Solid Metallic Component And Method For Producing Same

Abstract

The invention relates in particular to a solid metallic component. This component (1) is particularly notable in that it comprises a core (5) and an external shell (3) which surrounds said core (5) in all directions, this core (5) and this shell (3) being made of different grades of steel, the steel of said core (5) having martensite and bainite critical cooling rates lower than those of the steel or steels of said shell (3).

Claims

1. A solid metal component, which comprises a core and an outer shell which surrounds said core in all directions, said core and shell being made of different grades of steels, the steel of said core exhibiting martensite and bainite critical cooling rates lower than those of the steel or steels of said shell.

2. The component according to claim 1, wherein said core is itself surrounded by at least one inner shell, this inner shell being surrounded by said outer shell, the steel of said core exhibiting martensite and bainite critical cooling rates lower than those of the steel of said inner shell, these rates of said inner shell being themselves lower than those of said outer shell.

3. A method of manufacturing a component according to claim 1, which comprises a step of depositing said steels by additive manufacturing or welding, on a base previously manufactured, in order to form at the same time said core and the remainder of said shell or shells respectively.

4. The method according to claim 3, wherein the steel grade of the remainder of said outer shell is the same as that of said base.

5. The method according to claim 3, wherein the steel grade of the remainder of said outer shell is different from that of said base, these two grades exhibiting martensite and bainite critical cooling rates that are identical or almost identical.

6. The method according to claim 3, wherein said base is made by forging or rolling.

7. The method according to claim 3, wherein said base is made by additive manufacturing or welding.

Description

DESCRIPTION OF FIGURES

[0035] Other characteristics and advantages of the invention will become apparent from the description which will now be given, with reference to the accompanying drawings, which represent, for illustrative but not limitative purposes, various possible embodiments thereof.

[0036] In these drawings:

[0037] FIG. 1 is a schematic view, along a vertical section plane, of a component according to the present invention;

[0038] FIG. 2 is a schematic view illustrating a step in the manufacture of the component of FIG. 1;

[0039] FIG. 3 is a schematic view illustrating the manufacturing process of the component, at a later stage than the one shown in FIG. 2;

[0040] FIG. 4 is a diagram showing the hardness variation of a component according to the invention, at the center thereof, after quenching and tempering, using the materials indicated in Table I to which reference will be made hereafter.

DETAILED DESCRIPTION OF THE INVENTION

[0041] As it will be seen from the following, the present invention is based on a combination of carefully organized materials and a manufacturing process which, after quality treatment, provides high mechanical properties homogeneous throughout the thickness of the component thus generated.

[0042] Throughout the present description, including the claims, the term “component” is understood to mean both a plate, i.e. an object whose thickness is smaller than its length and width, and any other three-dimensional object, for example parallelepipedal or cylindrical, having a thickness greater than its other dimensions.

[0043] According to the invention and as shown in FIG. 1, a disk-shaped solid metal plate 1 is involved.

[0044] It is shown being positioned on a thickness 2 of stainless steel or of an alloy known under the trademark Inconel. Unlike what is shown in FIGS. 2 and 3, this thickness is preferably related to the plate 1, after it has been manufactured.

[0045] When the plate is a steam generator bottom plate (as explained above), the thickness 2 is in contact with the primary water and thus forms a corrosion barrier for the remainder of the plate 1.

[0046] This plate 1 comprises a core 5 and an outer shell 3 which surrounds said core 5 in all directions. This core 5 and this shell 3 are made of different grades of steels.

[0047] More precisely, in the example shown here, the core 5 is itself surrounded by an inner shell 4, this inner shell 4 being surrounded by said outer shell 3.

[0048] An embodiment not shown could involve a single outer shell 3 in direct contact with the core or, on the contrary, more than two shells.

[0049] In any event and according to the invention, the steel grades of the core 5 and of each shell 3 and 4 are different, and the steel of said core 5 has martensite and bainite critical cooling rates lower than those of the steel of the shell 4 which surrounds it, and so on for each shell that surrounds the previous shell.

[0050] Thus, in the case of FIG. 1, said rates of the inner shell 4 are lower than those of the outer shell 3.

[0051] This plate 1 can be manufactured according to the method statement detailed below.

[0052] First, a heavy plate or base 30 with a typical thickness generally between 10 to 15 cm is forged or rolled. Such thicknesses ensure a very good metallurgical quality without macro-segregation. Optionally, this plate 30 can be manufactured according to the same method statement as the one which will be described below.

[0053] The remainder of the plate 1 is said to be “deposited”, and is obtained by additive manufacturing or welding. This means that the entire thickness of the plate 1 is gradually increased.

[0054] If one refers to FIG. 2, this means that after having formed the base 30, not only the lower part of the shell 4, but also the side wall 31 of the shell 3 (the latter being formed at the end of the gathering of the base 30 and the side wall 31), are built simultaneously thereon.

[0055] This operation is preferably carried out by means of one of the following methods or a combination thereof: [0056] Gas Metal Arc Welding (GMAW) or Metal Inert Gas/Active inert Gas (MIG/MAG); [0057] Submerged Arc Welding (SAW) or submerged arc welding with solid flux (“ASF”) or else wire or strip under flux; [0058] Electroslag Welding (ESW) or vertical slag welding.

[0059] In these deposition methods, the encompassed variations are preferably the following metal buildups which have in common high deposition rates (kg/h): [0060] tandem (two wires or strips with their own power supply); [0061] multi-wire (several wires with their own power supply); [0062] twinned (2 wires or strips on the same power supply); [0063] co-buildup without power supply; [0064] combinations of the above techniques; [0065] hot (i.e. preheated) metal buildups.

[0066] The buildup materials are preferably chosen with an equivalent carbon less than 0.65%, typically 0.62%, and exhibit very low diffusible hydrogen levels, in order to prevent from cold cracking, with preheating temperatures as low as possible.

[0067] The fluxes used in the SAW and ESW methods will preferably be basic fluxes which allow better properties of the molten zones.

[0068] The concept of choice of steel grades with regard to the dimensions and the possibilities of thermal treatment of the plate is to select grades that are more “hardenable” (i.e. suitable for being hardened) when approaching the center of the final component.

[0069] The hardenability gradient thus generated is intended to compensate the decrease in the cooling rate during the quenching between the shell and the core.

[0070] To that end, the final properties after quenching and tempering, obtained for various chemical analysis and local cooling rates, are considered. Metallurgical transformation models associated with an estimate of local cooling rates can be usefully employed to achieve this in a predictive manner.

[0071] Regarding the tube plates of current steam generators, the grades will preferably be chosen as follows: [0072] The grade of the base 30 is ideally “18 MND 5”, according to the current specification, but in a version optimized for a thermal treatment. Its typical analysis in mass percentage is C 0.2, Mn 1.3, Mo 0.5, Ni 0.65. [0073] The grades of the metals deposited to constitute the remainder of plate 1 must present martensite and bainite critical cooling rates lower than those of the further outward previous layer, in order to maintain an overwhelmingly bainitic microstructure with perlite ferrite contents as small as possible (<10%) without exceeding 0.65% in carbon equivalent.

Example

[0074] An example based on commercial products is shown in Table 1 below (referred to as “Table 1”, including typical chemical analysis, equivalent carbon values, as well as martensite (VcM) and bainite (VcB) critical cooling rates.

[0075] These latter values should be compared with the low cooling rates obtained due to the very high thickness of the plate: Cooling rate at 700° C. Vr700 (K/h)=5400, 3300, 1700, 770, 475 respectively at 0, 5, 12, 20, 25 cm depth.

TABLE-US-00001 TABLE 1 Analysis (%) C* VcM VcB Layer C Si Mn Ni Cr Mo (%) (K/h) (K/h) Base 30 0.18 0.22 1.52 0.64 0.18 0.52 0.62 93000 4100 Inner shell 4 0.09 0.60 1.70 1.50 0.20 0.50 0.61 54000 1510 Core 5 0.07 0.30 1.50 2.00 0.25 0.58 0.62 49000 920 Part 31 of 0.08 0.60 1.70 1.50 0.20 0.50 0.62 60000 1650 shell 3

[0076] FIG. 3 presents hardness results calculated through the plate, in the center thereof, after quenching in water from 865° C., then tempering at 635° C., using the grades shown in Table 1.

[0077] The segments visible in the figure bear the numerical reference of the part of the plate 1 to which they relate.

[0078] It can be seen that the hardness is extremely homogeneous.

[0079] Moreover, the perlite ferrite contents remain below 10% in all the deposited metal, which indirectly indicates that resilience and toughness for these C—Mn—Ni steels will be high.

[0080] Indeed, if the real quality criterion of the microstructure is the relative quantity of bainite and martensite, emphasis is also placed on the quantity of ferrite and perlite. A microstructure exhibiting good mechanical properties preferably contains more than 90% bainite+martensite and therefore less than 10% ferrite+perlite.

[0081] Consequently, the transformation rate leading precisely to 10% of ferrite+perlite (abbreviated “V10FP” (in K/h)) is also significant.

[0082] The above Table could thus be completed as follows: [0083] for base 30: V10FP=1900; [0084] for inner shell 4: V10FP=590; [0085] for core 5: V10FP=335; [0086] for part 31 of shell 3: V10FP=640.

[0087] In the example described above, three to four different chemical compositions are used. It can adequately be declined in only two different grades. In these alternatives, it is appropriate to comply with the increasing hardenability evolution of the shells towards the core.

[0088] As the geometry of the plate 1 is circular, the deposits are easily but not necessarily made with welding heads that are movable only radially and weld circumferentially.

[0089] This avoids the more expensive use of a robot having the dimensions of this manufacturing.

[0090] Several welding heads can usefully be used simultaneously or sequentially, for example to make the external and internal passes, or merely to reduce the manufacturing time.

[0091] Temperature control devices are advantageously used in order to guarantee the preheating (greater than 150° C.), inter-pass and post-welding (greater than 250° C. for 24 h) temperatures.

[0092] For a better manufacturing strategy, this can be done as follows:

[0093] a) It is useful but not mandatory to start with the wrought base which will be clamped before welding on a turning device.

[0094] b) A peripheral strip can be used to limit the thicknesses to be machined after welding.

[0095] c) The construction is done additively, layer by layer, from the lower face to the upper face.

[0096] d) Intermediate thermal treatments can be carried out in order to limit deformations and residual stresses (stress relieving treatment above 550° C.), limit the risks due to hydrogen (precautionary treatment), and restore the properties of the underlying material.

[0097] e) Intermediate forging operations can be performed to further improve the final properties. Likewise, a final forging can easily be carried out.

[0098] f) Stress relieving treatment/first austenitization/air cooling.

[0099] g) Blank type machining.

[0100] h) Quality treatment with austenitization at low temperature (AC3+40° C.), water quenching, tempering according to the grades used (in the example given above: around 635° C.). AC3 is the conventional designation for the end of alpha/gamma transformation on heating.

[0101] The method according to the invention allows for the following advantages:

[0102] Main Benefits [0103] Removal of macro-segregations. [0104] Homogeneity of mechanical properties throughout the thickness of the plate. [0105] Better overall mechanical properties, in particular excellent resistance/toughness balance.

[0106] Side Benefits [0107] Great freedom of choice of supplier who no longer needs to have a very large ingot casting capacity. [0108] Potentially shortened overall manufacturing time. [0109] Possibility of local repair during manufacture. [0110] Possibility of intermediate thermal treatments. [0111] Possibility of intermediate and final forgings. [0112] Installation more economical than a large forge.

[0113] The users of such a technique are potentially steam generator manufacturers, blacksmiths of solid components, boilermakers, blacksmiths, welding equipment and products manufacturers.