.
Typically the relative movement during the deposition of each non-planar layer causes the orientation between the extrusion axis and the tool to change in accordance with a change in angle of the non-planar layer relative to the tool. In other words, the orientation is changed during deposition to follow the shape of the non-planar layer.
The material may be a thermoplastic material which cures by cooling, a thermosetting material which is cured by heating, or a material which is cured by some other mechanism (such as by photocuring or reacting with a chemical curing agent).
The extrudate which is extruded from the extrusion head and forms the object may be homogenous, but more typically it has a heterogenous structure. For instance the extrudate may comprise a reinforcement portion and a matrix portion which both run continuously along a length of the extrudate, wherein the reinforcement portion and the matrix portion have different material properties. The reinforcement portion and the matrix portion may for instance have a different melting point or a different crystallinity.
The tool may remain attached to the object, but more preferably the object and the tool are separated after the object has been manufactured, for instance by dissolving the tool. The tool may be dissolved by the action of a liquid dissolving agent, or by heating the tool so it melts and can be removed by a scraping tool or other mechanical method.
Typically at least some of the layers have a different size and/or a different shape in accordance with the stored three-dimensional model of the object.
The method may further comprise manufacturing the tool prior to manufacturing the object, the tool being manufactured by: extruding a tool material from an extrusion head onto a build member (such as a build plate); generating a relative movement between the extrusion head and the build member as the tool material is extruded onto the build member plate so that the tool material is deposited as a series of tool layers, wherein the tool material cures on or after deposition so that the tool layers are fused together, and controlling the extrusion of the tool material and the relative movement so that the series of tool layers are shaped in accordance with a stored three-dimensional model of the tool.
The extrusion head which manufactures the tool may be the same as the extrusion head which forms the object. Alternatively the tool and the object may be manufactured by different respective extrusion heads.
Typically each tool layer is substantially planar, in contrast with the object in which at least some of the layers are non-planar. In this case the tool and the object are preferably manufactured by different extrusion heads—the tool extrusion head being able to translate but not rotate.
The tool material may have different material properties to the material forming the object. For instance the tool material may be homogenous and the material forming the object may be heterogenous. In this case the tool and the object are preferably manufactured by different extrusion heads—it being easier to switch between different extrusion heads than to change the material being fed to a single extrusion head.
The relative rotation may be generated by rotating the extrusion head without rotating the tool, by rotating the tool without rotating the extrusion tool, or by rotating both. The relative motion of the extrusion head and the tool during deposition of the non-planar layers may be a pure orbital rotation (that is a rotation about a single point with no relative translation) but more typically it is a compound motion comprising a mixture of rotation and translation.
A further aspect of the invention provides a system for manufacturing an object by an extrusion-based additive manufacturing method, the system comprising: an extrusion head having a channel with an extrusion outlet; a build member; a feed mechanism for feeding material into the channel of the extrusion head so that the material is extruded from the extrusion outlet; a drive system arranged to cause relative translation between the extrusion head and the build member along three axes, and relative rotation between the extrusion head and the build plate about at least two axes; a memory (typically a computer memory) for storing a three-dimensional model of the object; and a controller programmed to operate the feed mechanism and the drive system in order to manufacture the object on the build plate by extrusion-based additive manufacturing in accordance with the three-dimensional model of the object stored in the memory, wherein the controller is programmed to cause the drive system to generate at least an element of relative rotation between the extrusion head and the build member at the same time that the feed mechanism causes the material to be extruded from the extrusion outlet.
Each layer of the object may be manufactured with a single extruded line or road only, for instance following a serpentine pattern. However more preferably each layer is manufactured with multiple extruded lines.
Embodiments of the invention will now be described with reference to the accompanying drawings, in which:
Apparatus for manufacturing an object by an extrusion-based additive manufacturing method is shown in
A 3-axis drive system 8a is arranged to move the tool extrusion head 1a along three axes relative to the build plate 7. The drive system 8a is capable of translating the tool extrusion head 1a back and forth in the X and Z directions (in the plane of
A 5-axis drive system 8b is arranged to move the object extrusion head 1b along and about five axes relative to the build plate 7. The drive system 8b is capable of translating the object extrusion head back and forth in the X and Z directions (in the plane of
In this embodiment of the invention the build plate 7 remains stationary and all movement is performed by the extrusion heads 1a,b. However it will be appreciated that in alternative embodiments some or all of the relative movement between the extrusion heads and the build plate 7 may be achieved by moving the build plate instead. For instance the build plate 7 could be translated in Z so the 5-axis drive system 8b is replaced by a 4-axis drive system and the 3-axis drive system 8a is replaced by a two-axis drive system.
The detailed construction of the extrusion heads 1a,b is shown in
A controller 35 controls the heaters 5a, 5b, 6, 34, the motorized rollers 4a, 4b, 30 and the drive systems 8a,b in order to manufacture an object in accordance with a Computer Aided Design (CAD) model of the object in a computer memory 36 by following the process shown in
First, the tool extrusion head 1a is used to manufacture a tool on the build plate by the process of
The process of
Next, the tool extrusion head 1a is moved away and the object extrusion head 1b is used to manufacture an object on the tool 40 by the process of
The drive rollers 4b feed a reinforcement fibre 20 into the chamber 2 via the fibre feed channel at a velocity V1 m/s. The diameter of the reinforcement fibre 20 is typically of the order of 0.08 mm to 0.6 mm, with the drive rollers 4b being spaced apart as required to provide a fibre feed channel with an equivalent diameter.
The reinforcement fibre 20 is manufactured by spinning and drawing a polymer under tension to form one or more filaments with crystallites aligned with the length of the fibre. The reinforcement fibre 20 may consist of a single one of such filaments, or it may comprise a plurality of such filaments. The polymer chains and crystallites in the reinforcement fibre 20 are aligned with its length.
Suitable materials for the reinforcement fibre 20 include polyethylene (PE), High Density polyethylene (HDPE), Ultra High Density polyethylene (UHDPE), Acrylonitrile butadiene styrene (ABS), Polypropylene (PP), Polydimethyl siloxane (PDMS), Polyoxymethylene (POM), Polyethylene terephthalate (PET), Polyetheretherketone (PEEK), Polyamide (PA), Polysulphone (PS), Polyphenylene sulphide (PPS), Polyphenylsulfone (PPSF), Polytetrafluoroethylene (PTFE), or polyvinylidene fluoride (PVDF).
Dyneema® is one example of a suitable UHDPE fibre which can provide a yield strength greater than 2 GPa and preferably greater than 2.4 GPa, a crystallinity by weight which is greater than 80% and preferably greater than 85%, and has polymer chains with a parallel orientation greater than 90% or more preferably greater than 95%.
A matrix feed tube 37 is mounted to the body 10 towards the upper end of the chamber 2b. The interior of the matrix feed tube 37 provides a cylindrical matrix feed channel with an inlet 31 at its outer (distal) end and an outlet 32 in the side of the body 10 at its inner (proximal) end. A pair of motorized matrix feed rollers 30 are arranged to feed a matrix fibre (not shown) into the matrix feed channel. Alternatively the matrix material could be fed into the matrix feed channel in the form of a powder. The tube 37 carries a matrix heater 34 which melts the matrix fibre in the tube 37 to transform it into liquid matrix material. The liquid matrix material then flows into the chamber 2b through the outlet 32 at a velocity V2 m/s controlled by the rotation rate of the rollers 30.
The matrix feed tube 37 is oriented at right angles to the fibre feed tube 15,16 but may also be oriented so that the matrix is fed downwardly into the chamber at an acute angle to the reinforcement fibre if desired.
The matrix material forming the matrix fibre is typically the same polymer as the material forming the reinforcement fibre 20, optionally with different molecular weights. Where the molecular weights are different, then preferably the reinforcement fibre material has the higher molecular weight (for instance between 2,000,000 and 6,000,000 in the case of UHDPE). The reinforcement fibre 20 also has a higher crystallinity than the matrix fibre 33. This higher crystallinity results in a higher melting point.
Typically the fibres are both formed by drawing the fibre under tension from a polymer melt. However the crystallinity of the reinforcement fibre 20 is enhanced compared with the matrix fibre by using a slower cooling rate, a higher drawing rate and/or a polymer with a higher molecular weight.
First, the fibre drive rollers 4b are driven to feed the reinforcement fibre 20 into the chamber and through the extrusion outlet 3b. The inwardly tapering shape of the lower part of the chamber 2b assists in guiding the fibre 20 towards the extrusion outlet 3b. The drive system 8b is driven to move the extrusion head 1b into a desired position. The matrix heater 34 is turned on to melt the matrix fibre in the tube 37 and transform it into liquid matrix material. The matrix drive rollers 30 are then operated to feed the liquid matrix material into the chamber 2b.
The liquid matrix material wets the upper portion of the reinforcement fibre 20 in the fibre feed tube 16 via the lateral holes in the lattice structure, as well as contacting the lower portion of the reinforcement fibre 20 between the outlet of the fibre feed channel and the extrusion outlet 3b.
The fibre feed rollers 4b and matrix feed rollers 30 are then driven simultaneously to extrude a coated fibre 50 from the extrusion outlet 3b as shown in
The diameters of the fibre 20 and the extrusion outlet 3b are selected to provide an extrudate (that is, the coated fibre 50) in which the fibre 20 occupies a volume greater than 30% of the extrudate and preferably a volume in the range of 40-60% of the extrudate.
The reinforcement fibre 20 may be relatively rigid so it can be “pushed” through the chamber by the fibre driver rollers 4b, moving in and out of the chamber at the same velocity V1 relative to the chamber. Alternatively the reinforcement fibre 20 may be pulled into the chamber by the viscous drag forces created by the action of the flowing liquid matrix material on the reinforcement fibre in the chamber.
The reinforcement fibre 20 does not change in cross-section as it passes through the chamber, so the extruded coated fibre 50 has a cross-sectional area transverse to its length (defined by the area of the extrusion outlet 3b) which is greater than that of the fibre 20 entering the chamber.
The matrix feed channel on the other hand has a diameter D2 of the order of 3 mm which is much greater than the diameter D1 of the extrusion outlet 3b. Consequently the cross-sectional area A2 of the matrix feed channel (and the solid matrix fibre being fed into it) is greater than the cross-sectional area A1 of the extrusion outlet (and the coated fibre 50 being extruded from it). The area A2 is also greater than the cross-sectional area of the matrix coating of the coated fibre 50. Consequently the liquid matrix material has a relatively slow velocity V2 relative to the chamber as it flows into the chamber at the inlet 32 into the chamber, but it is extruded out of the extrusion outlet 3b with the coated fibre 50 at a higher velocity V1.
The large diameter D2 of the matrix feed channel (and the solid matrix fibre being fed into it) means that the solid matrix fibre has sufficient buckling strength to allow it to be driven by the matrix feed rollers 30 into the matrix feed channel with sufficient force to apply a positive pressure. This positive pressure elevates the pressure of the liquid matrix material in the extrusion chamber, and can be controlled by appropriate operation of the rollers 30. The elevated pressure in the extrusion chamber provides two benefits. Firstly it assists the wetting of the reinforcement fibre 20 by the liquid matrix material. Secondly, it reduces the likelihood of defects in the coating of the extruded coated fibre 50.
As the coated fibre 50 is extruded, the drive system 8b is operated to cause relative movement between the extrusion outlet 3b and the build plate 7 and tool 40 as the coated fibre 50 is extruded from the extrusion outlet, depositing a first extruded line 50 (also known as a “road”) onto the tool as shown in
The pair of heaters 5b,6 are independently controllable by the controller 35. As the coated fibre is extruded, both heaters 5b,6 are operated to heat the chamber and prevent the matrix material in the chamber from solidifying. However during extrusion the temperature in the chamber is kept below the melting point of the reinforcement fibre 20 so it remains rigid.
When a break is required in the extruded line 50, then the fibre heater 6 is operated to temporarily raise the temperature of the reinforcement fibre in the lower part of the extrusion head 1b above its melting point, thereby forming a break in the continuous reinforcement fibre. At the same time the drive system 8b is operated to move the extrusion head 1b away from the tool 40 and effectively “cut” the coated fibre to form an end 22 of the extruded line 50.
Next, the fibre heater 6 is turned down to lower the temperature in the lower part of the extrusion chamber back below the melting point of the reinforcement fibre 20 to enable a further line 51 to be extruded as shown in
A small amount of amorphous material is extruded out of the chamber 2b between the cut lines 50 and 51. This material can deposited at the edge of the part and machined away after the whole part has been formed. The number of cuts 22 in a given part is minimised in order to minimise the quantity of such amorphous material.
The length of time of the heat pulse which “cuts” the coated fibre at the end of each line will depend on a number of factors, mainly the thermal mass of the extrusion head 1b, but it will typically be of the order of 0.1 to 10 s.
The matrix coating of the extruded coated fibre 51 fuses with the coating of the previously extruded coated fibre 50 and solidifies after it has done so. In the case of
Next, the fibre heater 6 is operated again to temporarily raising the temperature of the fibre in the extrusion head above its melting point after the second line 51 has been extruded, thereby forming a break. At the same time the drive system 8b is operated to move the head 1b away from the tool and effectively “cut” the fibre to form an end of the extruded line 51.
This process is then repeated a number of times as required to manufacture a first layer 55 of the object in accordance with the CAD model in the memory as shown in the plan view of
The next layer 70 is then formed over the first layer 55 as shown in
The process is then repeated further until the entire object has been built with a series of dome-shaped layers similar to the layers of an onion. The object may be, for example, a helmet.
The rotation 60 of the head 1b shown in
In the simplified example of
This change of orientation of the head 1b relative to the tool axis 64 during extrusion provides a number of advantages:
After the object has been fully formed, the tool 40 carrying the object 80 is immersed in a bath of solvent 85 as shown in
Although the invention has been described above with reference to one or more preferred embodiments, it will be appreciated that various changes or modifications may be made without departing from the scope of the invention as defined in the appended claims.
Number | Date | Country | Kind |
---|---|---|---|
1314030.6 | Aug 2013 | GB | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/GB2014/052256 | 7/24/2014 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2015/019053 | 2/12/2015 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4247508 | Housholder | Jan 1981 | A |
5121329 | Crump | Jun 1992 | A |
5134569 | Masters | Jul 1992 | A |
5340433 | Crump | Aug 1994 | A |
5633021 | Brown | May 1997 | A |
5717599 | Menhennett | Feb 1998 | A |
5866058 | Batchelder | Feb 1999 | A |
6324440 | Hillier | Nov 2001 | B1 |
6441338 | Rabinovich | Aug 2002 | B1 |
7848838 | Gershenfeld | Dec 2010 | B2 |
9364995 | Roberts, IV | Jun 2016 | B2 |
9789652 | Armstrong | Oct 2017 | B2 |
9962799 | Hascoet | May 2018 | B2 |
20110215501 | Elyasi | Sep 2011 | A1 |
20130015596 | Mozeika | Jan 2013 | A1 |
20130197683 | Zhang | Aug 2013 | A1 |
20130209600 | Tow | Aug 2013 | A1 |
20140232035 | Bheda | Aug 2014 | A1 |
20140252668 | Austin | Sep 2014 | A1 |
20140284832 | Novikov | Sep 2014 | A1 |
20140287139 | Farmer et al. | Sep 2014 | A1 |
20140328963 | Mark | Nov 2014 | A1 |
20150021832 | Yerazunis | Jan 2015 | A1 |
20150230912 | Lee | Aug 2015 | A1 |
20150239148 | Israel | Aug 2015 | A1 |
20150266243 | Mark | Sep 2015 | A1 |
20150266244 | Page | Sep 2015 | A1 |
20150298393 | Suarez | Oct 2015 | A1 |
20150375344 | Adcock | Dec 2015 | A1 |
20160001461 | Gardiner | Jan 2016 | A1 |
20160046755 | Boday | Feb 2016 | A1 |
20160096331 | Linnell | Apr 2016 | A1 |
20160198576 | Lewis | Jul 2016 | A1 |
20170066194 | Bromer | Mar 2017 | A1 |
20170106594 | Gardiner | Apr 2017 | A1 |
20170173868 | Mark | Jun 2017 | A1 |
20170240298 | Goehlich | Aug 2017 | A1 |
Number | Date | Country |
---|---|---|
3904230 | Aug 1990 | DE |
4422146 | Jan 1996 | DE |
2013146936 | Aug 2013 | JP |
2012037329 | Mar 2012 | WO |
2013108914 | Jul 2013 | WO |
Entry |
---|
http://www.thingiverse.com/thing:75735 dated Jan. 25, 2016. |
http://www.dezeen.com/2013/05/17/mataerial-3d-printer-by-petr-novikov-sasa-jokic-and-joris-laarman-studio/. |
UKIPO Search Report dated Jan. 22, 2014 issued in Great Britain Application No. 1314030.6. |
ISR and WO dated Oct. 23, 2014 issued in PCT/GB2014/052256. |
Number | Date | Country | |
---|---|---|---|
20160176109 A1 | Jun 2016 | US |