Systems and methods for tailoring coefficients of thermal expansion between extreme positive and extreme negative values
US-10557182-B2 · Feb 11, 2020 · US
US11643698B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11643698-B2 |
| Application number | US-202017026880-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 21, 2020 |
| Priority date | Jun 14, 2013 |
| Publication date | May 9, 2023 |
| Grant date | May 9, 2023 |
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A controlled thermal coefficient product manufacturing system and method is disclosed. The disclosed product relates to the manufacture of metallic material product (MMP) having a thermal expansion coefficient (TEC) in a predetermined range. The disclosed system and method provides for a first material deformation (FMD) of the MMP that comprises at least some of a first material phase (FMP) wherein the FMP comprises martensite randomly oriented and a first thermal expansion coefficient (FTC). In response to the FMD at least some of the FMP is oriented in at least one predetermined orientation. Subsequent to deformation, the MMP comprises a second thermal expansion coefficient (STC) that is within a predetermined range and wherein the thermal expansion of the MMP is in at least one predetermined direction. The MMP may be comprised of a second material phase (SMP) that may or may not transform to the FMP in response to the FMD.
Opening claim text (preview).
What is claimed is: 1. A controlled thermal coefficient product manufacturing method comprising: (1) plastically deforming a metallic material; and (2) texturing said metallic material in at least one selected material direction in response to said plastic deforming; wherein: said metallic material comprises a material selected from a group consisting of: (1) a material characterized by a general formula Fe 100-A-B Mn A X B , wherein X is at least one of Ga, Ni, Co, Al, Ta, Si, or combinations thereof, and A is in a range from 0 to 50 atomic percent composition, and B is in a range from 0 to 50 atomic percent composition such that A plus B is less than 100; (2) a material characterized by a general formula Fe 100-A-B Ni A X B , wherein X is at least one of Ga, Mn, Co, Al, Ta, Si, or combinations thereof, and A is in a range from 0 to 50 atomic percent composition, and B is in a range from 0 to 50 atomic percent composition such that A plus B is less than 100; (3) a material characterized by a general formula Fe 100-A-B-c Ni A CO B Al c X D , wherein X is at least one of Ti, Ta, Nb, Cr, W or combinations thereof, and A is in a range from 0 to 50 atomic percent composition, B is in a range from 0 to 50 atomic percent composition, C is in a range from 0 to 50 atomic percent composition, and D is in a range from 0 to 50 atomic percent composition such that such that A plus B plus C plus D is less than 100; and (4) a material characterized by a general formula Fe 100-A-B-c Ni A Co B Ti c X D , wherein X is at least one of Al, Ta, Nb, Cr, W or combinations thereof, and A is in a range from 0 to 50 atomic percent composition, B is in a range from 0 to 50 atomic percent composition, C is in a range from 0 to 50 atomic percent composition, and D is in a range from 0 to 50 atomic percent composition such that such that A plus B plus C plus D is less than 100; said metallic material prior to said plastic deformation and said texturing comprises a martensitic phase exhibiting different thermal expansion coefficients in different crystallographic directions; said texturing comprises texturing of said martensitic phase; said metallic material exhibits a first bulk thermal expansion characteristic having a first thermal expansion coefficient prior to said plastic deformation; said metallic material, subsequent to said plastic deformation, exhibits a second bulk thermal expansion characteristic having a second thermal expansion coefficient; said second thermal expansion coefficient is within a selected range; and said second bulk thermal expansion characteristic is in said at least one selected material direction due to said texturing of said martensitic phase. 2. The controlled thermal coefficient product manufacturing method of claim 1 wherein said plastic deforming is achieved by at least one of: (1) hot-rolling; (2) cold-rolling; (3) plain strain compression; (4) bi-axial tension; (5) conform processing; (6) bending; (7) drawing; (8) wire-drawing; (9) swaging; (10) extrusion; (11) equal channel angular extrusion; (12) precipitation heat treatment under stress; (13) annealing; (14) sintering; (15) monotonic tension processing; (16) monotonic compression processing; (17) monotonic torsion processing; (18) cyclic thermal training under stress; and (19) combinations thereof. 3. The controlled thermal coefficient product manufacturing method of claim 1 wherein said selected range of said second thermal expansion coefficient ranges from −150×10 −6 K −1 to +500×10 −6 K −1 . 4. The controlled thermal coefficient product manufacturing method of claim 1 wherein said plastic deforming of said metallic material further comprises texturing said metallic material in a direction comprising at least one of a [111], a [100], or a [001] direction.
Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment (hardening articles or materials formed by forging or rolling with no further heating beyond that required for the formation C21D1/02) · CPC title
Deep-drawing (special deep-drawing arrangements in, or in connection with, presses B21D24/00) · CPC title
Processes combined with methods covered by groups B21D1/00 - B21D31/00 · CPC title
comprising lenses · CPC title
of copper or alloys based thereon · CPC title
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