Patent Application
20210207239
This invention relates to a process for making an article of manufacture from an equiatomic, soft-magnetic, Fe—Co alloy and to a useful article made therefrom.
Equiatomic, soft-magnetic Fe—Co alloys, including the Fe—Co-2V alloy, are known and have been used primarily to make laminated components for the stators and rotors of electric motors and generators. The known Fe—Co alloys provide a combination of soft magnetic properties together with good strength, ductility, and processability. Parts fabricated from these alloys are usually annealed to reduce stresses in the alloy material and to obtain the desired combination of magnetic and mechanical properties. The alloys undergo a transition from the disordered state to an ordered state when heat treated. The disordered phase is characterized by a random distribution of the Fe and Co atoms in the unit cells of the body-centered-cubic (bcc) lattice structure of the alloy. In the ordered phase, the Fe and Co atoms occupy specific locations in the unit cells throughout the crystal lattice structure.
Prior to the post-fabrication annealing heat treatment, the alloy is in the disordered state. However, when the alloy is cooled from the annealing temperature it transforms to the ordered state as it cools through the ordering temperature (TOrder). TOrder is about 730° C. (about 1345° F.) for the soft magnetic Fe—Co alloys to which the present invention applies. The disordered phase of the alloy has a larger coefficient of thermal expansion (CTE) than the ordered phase. Consequently, during the post-fabrication heat treatment parts made from the alloy undergo a net increase in size because of the different CTE's of the two phases. In other words, the alloy grows more during heating than it shrinks during cooling. That phenomenon results in the net increase in the size of a part made from the alloy after the post-fabrication heat treatment.
The net size increase is difficult to account for because the inventor has determined that the net size increase is significantly greater in the rolling direction than in the direction transverse to the rolling direction. Manufacturers of laminated parts made from the Fe—Co soft magnetic alloys have few techniques to account for unsymmetrical net size change of the annealed finished parts. The extent of the net size change is difficult to assess because it is affected by such factors as the complex shapes that may be fabricated, the thermal stresses induced during heat treatment, and the mechanical stresses associated with the fabrication techniques used, such as stamping. Consequently, the net size change is not always uniform or consistent.
There has been an increasing demand for tighter tolerance laminations and parts made from Fe—Co soft magnetic alloys to meet the ever more challenging engineering design criteria for electric motors and generators. In order to meet that demand a need has arisen to be able to limit or control the net size change of parts fabricated from the equiatomic soft-magnetic Fe—Co alloys in order to better meet the tighter tolerance requirements.
The dimension-related problems associated with the manufacturing of parts from the known equiatomic Fe—Co alloys are resolved to a large degree by the process in accordance with the present invention. According to a first aspect of the invention there is provided a process for making an article of manufacture from a soft-magnetic Fe—Co alloy. The process includes a step of providing a substantially flat, elongated length of a soft-magnetic Fe—Co alloy wherein the Fe—Co alloy has a structure that is characterized by consisting essentially of a disordered phase. The process also includes a prefabrication or intermediate annealing step in which the elongated length of the soft-magnetic steel alloy is annealed before it is fabricated into parts. The prefabrication annealing step is carried out at a temperature that is greater than the ordering temperature of the alloy. The process further includes the step of cooling the alloy from the annealing temperature at a rate that is selected to cause substantial transformation of the disordered phase of the soft-magnetic Fe—Co alloy to an ordered phase thereof, whereby the soft-magnetic Fe—Co alloy undergoes a change in size. After the prefabrication annealing step, the elongated length of the alloy is fabricated into an article of manufacture. The article is then a given a post-fabrication annealing heat treatment that is carried out under conditions of atmosphere, temperature, and time selected to obtain a desired combination of magnetic and mechanical properties in the article of manufacture.
In accordance with another aspect of the present invention there is provided an elongated soft magnetic article made of a soft-magnetic Fe—Co alloy. The article is characterized by the alloy having a substantial amount of an ordered phase of said alloy. The article is further characterized by exhibiting a net size change that is substantially symmetrical in magnitude in the longitudinal (rolling) and transverse directions after post-fabrication annealing.
Here and throughout this specification the following definitions apply. The term “Fe—Co alloy” means an alloy having a total Fe+Co content of more than 90 atomic percent and in which the ratio Fe:Co is about 0.33 to about 3. The alloy may include small amounts of additional elements that are added to benefit particularly desired properties and will typically include the usual impurities found in other alloys intended for the same or similar service. The term “percent” or the symbol “%” means percent by weight unless otherwise indicated. The term “disordered” means a crystal lattice structure having unit cells in which the iron and cobalt atoms are randomly arranged. The term “ordered” means a crystal lattice structure having unit cells in which the iron and cobalt atoms occupy specific sites in the crystal lattice unit cell throughout the alloy.
The following detailed description as well as the foregoing summary of the invention will be better understood when read in conjunction with the drawings wherein:
Referring now to
The alloy can be melted by any conventional melting technique, but the alloy is preferably melted by vacuum induction melting (VIM). The molten alloy is cast into one or more ingots and allowed to solidify and cool to room temperature. In step 200 the alloy ingot is preferably hot worked, such as by pressing, cogging, or rolling to billet or bar form, followed by hot rolling to provide an intermediate elongated article such as thick strip, rod, or bar. The intermediate elongated article is cold rolled as in Step 300 to a cross-sectional area and thickness that are selected based on the final form of the parts to be fabricated from the material. Preferably the cold rolled intermediate article is realized as strip material having a thickness and width that are selected for making laminated parts for stators and rotors used in electric motors and generators. The cold rolling step may be performed in one or more reductions.
Prior to the fabrication of the laminated parts, the alloy used to make the cold rolled elongated intermediate article has a lattice structure that consists essentially of a disordered phase as described above. In Step 400, the cold rolled elongated intermediate article is annealed prior to fabrication of part laminations in order to minimize the net size change in the laminations and the parts assembled therefrom that would otherwise occur during post-fabrication annealing of such parts. The pre-fabrication annealing step is carried out under conditions of temperature, time, and atmosphere that promote the transformation of the alloy to the ordered phase. It is only necessary that a substantial portion of the alloy transform to the ordered phase to obtain the benefit of the pre-fabrication annealing step. A substantial portion of the alloy is considered to be transformed to the ordered phase when the degree of ordering achieved is greater than 40% by volume and preferably greater than 50% by volume. More specifically, the pre-fabrication annealing step includes heating the cold rolled intermediate elongated article at a temperature that is greater than the ordering temperature of the Fe—Co alloy. The cold rolled intermediate elongated article is then cooled as indicated in Step 500 at a rate that is sufficient to cause the alloy to transform to the ordered state as the alloy cools down through the ordering temperature from the annealing temperature.
The prefabrication annealing step may be carried out by heating the elongated intermediate form of the alloy at a temperature that is above the temperature at which the ordered phase becomes metastable (e.g., about 600° C.), but not higher than the temperature at which the austenitic phase becomes thermodynamically stable (e.g., about 871° C.). Preferably, the prefabrication annealing step is carried out by heating the elongated intermediate form of the alloy at a temperature that is above the temperature at which the ordered phase becomes stable (e.g., about 700° C.), but not higher than the temperature at which the austenitic phase becomes thermodynamically stable. The elongated intermediate form is preferably strand annealed in a non-oxidizing atmosphere with a feed-through rate sufficient to heat the alloy at the annealing temperature for at least about 1 minute. The elongated intermediate form is preferably cooled in air from the annealing temperature. The non-oxidizing atmosphere is preferably dry hydrogen, i.e., hydrogen gas having a dew point of −40° F. (−40° C.) or lower.
After the intermediate elongated article is cooled to room temperature it can be formed into laminations having a shape that is selected based on the design of the part to be made from the laminations. The laminations may be fabricated by stamping the cold rolled elongated article as indicated in Step 600. The laminations may be formed by other cutting techniques known to those skilled in the art including, but not limited to, laser cutting, electrical discharge machining (EDM), photo etching, and water jet cutting. The laminations are batch annealed as in Step 700 in a protective atmosphere under conditions of temperature and time that are selected to provide a combination of mechanical and magnetic properties sufficient to withstand the high physical stresses that will be encountered in service. For example, the laminated parts may be annealed by heating at a temperature of 1300 to 1600° F. (704 to 871° C.) for 2-4 hours in dry hydrogen. The heated parts are then cooled from the annealing temperature at a rate of 250-) 400 F° (139-222 C° per hour down to about 600° F. (316° C.) after which the parts can be cooled at any rate to room temperature. The protective atmosphere is preferably dry hydrogen. The shaped laminations are then stacked and bonded together to form the magnetic component as indicated in Step 800.
The process according to the present invention provides a significant advantage compared to the known processes for making laminated soft magnetic articles from equiatomic Fe—Co alloys. The intermediate, prefabrication annealing step provides an elongated alloy article having a structure that is characterized by substantial transformation of the disordered phase to the ordered phase of the alloy. When the shaped laminations are subsequently annealed, the net increase in size of the laminations after post-fabrication annealing heat treatment is significantly less than when the prefabrication annealing step is not performed. The inventor has observed that the use of the intermediate annealing step results in about a 63% reduction in size change in the rolling direction and about a 55% reduction in size change in the transverse direction. Furthermore, the inventor has determined that the net size change in the transverse direction is significantly more symmetrical with the net size change in the rolling direction.
The advantage provided by the process according to the present invention is illustrated in
In order to demonstrate the effectiveness of the process according to the present invention comparative testing was performed on samples of HIPERCO® 50 iron-cobalt-vanadium alloy. The HIPERCO 50 alloy has a nominal weight percent composition of 0.01% carbon, 0.05% manganese, 0.05% silicon, 48.75% cobalt, 0.05% niobium, and 1.90% vanadium. The balance of the alloy is iron and usual impurities. The test specimens were prepared from two ingots that were cast after vacuum induction melting and then vacuum arc remelted (VAR) after solidification. The VAR ingots were forged to billet form and then hot rolled to strip form having a first intermediate thickness. The strip from each ingot was annealed, cold rolled to a second intermediate thickness, cold rolled to final thickness, and then cut to a preselected final width.
The strip produced from one ingot was annealed in accordance with the process according to the present invention as described at page 5 above and then cooled to room temperature. The strip produced from the other ingot was not annealed. Two sets of shaped laminations were fabricated by stamping the annealed strip material. The first set of shaped laminations had an inside diameter of 2.680 in. and an outside diameter of 5.4761 in. and the second set of shaped laminations had an inside diameter of 5.51925 in. and an outside diameter of 7.1045 in. An additional two sets of shaped laminations were stamped from the unannealed strip material. The first set of the additional shaped laminations had an inside diameter of 2.680 in. and an outside diameter of 5.4761 in. and the second set of the additional shaped laminations had an inside diameter of 5.51925 in. and an outside diameter of 7.1045 in. The four sets of shaped laminations were batch annealed and then cooled to room temperature in accordance with the usual practice for the HIPERCO 50 alloy and as described generally at page 6 above.
The inside and outside diameters of eleven (11) of the pre-annealed, 5.4761 in. OD, shaped laminations and twelve (12) of the pre-annealed 7.1045 in. OD shaped laminations were measured after fabrication and again after post-fabrication annealing. The inside and outside diameters of nine (9) of the unannealed, shaped laminations were measured after fabrication and again after post-fabrication annealing. The amount of growth realized after the post-fabrication anneal was determined for each part. The measured diameters (I.D. and O.D.) are presented in Tables 1A and 1B below in inches.
The magnitudes of the growth in size of the parts (A) were determined by calculating the differences in the measured I.D.'s and O.D.'s of the sets of parts from the measurements presented in Tables 1A and 1B and are presented in Table 2 below. All values are in inches.
It is clear from the data in Table 2 that the magnitude of the size growth of the ring laminations processed according the present invention is significantly smaller than the magnitude of the size growth of the ring laminations given the standard processing. To emphasize the difference realized from the use of the process of the present invention compared to the standard processing Table 3 below presents the average growth of the parts processed according to the invention as a percentage of the average growth of the standard processing parts.
It is evident from Table 3 that the laminations processed with the method according the present invention had significantly less growth after the final annealing heat treatment than the parts prepared with the standard process.
The terms and expressions which are employed in this specification are used as terms of description and not of limitation. There is no intention in the use of such terms and expressions of excluding any equivalents of the features shown and described or portions thereof. It is recognized that various modifications are possible within the invention described and claimed herein.
This application is a continuation of U.S. patent application Ser. No. 15/789,197, filed Oct. 20, 2017, which claims the benefit of U.S. Provisional Patent Application No. 62/410,926, filed Oct. 21, 2016, the entireties of which are incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| 62410926 | Oct 2016 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 15789197 | Oct 2017 | US |
| Child | 17186975 | US |
