FIXTURE FOR ADDITIVE MANUFACTURING AND HEAT TREATMENT

Abstract

A fixture for use in an additive manufacturing and heat treatment process is disclosed. The fixture includes a tool with an upper surface and a lower surface, and an attachment system configured to releasably secure a substrate to the upper surface of the tool. The tool includes a body with an upper face and a lower face, and a reinforcement layer cladding the upper or lower face of the body. The reinforcement layer may be a superalloy.

Claims

1. A fixture for use in an additive manufacturing and heat treatment process, the fixture comprising: a tool with an upper surface and a lower surface; and an attachment system configured to releasably secure a substrate to the upper surface of the tool, wherein the tool comprises a body with an upper face and a lower face, and a reinforcement layer cladding the upper or lower face of the body.

2. A fixture according to claim 1 wherein the reinforcement layer is a lower reinforcement layer cladding the lower face of the body.

3. A fixture according to claim 2 wherein the lower reinforcement layer has a lower thermal expansion coefficient than the body.

4. A fixture according to claim 1 wherein the reinforcement layer is an upper reinforcement layer cladding the upper face of the body.

5. A fixture according to claim 4 further comprising a lower reinforcement layer cladding the lower face of the body.

6. A fixture according to claim 1 wherein the or each reinforcement layer comprises a metal reinforcement material.

7. A fixture according to claim 1 wherein the or each reinforcement layer has a thickness greater than 1 mm.

8. A fixture according to claim 1 wherein the or each reinforcement layer has a thickness less than 30 mm.

9. A fixture according to claim 1 wherein the upper and lower faces of the body are separated by a depth of the body, and the or each reinforcement layer has a thickness which is less than the depth of the body.

10. A fixture according to claim 1 wherein the or each reinforcement layer comprises a reinforcement material with a Young's modulus which reduces by less than 30% or less than 20% between 93 C. and 649 C.

11. A fixture according to claim 1 wherein the or each reinforcement layer comprises a reinforcement material with a yield strength 0.2% which reduces by less than 30% or less than 20% between 93 C. and 649 C.

12. A fixture according to claim 1 wherein the or each reinforcement layer comprises a reinforcement material with a Young's modulus at 500 C. which is greater than 100 GPa or greater than 150 GPa.

13. A fixture according to claim 1 wherein the body comprises a body material; the or each reinforcement layer comprises a reinforcement material; and a Young's modulus at 500 C. of the or each reinforcement material is greater than a Young's modulus at 500 C. of the body material.

14. A fixture according to claim 1 wherein the or each reinforcement layer comprises a reinforcement material with a yield strength 0.2% at 500 C. which is greater than 400 MPa or greater than 600 MPa.

15. A fixture according to claim 1 wherein the body comprises a body material; the or each reinforcement layer comprises a reinforcement material; and a yield strength 0.2% at 500 C. of the or each reinforcement material is greater than a yield strength 0.2% at 500 C. of the body material.

16. A fixture according to claim 1 wherein the or each reinforcement layer is bonded to the body.

17. A fixture according to claim 1 wherein the reinforcement layer clads the upper or lower face of the body, and the lower or upper face of the body opposite the reinforcement layer is not clad in reinforcement material.

18. A method of manufacturing the fixture of claim 1, the method comprising cladding the body with the or each reinforcement layer by a welding process or a spraying process.

19. A method of additive manufacturing and heat treatment, the method comprising: a. providing a fixture according to claim 1; b. securing a substrate to the upper surface of the tool with the attachment system; c. operating an additive manufacturing system to perform a build process by building a part on the substrate secured to the tool, the part being built by forming a series of layers of metallic material on the substrate, the metallic material melting and solidifying during the build process thereby bonding the part to the substrate and creating thermally induced stress in the part; d. moving the part, the substrate and the fixture from the additive manufacturing system to a heat treatment system, wherein the substrate remains secured to the tool and the part remains bonded to the substrate as they are moved; e. operating the heat treatment system to perform a heat treatment process by heating the part, the substrate and the fixture together thereby relieving the thermally induced stress in the part, the substrate remaining secured to the tool during the heat treatment process; f. operating the attachment system to release the substrate from the tool so that the substrate is no longer secured to the tool by the attachment system; and g. separating the part and the substrate from the fixture, wherein the part remains bonded to the substrate as they are separated from the fixture.

20. Apparatus for performing the method of claim 19, the apparatus comprising: a. an additive manufacturing system which can be operated to perform the build process; b. a heat treatment system which can be operated to perform the heat treatment process; and c. a fixture comprising a tool with an upper surface and a lower surface, and an attachment system configured to releasably secure a substrate to the upper surface of the tool, wherein the tool comprises a body with an upper face and a lower face, and a reinforcement layer cladding the upper or lower face of the body, wherein the fixture can be moved between the additive manufacturing system and the heat treatment system.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0047] Embodiments of the invention will now be described with reference to the accompanying drawings, in which:

[0048] FIG. 1 illustrates an additive manufacturing system and heat treatment system;

[0049] FIG. 2 illustrates the forces acting on the substrate in the clamped condition during deposition;

[0050] FIG. 3 illustrates the distortion which would result if the clamps were released before heat treatment;

[0051] FIG. 4 is a plan view of an alternative tooling arrangement;

[0052] FIG. 5 is a side view of the tooling arrangement of FIG. 4;

[0053] FIG. 6 is an isometric view of the tooling arrangement of FIG. 4;

[0054] FIG. 7 shows an alternative method of securing the substrate to the tool;

[0055] FIG. 8 shows a method of forming one of the reinforcement layers;

[0056] FIG. 9 is a graph of yield strength 0.2% versus temperature;

[0057] FIG. 10 is a graph of Young's module versus temperature; and

[0058] FIG. 11 shows a further alternative tooling arrangement with only a lower reinforcement layer.

DETAILED DESCRIPTION OF EMBODIMENT(S)

[0059] FIG. 1 shows an additive manufacturing system 1 and a heat treatment system 2. The additive manufacturing system 1 comprises a chamber containing a table 3 and a build head 4. A fixture 15 is shown in FIG. 1 on the table 3. The fixture 15 comprises a tool 5, 25a, 25b; and a pair of clamps 7, 8.

[0060] The tool comprises a body 5 and a pair of reinforcement layers 25a, 25b. The body 5 comprises a continuous block of body material (for instance mild steel S355J2H) with an upper face 5a and a lower face 5b. The upper reinforcement layer 25a clads the external upper face 5a of the body, and the lower reinforcement layer 25b clads the external lower face 5b of the body. The upper and lower reinforcement layers 25a, 25b are made from the same reinforcement material, which by way of example may be a super alloy such as Inconel 623, Inconel 718, or a cobalt chrome alloy.

[0061] The tool has an upper surface 14 (the external face of the upper reinforcement layer 25a) and a lower surface (the external face of the lower reinforcement layer 25b) opposite the upper surface 14. In a first step, a substrate 6 is placed on the upper surface 14 of the tool and secured by clamps 7, 8 to the upper surface 14 of the tool. The upper surface 14 of the tool is the external face of the upper reinforcement layer 25a, so the substrate 6 is in direct contact with the reinforcement material rather than the mild steel forming the body 5.

[0062] Optionally the upper surface 14 of the tool comprises a coating of graphite which covers the upper reinforcement layer 25a and inhibits diffusion bonding between the substrate 6 and the reinforcement material. So in this case the substrate 6 would by secured by the clamps 7, 8 in direct contact with the graphite coating, rather than in direct contact with the reinforcement material of the upper reinforcement layer 25a.

[0063] The substrate 6 is pre-formed, in other words it is not formed by additive manufacturing on the tool. Typically the substrate 6 is secured to the tool outside the chamber of the additive manufacturing system 1, and then the fixture 15 carrying the substrate 6 is introduced into the chamber and placed on the table 3.

[0064] In a second step, the build head 4 is operated to perform a build process by building a near net shape part 11 on the substrate 6 secured to the tool. The build head 4 feeds metallic feedstock material 9 (such as titanium alloy or aluminium alloy) towards the substrate 6, and the material 9 is melted by a laser beam 10 as it is fed onto the substrate 6. The feedstock material 9 may be fed in the form of a wire or a blown powder, for example. The build head 4 is scanned across the substrate 6 to build a part by forming a series of layers of metallic material on the substrate 6. These layers include a first layer which fuses to the substrate at a part/substrate interface 12, and a series of additional layers each of which fuses with a previously deposited layer. One of these additional layers 13 is shown in the process of being laid down by the build head 4. The shape and size of each layer is determined in accordance with a computer aided design (CAD) model of the part 11 stored in a memory. Although the layers are all identical in FIG. 1 for ease of illustration, they may in general have different shapes and/or sizes.

[0065] The metallic material melts and solidifies during the build process, thereby fusing the part 11 to the substrate 6 and creating thermally induced stress in the part 11. The forces acting on the substrate 6 in the clamped condition during the build process are shown in FIG. 2. These include shear forces 20 at the interface 12 generated by the shrinkage of the metal as it solidifies and fuses to the substrate 6. These shear forces 20 are reacted by upward reaction forces 21 from the tool and downward reaction forces 22 from the clamps. If the clamps 7, 8 were released then the bending moment generated by the shear forces 20 would cause the part 11 and substrate 6 to become distorted as shown in FIG. 3.

[0066] Returning to FIG. 1, after the part 11 has been fully built, the part 11, the substrate 6 and the fixture 15 are lifted off the table 3, removed from the chamber, and moved together to the heat treatment system 2. The substrate 6 remains clamped to the tool and the part 11 remains bonded to the substrate 6 as they are moved.

[0067] The tool 5, 25a, 25b and clamps 7, 8 are as light as possible so they can be manually moved relatively easily between the additive manufacturing system 1 and the heat treatment system 2. Typically a collective weight of the tool 5, 25a, 25b and the clamps 7, 8 is less than ten times the collective weight of the substrate 6 and the part 11. More preferably a collective weight of the tool 5, 25a, 25b and the clamps 7, 8 is less than five times the collective weight of the substrate 6 and the part 11. Most preferably a collective weight of the tool 5, 25a, 25b and the clamps 7, 8 is less than twice the collective weight of the substrate 6 and the part 11.

[0068] Next the heat treatment system 2 is operated to perform a heat treatment process by heating the part 11, the substrate 6 and the fixture 15 together thereby relieving the thermally induced stress in the part, the substrate remaining clamped to the tool during the heat treatment process. The heat treatment system 2 comprises a chamber 30 and heating elements 31 such as electric resistive heaters (or any other kind of heating element). The nature of the heat treatment process depends on a number of factors, principally the material of the part 11specifically the chemical composition of the feedstock material and the desired microstructure and properties of the part. Generally speaking, the heat treatment process involves increasing the temperature to an elevated stress relieving temperature at which at least some of the thermally induced stress in the part 11 is relieved by a process of creep relaxation.

[0069] In one example, in the case where the part 11 and substrate 6 are formed from a titanium alloy such as Ti6Al4V, the heating elements 31 are operated to increase the temperature in the chamber from room temperature up to an elevated stress relieving temperature of about 680 C. over a period of about 90 minutes, the temperature is held at this elevated temperature for about 180 minutes, and then the heating elements 31 are turned off and the temperature returns to room temperature over a period of the order of 90 minutes. In another example, in which the part 11 and substrate 6 are formed from an aluminium alloy, then a lower stress relieving temperature of the order of 320 C. can be used.

[0070] Ideally the maximum bending stress generated in the tool 5, 25a, 25b by the internal stresses in the part 11 is much less than the stress at which the tool 5, 25a, 25b will experience plastic deformation at the heat treatment temperature, so the tool 5, 25a, 25b remains in the linear elastic regime during the heat treatment process.

[0071] The tool 5, 25a, 25b is designed with sectional and material properties such that at the elevated stress relieving temperature the bending stiffness of the tool 5, 25a, 25b is much greater than the bending stiffness of the part 11 (typically at least ten times greater) measured perpendicular to the axis along which deposition takes placein this case the vertical (Z) axis. That is, for each horizontal axis (X,Y): E.sub.f*I.sub.f>>E.sub.p*I.sub.p where E.sub.f is the elastic modulus of the material forming the fixture 15, I.sub.1 is the areal moment of inertia of the fixture 15, E.sub.p is the elastic modulus of the material forming the part 11 and I.sub.p is the areal moment of inertia of the part 11. This ensures that the part 11 is held approximately flat during both the build process and the heat treatment process.

[0072] Note that the fixture 15, the substrate 6 and the part 11 are all heated during the heat treatment process. The tool 5, 25a, 25b and clamps 7, 8 are both formed from a material which is be able to withstand the high temperature of the heat treatment process. Also the thermal mass of the fixture 15 is designed to be relatively low so that the time (and energy) required to heat it up is not too great.

[0073] Typically a thermal mass of the fixture 15 is less than ten times the collective thermal mass of the substrate 6 and the part 11. Preferably a thermal mass of the fixture 15 is less than five times the collective thermal mass of the substrate 6 and the part 11. More preferably a thermal mass of the fixture 15 is less than twice the collective thermal mass of the substrate 6 and the part 11.

[0074] Optionally a thermal mass of the fixture 15 is approximately equal to the collective weight of the substrate 6 and the part 11, in other words: Cp(fix)*m(fix)+Cp(cl)*m(cl) Cp(sub)*m(sub)+Cp(part)*m(part), where Cp(fix) is the specific heat capacity of the tool 5, 25a, 25b; m(fix) is the mass of the tool 5, 25a, 25b; Cp(cl) is the specific heat capacity of the clamps 7, 8; m(cl) is the mass of the clamps 7, 8; Cp(sub) is the specific heat capacity of the substrate 6; m(sub) is the mass of the substrate 6; Cp(part) is the specific heat capacity of the part 11; and m(part) is the mass of the part 11.

[0075] Making the collective thermal masses approximately equal means that the various elements will tend to heat and cool at a similar rate during and immediately after the heat treatment process.

[0076] Alternatively it may be beneficial for the fixture 15 to have a higher thermal mass than the substrate 6 and part 11. The temperature rise of the fixture 15 will lag behind the substrate 6 and part 11, increasing the difference between their respective stiffness and yield strengths.

[0077] The substrate 6 is preferably formed from a material which is dissimilar to the material forming the upper surface 14 of the tool 5, 25a, 25b at the substrate/tool interface where they engage each other thereby inhibiting diffusion bonding between them during the heat treatment process. Similarly the substrate 6 is preferably formed from a material which is dissimilar to the material forming the clamps 7, 8 at the interface where they engage each other thereby inhibiting diffusion bonding between them during the heat treatment process.

[0078] Optionally the substrate 6 is formed from a titanium alloy such as Ti6Al4V, i.e. the same material as the part 11.

[0079] When the tool bends upwards in the same sense as the substrate 6 and part 11 as shown in FIG. 3, the upper reinforcement layer 25a is in compression, the lower reinforcement layer 25b is in tension, and a neutral bending axis 18 is neither in compression nor in tension. By placing the reinforcement layers 25a, 25b as far away as possible from the neutral axis 18, the bending stiffness of the tool is enhanced without adding much thermal mass. Note that the neutral axis 18 is not at the mid-plane of the tool (i.e. the plane half way between the upper and lower reinforcement layers 25a, 25b) but rather it is offset from the mid-plane so it is closer to the upper reinforcement layer 25a. This upward offset of the neutral axis is due to the presence of the substrate 6 and part 11.

[0080] Thermocouple temperature sensors 32, 33, 34 are used to measure the temperature of the lower reinforcement layer 25b, substrate 6 and part 11 respectively during the heat treatment process, and the measured temperatures are used to control the heating elements 31. The sensors 32 and 33 are integrated into the reinforcement layer 25b and clamp 8 respectively. The sensor 33 is thermally insulated from the clamp 8 but pressed into intimate engagement with the substrate 6 by the clamp.

[0081] When the heat treatment process is complete, the fixture 15, substrate 6 and part 11 are removed together from the heat treatment chamber 30. Then the substrate 6 is released from the upper surface of the tool by removing the clamps 7, 8. The heat treatment process reduces the degree of distortion (distance D in FIG. 3) when the clamps 7, 8 are released. Finally the part 11 and the substrate 6 are removed together from the fixture 15, the part 11 remaining bonded to the substrate 6 as they are removed.

[0082] FIGS. 4-6 show an alternative fixture suitable for use in the process of FIG. 1. In this case the fixture has two end clamps 40, 41 each of which is secured to the tool 42, 45a, 45b by four fasteners 40a, 41a; and four central clamps 43 each of which is secured to the tool by a respective fastener 43a. The clamps 40, 41, 43 are tightened by screwing the fasteners 41a, 43a into the tool, and released by removing the fasteners then lifting off the clamps.

[0083] The reinforcement layers 45a, 45b are similar to the reinforcement layers 25a, 25b of the previous embodiment.

[0084] As shown by a comparison of FIG. 4 with FIG. 5, the body 42 of the tool is deep relative to the thickness of the reinforcement layers 45a, 45b, in order to maximise its bending stiffness for a given amount of reinforcement material (noting that the reinforcement material is very expensive so it is not desirable to make the whole tool from this material). More specifically, the upper and lower faces 42a, 42b of the body 42 of the tool are separated by an average depth D of the order of 100 mm, the upper reinforcement layer 45a has an average thickness T.sub.u of about 3-10 mm, and the lower reinforcement layer 45b has an average thickness T.sub.l of about 3-10 mm Thus each reinforcement layer 451, 45b has a thickness which is 3%-10% of the depth D of the body 42 between its upper and lower faces. This maximises the stiffening effect of the reinforcement layers 45a, 45b by spacing them far away from the neutral axis, whilst minimising the amount of expensive reinforcement material required.

[0085] As shown in FIGS. 4 and 6, the mild steel body 42 has a pair of end faces 42c and a pair of side faces 42d. These end faces 42c and side faces 42d are unreinforcedthat is, they are not clad with a reinforcement layer. Optionally the side faces 42d are clad with respective reinforcement layers made of the same reinforcement material as the upper and lower reinforcement layers.

[0086] In the example of FIGS. 4-6 there are a number of clamps distributed around the periphery of the substrate 6, but in a further embodiment (not shown) a single picture frame clamp may be used to clamp the substrate to the tool around its full periphery.

[0087] In a further embodiment shown in FIG. 7, the substrate 6 is replaced by a substrate 6a with pre-formed undersized countersunk holes 50, only one of which is shown in FIG. 7. Rather than being secured to the upper surface of the tool by clamps, the substrate 6a is secured to the tool by a number of screws 51 or other fasteners, each of which passes through a respective hole 50 and is screwed into the tool below it. After the part 11 has been built on the substrate 6a, the screws 50 are released by removing them from their holes 50, and the substrate 6a is removed from the tool. Then the holes 50 are enlarged by drilling out material 52 to form cylindrical holes with parallel sides indicated by dotted lines in FIG. 7.

[0088] In a further embodiment (not shown) bolts come in from the bottom of the fixture and engage in threaded holes in the substrate.

[0089] FIG. 8 illustrates a method of cladding either of the tools described above by a weld coating process. In this example the upper reinforcement layer 42a is shown being formed on the upper face of the body 42 of the tool of FIG. 6, but the same process can be used to form any of the other reinforcement layers 25a, 25b, 42b.

[0090] A welding head 51 deposits a series of lines 50 of molten reinforcement material (for instance Inconel 625 or 718) onto the upper face of the body 42. Each line cools, solidifies and fuses to the upper face of the body, forming a continuous bond between the reinforcement layer and the upper face of the body 42 across the full area of the reinforcement layer. After the entire face has been clad, the reinforcement material is ground back to a desired level indicated by a dashed line 54.

[0091] Alternative methods of forming and/or bonding the reinforcement layers include cold metal spraying, diffusion bonding and linear friction welding. Another possible method is to place the body of the tool in a mould, and pour molten reinforcement material into the mould so that it coats the upper and/or lower faces of the body.

[0092] The material properties of the reinforcement material forming the reinforcement layers 25a, 25b; 42a, 42b are selected to enhance the stiffness and yield strength of the tool at high temperature, and ensure that the tool remains in the linear elastic regime during the heat treatment process.

[0093] Tables 1-5 below show material properties of Ti6Al4V (a preferred material for the substrate 6 and the part 11); mild steel S355J2H (a preferred material for the body 5, 42 of the tool); Inconel 718 (a first reinforcement material); Inconel 625 (a second reinforcement material); and Tungsten (a third reinforcement material).

[0094] In Tables 1-5, temperature is given in C., the coefficient of linear expansion is given in 10.sup.6 K.sup.1, the Young's modulus E is given in Gpa, and the yield strength is given as the stress in MPa at which a permanent deformation of 0.2% of the original dimension will result.

[0095] The parameters in Tables 1-5 may be determined by standard methods. Two ASTM standards that can be used for measuring yield strength and Young's modulus respectively are: ASTM E8/E8MStandard Test Methods for Tension Testing of Metallic Materials; and ASTM E111 Standard Test Method for Young's Modulus, Tangent Modulus and Chord Modulus.

TABLE-US-00001 TABLE 1 Ti6Al4V Linear expansion E Yield Strength 0.2% Temp Coefficient Temp G Pa Temp M Pa 20 to 100 8.6 20 114 0 900 20 to 315 9.2 100 114 100 800 20 to 650 9.7 200 114 200 760 300 85 300 570 400 85 400 500 500 75 500 480 600 42

TABLE-US-00002 TABLE 2 Mild Steel - Structural Steel - S355J2H Linear expansion E Yield Strength 0.2% Temp Coefficient Temp G Pa Temp M Pa 0 to 250 11.7 20 210 20 520 0 to 500 12.8 100 210 100 520 0 to 1000 13.9 200 189 200 485 300 168 300 439 400 147 400 381 500 126 500 255 600 65.1 600 118 700 27.3 700 66

TABLE-US-00003 TABLE 3 Inconel 718 Linear expansion E Yield Strength 0.2% Temp Coefficient Temp G Pa Temp M Pa 21 208 21 200 12.8 93 205 93 1172 400 13.5 204 202 204 1124 600 13.9 316 194 316 1096 800 14.2 427 186 427 1076 1000 14.4 538 179 538 1069 1200 15.1 649 172 649 1027 1400 16 760 162 760 758 871 127

TABLE-US-00004 TABLE 4 Inconel 625 Linear expansion E Yield Strength 0.2% Temp Coefficient Temp G Pa Temp M Pa 21 207.5 21 414 93 12.8 93 204.1 204 13.1 204 197.9 316 13.3 316 191.7 427 13.7 427 185.5 538 14 538 178.6 649 734.3 649 14.8 649 170.3 760 544.7 760 15.3 760 160.6 871 275.8 871 15.8 871 147.5 927 16.2

TABLE-US-00005 TABLE 5 Tungsten Linear expansion E Yield Strength 0.2% Temp Coefficient Temp G Pa Temp M Pa 20 400 20 750 100 4.4 800 370 1200 350 1800 300

[0096] FIGS. 9 and 10 illustrate some of the data of Tables 1-3 graphically.

[0097] It can be seen from FIGS. 9 and 10 that Inconel 718 has a yield strength and Young's modulus which reduces much less (in percentage terms) with temperature than both Ti6Al4V and mild steel. For instance the Young's modulus and yield strength 0.2% reduce by only about 17% and 13% respectively between 93 C. and 649 C.

[0098] It can also be seen from FIGS. 9 and 10 that Inconel 718 has a higher yield strength and Young's modulus than both Ti6Al4V and mild steelparticularly at high temperatures. Note that the Young's modulus of Inconel 718 is about the same as mild steel at room temperature, but the Young's modulus of mild steel drops off quickly with temperature as shown in FIG. 10.

[0099] The Young's modulus at 600 C. of Inconel 718 (about 175 GPa) is greater than the Young's modulus at 600 C. of mild steel (65.1 GPa) by a factor of about 2.7.

[0100] The yield strength 0.2% at 600 C. of Inconel 718 (about 1050 MPa) is greater than the yield strength 0.2% at 600 C. of mild steel (118 MPa) by a factor of about 8.9.

[0101] FIG. 11 shows an alternative tool which is identical to the tool of FIGS. 4-6 except it omits the upper reinforcement layer 45a. So in this case the lower reinforcement layer 45b clads the lower face 42b of the body 42, and the upper face 42a of the body is unreinforcedthat is, it is not clad with a reinforcement layer. The attachment system 40, 41, 43 is configured to releasably secure the substrate 6 to the upper surface 14 of the tool, which in this case is the unreinforced upper face 42a of the body rather than the upper reinforcement layer as in the tool of FIGS. 4-6.

[0102] Optionally the upper surface 14 of the tool of FIG. 11 comprises a coating of graphite which inhibits diffusion bonding between the substrate and the upper surface of the tool. In the case of FIGS. 4-6 such a graphite coating would cover the upper reinforcement layer 25a, and in the case of FIG. 11 it would cover the upper face 42a of the body 42 so the substrate is secured by the clamps in direct contact with the graphite coating, rather than in direct contact with the mild steel of the upper face 42a of the body 42.

[0103] The tool of FIG. 11 takes advantage of the fact that the lower face 42b of the body, being opposite the substrate, is further from the neutral axis than the upper face 42a of the body. So reinforcement material cladding the lower face 42b is more effective in stiffening the tool than reinforcement material cladding the upper face 42a.

[0104] The tool of FIG. 11 has an asymmetrical thermal expansion profile like a bi-metallic strip. That is, the reinforcement layer 45b will have a different thermal expansion coefficient to the mild steel of the body 42, which will result in a bending force being generated as the temperature rises. If the reinforcement material forming the reinforcement layer 45b has a lower thermal expansion coefficient than the mild steel, then this bending force will tend to counteract the bending forces which tend to bend the tool upwards as in FIG. 3. Therefore optionally the reinforcement material forming the reinforcement layer 45b is a low thermal expansion coefficient material which has a thermal expansion coefficient less than that of mild steel, and preferably also less than Ti6Al4V. A suitable low thermal expansion coefficient reinforcement is Tungsten or a Tungsten alloy. As shown in Table 5 above, Tungsten has a thermal expansion coefficient at 100 C. of 4*10.sup.6 K.sup.1 which is less than half that of mild steel (11.7*10.sup.6 K.sup.1) and Ti6Al4V (8.6*10.sup.6 K.sup.1).

[0105] 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.