US20140212324A1 - Fine crystallite high-function metal alloy member and method for manufacturing same - Google Patents
Fine crystallite high-function metal alloy member and method for manufacturing same Download PDFInfo
- Publication number
- US20140212324A1 US20140212324A1 US14/124,212 US201214124212A US2014212324A1 US 20140212324 A1 US20140212324 A1 US 20140212324A1 US 201214124212 A US201214124212 A US 201214124212A US 2014212324 A1 US2014212324 A1 US 2014212324A1
- Authority
- US
- United States
- Prior art keywords
- metal alloy
- gadolinium
- alloy
- cast
- fine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 229910001092 metal group alloy Inorganic materials 0.000 title claims abstract description 130
- 238000000034 method Methods 0.000 title claims abstract description 66
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 19
- 239000013078 crystal Substances 0.000 claims abstract description 16
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 129
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 129
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 claims description 69
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 69
- 239000000463 material Substances 0.000 claims description 53
- 239000010949 copper Substances 0.000 claims description 52
- 230000032683 aging Effects 0.000 claims description 43
- 239000011777 magnesium Substances 0.000 claims description 36
- 239000010931 gold Substances 0.000 claims description 34
- 239000010936 titanium Substances 0.000 claims description 33
- 238000010438 heat treatment Methods 0.000 claims description 30
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 26
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 26
- 229910052802 copper Inorganic materials 0.000 claims description 26
- 229910052709 silver Inorganic materials 0.000 claims description 26
- 239000004332 silver Substances 0.000 claims description 26
- 229910052782 aluminium Inorganic materials 0.000 claims description 25
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 25
- 229910052763 palladium Inorganic materials 0.000 claims description 23
- 229910052697 platinum Inorganic materials 0.000 claims description 23
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 22
- 238000001816 cooling Methods 0.000 claims description 19
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 18
- 229910052749 magnesium Inorganic materials 0.000 claims description 18
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 17
- 229910052737 gold Inorganic materials 0.000 claims description 17
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 16
- 229910052719 titanium Inorganic materials 0.000 claims description 16
- 238000000465 moulding Methods 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 7
- 239000002184 metal Substances 0.000 claims description 7
- 239000012776 electronic material Substances 0.000 claims description 2
- 239000010929 jewellery material Substances 0.000 claims 1
- 239000000956 alloy Substances 0.000 abstract description 127
- 229910045601 alloy Inorganic materials 0.000 abstract description 108
- 230000002708 enhancing effect Effects 0.000 abstract description 3
- 239000000203 mixture Substances 0.000 description 56
- 230000000694 effects Effects 0.000 description 50
- 230000001965 increasing effect Effects 0.000 description 31
- 230000006866 deterioration Effects 0.000 description 19
- 238000011156 evaluation Methods 0.000 description 19
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 18
- 238000002441 X-ray diffraction Methods 0.000 description 10
- 238000003672 processing method Methods 0.000 description 9
- 239000010409 thin film Substances 0.000 description 9
- 239000000843 powder Substances 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 6
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 5
- 229910052784 alkaline earth metal Inorganic materials 0.000 description 5
- 150000001342 alkaline earth metals Chemical class 0.000 description 5
- 229910052738 indium Inorganic materials 0.000 description 5
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 5
- 229910000923 precious metal alloy Inorganic materials 0.000 description 5
- 229910052761 rare earth metal Inorganic materials 0.000 description 5
- 150000002910 rare earth metals Chemical class 0.000 description 5
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 description 5
- 239000000126 substance Substances 0.000 description 5
- 229910001020 Au alloy Inorganic materials 0.000 description 4
- 239000000654 additive Substances 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 239000003353 gold alloy Substances 0.000 description 4
- 239000011572 manganese Substances 0.000 description 4
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 239000010408 film Substances 0.000 description 3
- 229910052733 gallium Inorganic materials 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- JBQYATWDVHIOAR-UHFFFAOYSA-N tellanylidenegermanium Chemical compound [Te]=[Ge] JBQYATWDVHIOAR-UHFFFAOYSA-N 0.000 description 3
- 230000001988 toxicity Effects 0.000 description 3
- 231100000419 toxicity Toxicity 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000002542 deteriorative effect Effects 0.000 description 2
- 238000002845 discoloration Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000010970 precious metal Substances 0.000 description 2
- 239000010948 rhodium Substances 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 229910001260 Pt alloy Inorganic materials 0.000 description 1
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- IYRDVAUFQZOLSB-UHFFFAOYSA-N copper iron Chemical compound [Fe].[Cu] IYRDVAUFQZOLSB-UHFFFAOYSA-N 0.000 description 1
- IUYOGGFTLHZHEG-UHFFFAOYSA-N copper titanium Chemical compound [Ti].[Cu] IUYOGGFTLHZHEG-UHFFFAOYSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 229910052741 iridium Inorganic materials 0.000 description 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 1
- 229910052762 osmium Inorganic materials 0.000 description 1
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052707 ruthenium Inorganic materials 0.000 description 1
- 238000005987 sulfurization reaction Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 230000035899 viability Effects 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D25/00—Special casting characterised by the nature of the product
- B22D25/06—Special casting characterised by the nature of the product by its physical properties
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D5/00—Heat treatments of cast-iron
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/001—Heat treatment of ferrous alloys containing Ni
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/02—Alloys based on gold
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/04—Alloys based on a platinum group metal
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/06—Alloys based on silver
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/06—Alloys based on silver
- C22C5/08—Alloys based on silver with copper as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/04—Alloys based on copper with zinc as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/14—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of noble metals or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
-
- A—HUMAN NECESSITIES
- A44—HABERDASHERY; JEWELLERY
- A44C—PERSONAL ADORNMENTS, e.g. JEWELLERY; COINS
- A44C27/00—Making jewellery or other personal adornments
- A44C27/001—Materials for manufacturing jewellery
- A44C27/002—Metallic materials
- A44C27/003—Metallic alloys
Definitions
- the present invention relates to a high-performance elastic limit metal alloy member and a method for manufacturing the same, in which the said alloy member is suitable for an electronic member, a car and an aerial member, a physicochemical member, a medical care member, a jewelry member, a musical instrument members, a tableware member, a structural member, and the like.
- gold (Au), platinum (Pt), silver (Ag), copper (Cu), iron (Fe), aluminum (Al), magnesium (Mg), titanium (Ti), and the like have been known as a metal material; and they have been used in many fields.
- the present invention is characterized in providing fine crystallite high-function alloy of a metal and a precious metal which are novel modified metal alloys with free of toxicity, not only having improved various characteristics but also being capable of adjusting these characteristics without losing the superior characteristics of a metal alloy and a precious metal alloy.
- the present invention is characterized in providing, by adjusting the fine crystallite, a fine crystallite high-function metal alloy having strength, Young's modulus, elongation, heat resistance, corrosion resistance, and spring property, wherein sustainability thereof and so forth may be controlled easily while having easy processability and good workability.
- the present invention provides a fine crystallite high-function metal alloy member and a method for manufacturing the same, in which the said alloy member has enhanced functional characteristics whereby enhancing sustainability and processability with easy operation and no uselessness, while keeping or enhancing hardness, tensile strength, Young's modulus, elongation, corrosion resistance, discoloration, high-temperature characteristics, and workability.
- An object of the present invention is to solve and remedy these problematic properties for betterment while keeping the above-mentioned characteristics of the metal materials thereby obtaining a novel fine crystallite high-function metal alloy member that has been wanted.
- a novel fine crystallite high-function metal alloy member having superior characteristics including physical, electrical, mechanical, and chemical characteristics, and also having excellent performance, quality, function, processability, workability, and so on, could be obtained by making the crystallite fine (to the size of 10 ⁇ 9 m to 10 ⁇ 3 m) and by controlling the size and the form thereof; and based on this finding, a method for manufacturing the same could be established.
- the fine crystallite metal alloy member of the present invention is characterized in that by controlling the size and the form of a newly developed fine crystallite, not only various characteristics of existing metal alloys such as hardness, tensile strength, elongation, Young's modulus, resisting force, softening property, electrical conductivity, thermal conductivity, processability, and workability may be kept or enhanced, but also these various characteristics may be controlled, so that unnecessity in function, performance, quality, process, operation, and so forth may be cut away.
- the fine crystallite metal alloy of the present invention 90% or more thereof may be processed without annealing. This alloy shows characteristics including not causing cracks even if the rolling direction is changed.
- This metal alloy is easy to be processed and is not easily deformed, while having sustainability; and thus, this is suitable for the purpose to reduce the size and weight upon commercialization thereof.
- the fine crystallite high-function alloy of a metal and a precious metal in the present invention has superior characteristics as to hardness, tensile strength, Young's modulus, resisting force, elastic limit, elongation, spring property, and so forth; and in addition, this can be processed easily with good workability.
- This is highly pure, a crystallite thereof is fine, and the volume-occupation rate of an added element is small; and thus, an electronic material having high electrical conductivity and thermal conductivity may be obtained.
- These characteristics can be enhanced without deteriorating Young's modulus, so that a covering range of its commercial deployment is wide. When this is used to make a musical instrument, a creative tone and an acoustic effect may be obtained.
- the spring property can be enhanced, a wire rod and a plate material having flexibility and toughness can be obtained. Because heat resistance can be enhanced, its application is wide. A material having superior physical, mechanical, electrical, and chemical characteristics can be obtained.
- the characteristics that various properties can be enhanced without substantial deterioration of electrical conductivity and Young's modulus were found and established.
- the fine crystallite high-function metal alloy of the present invention similar high function characteristics can be obtained also in thin films of a spatter film, a vapor-deposited film, and a plated film, because the crystallite is in the size of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) or the size of micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the present invention was made in view of the needs from the market as mentioned above; and an object thereof is to provide a fine crystallite high-function metal alloy member and a method for manufacturing the same, in which the said metal alloy keeps, enhances, and adjusts mechanical, physical, and chemical properties while having desired function, performance, and quality, with good workability and free of toxicity.
- the present invention has objects to provide: a fine crystallite high-function metal alloy member having also excellent corrosion resistance and discoloration resistance and a method for manufacturing this; and a fine crystallite metal alloy member having excellent various properties not only at normal temperature but also at high temperature and a method for manufacturing this.
- FIG. 1 is a diagrammatic representation of FIG. 1 :
- Gadolinium Gadolinium
- crystallite size could be adjusted by a cast molding method, a processing method, and a heat-treatment method.
- the size thereof could be adjusted in the range of 10 ⁇ 9 m to 10 ⁇ 3 m, and in addition, the texture form thereof could be adjusted.
- crystal lattice thereof was a face-centered cubic lattice, a body-centered cubic lattice, or a close-packed hexagonal lattice
- size of the crystallite could be made fine, and the texture form thereof could be adjusted.
- FIG. 2
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a gold (Au) alloy including a high-purity gold (Au) alloy.
- the fine crystallite high-function gold (Au) alloy member according to the first embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of gold (Au) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- Gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of gold (Au) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- Gadolinium Gadolinium
- Au gold
- Ag silver
- gadolinium (Gd) was added to a gold (Au) alloy comprising 50% by weight of gold (Au) and 50% by weight of silver (Ag), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was heat-treated, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a gold alloy comprising 10% by weight of gold (Au) and 90% by weight of silver (Ag), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 27 nm, 15 nm, 19 nm, and 23 nm, respectively.
- the crystallite size thereof could be newly adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the solution treatment may be done in the temperature range of 500 to 2700° C.
- the ageing treatment may be done in the temperature range of 100 to 700° C.
- especially preferable production conditions are the temperature range of 600 to 1000° C. for the solution treatment, and the temperature range of 150 to 550° C. for the ageing treatment.
- the addition effect appears from 5 ppm, and the characteristics thereof decreases when the content thereof is 30000 ppm or more.
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a silver (Ag) alloy including a high-purity silver (Ag) alloy.
- the fine crystallite high-function silver (Ag) alloy member according to the second embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of silver (Ag) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a silver (Ag) alloy comprising 90% by weight of silver (Ag) and 10% by weight of palladium (Pd), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a silver (Ag) alloy comprising 50% by weight of silver (Ag) and 50% by weight of palladium (Pd), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was heat-treated, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a silver (Ag) alloy comprising 10% by weight of silver (Ag) and 90% by weight of palladium (Pd), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 8 nm, 19 nm, 23 nm, and 25 nm, respectively.
- the crystallite size could be newly adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the solution treatment may be done in the temperature range of 450 to 2200° C.
- the ageing treatment may be done in the temperature range of 100 to 600° C.
- Especially preferable conditions are the temperature range of 500 to 1550° C. for the solution treatment, and the temperature range of 150 to 500° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gd gadolinium
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a platinum (Pt) alloy including a high-purity platinum (Pt) alloy.
- the fine crystallite high-function platinum (Pt) alloy according to the third embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of platinum (Pt) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a platinum (Pt) alloy comprising 90% by weight of platinum (Pt) and 10% by weight of palladium (Pd), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a platinum (Pt) alloy comprising 50% by weight of platinum (Pt) and 50% by weight of copper (Cu), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was heat-treated, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a platinum (Pt) alloy comprising 10% by weight of platinum (Pt) and 90% by weight of copper (Cu), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 11 nm, 19 nm, 17 nm, and 22 nm, respectively.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- This comprises a precious metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a platinum (Pt) alloy including a high-purity platinum (Pt) alloy.
- the solution treatment may be done in the temperature range of 600 to 2800° C.
- the ageing treatment may be done in the temperature range of 150 to 1400° C.
- Especially preferable conditions are the temperature range of 500 to 1600° C. for the solution treatment, and the temperature range of 150 to 1000° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gd gadolinium
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a palladium (Pd) alloy including a high-purity palladium (Pd) alloy.
- the fine crystallite high-function palladium (Pd) alloy member according to the fourth embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of palladium (Pd) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plate having the thickness of 0.3 mm was analyzed by the X-ray analysis; and the average crystallite diameter obtained by the Scherrer's equation was 15 nm.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the metal alloy member comprises a precious metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a palladium (Pd) alloy including a palladium (Pd) alloy.
- the solution treatment may be done in the temperature range of 500 to 2700° C.
- the ageing treatment may be done in the temperature range of 150 to 1300° C.
- Especially preferable conditions are the temperature range of 550 to 1500° C. for the solution treatment, and the temperature range of 150 to 900° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gd gadolinium
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in an aluminum (Al) alloy including a high-purity aluminum (Al) alloy.
- the fine crystallite high-function aluminum (Al) alloy member according to the fifth embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of aluminum (Al) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to an aluminum (Al) alloy comprising 90% by weight of aluminum (Al) and 10% by weight of magnesium (Mg), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to an aluminum (Al) alloy comprising 50% by weight of aluminum (Al) and 50% by weight of magnesium (Mg), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was heat-treated, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to an aluminum (Al) alloy comprising 10% by weight of aluminum (Al) and 90% by weight of magnesium (Mg), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 6 nm, 13 nm, 27 nm, and 19 nm, respectively.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 8 nm, 13 nm, 27 nm, and 19 nm, respectively.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the aluminum (Al) alloy member comprises the aluminum (Al) alloy containing 5 to 30000 ppm of gadolinium (Gd).
- the solution treatment may be done in the temperature range of 300 to 2000° C.
- the ageing treatment may be done in the temperature range of 50 to 450° C.
- Especially preferable conditions are the temperature range of 500 to 1600° C. for the solution treatment, and the temperature range of 50 to 400° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gadolinium (Gd) the member having high function and sustainability, capable of being readily processed, could be obtained.
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a magnesium (Mg) alloy including a high-purity magnesium (Mg) alloy.
- the fine crystallite high-function magnesium (Mg) alloy member according to the sixth embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of magnesium (Mg) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plate having the thickness of 0.3 mm was analyzed by the X-ray analysis; and the average crystallite diameter obtained by the Scherrer's equation was 12 nm.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the fine crystallite high-function magnesium alloy comprises the magnesium (Mg) bare metal containing 5 to 30000 ppm of gadolinium (Gd) or the magnesium (Mg) alloy containing the same.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the solution treatment may be done in the temperature range of 250 to 1050° C.
- the ageing treatment may be done in the temperature range of 110 to 500° C.
- Especially preferable conditions are the temperature range of 500 to 1000° C. for the solution treatment, and the temperature range of 50 to 450° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gadolinium (Gd) the member having high function and durability, capable of being readily processed, could be obtained.
- Gd gadolinium
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a copper (Cu) alloy including a high-purity copper (Cu) alloy.
- the fine crystallite high-function copper (Cu) alloy member according to the seventh embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of copper (Cu) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a copper (Cu) alloy comprising 90% by weight of copper (Cu) and 10% by weight of zinc (Zn), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a copper (Cu) alloy comprising 65% by weight of copper (Cu) and 35 by weight of zinc (Zn), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was heat-treated, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a copper (Cu) alloy comprising 10% by weight of copper (Cu) and 90% by weight of silver (Ag), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 17 nm, 7 nm, 21 nm, and 13 nm, respectively.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the solution treatment may be done in the temperature range of 600 to 2500° C.
- the ageing treatment may be done in the temperature range of 150 to 850° C.
- Especially preferable conditions are the temperature range of 600 to 1600° C. for the solution treatment, and the temperature range of 150 to 780° C. for the ageing treatment.
- Gadolinium (Gd) the member having high function and durability, capable of being readily processed, could be obtained.
- Gd gadolinium
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in an iron (Fe) alloy including a high-purity iron (Fe) alloy.
- the fine crystallite high-function iron (Fe) alloy member according to the eighth embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of iron (Fe) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) 500 g was added to an iron (Fe) alloy comprising 99% by weight of iron (Fe) and 1% by weight of silicon Si, and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) 500 g was added to an iron (Fe) alloy comprising 75% by weight of iron (Fe), 17% by weight of nickel Ni, and 8% by weight of aluminum (Al), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was heat-treated, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 7 nm, 27 nm, and 18 nm, respectively.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the solution treatment was done at 820° C. for 1 hour; and the ageing treatment was done at 480° C. for 3 hours.
- the solution treatment may be done in the temperature range of 600 to 2800° C.
- the ageing treatment may be done in the temperature range of 150 to 700° C.
- Especially preferable conditions are the temperature range of 600 to 2000° C. for the solution treatment, and the temperature range of 150 to 700° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gadolinium (Gd) the member having high function and durability, capable of being readily processed, could be obtained.
- Gd gadolinium
- rare earth metals other than gadolinium (Gd) alkaline earth metals, silicon (Si), boron (B), zirconium (Zr), tin (Sn), indium (In), lead (Pb), nickel (Ni), manganese (Mn), copper (Cu), vanadium (V), phosphorous (P), and
- a fine crystallite high-function metal alloy member comprises a metal alloy containing 5 to 30000 ppm of gadolinium (Gd) in a titanium (Ti) alloy including a high-purity titanium (Ti) alloy.
- the fine crystallite high-function titanium (Ti) alloy member according to the ninth embodiment of the present invention was obtained as following: gadolinium (Gd) was added to a metal alloy containing 99.95% by weight of titanium (Ti) so that the resultant metal alloy has gadolinium (Gd) content of 500 ppm and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- gadolinium (Gd) was added to a titanium (Ti) alloy comprising 99.8% by weight of titanium (Ti) and 0.2% by weight of palladium (Pd), and then, the mixture thereof was cast-molded to a thick plate having the widths of 30 mm and 10 mm; and then, this plate was solution-treated, aged, and then roll-processed to a thick plate having the thickness of 0.3 mm.
- the foregoing finishing-processed thick plates having the thickness of 0.3 mm were analyzed by the X-ray analysis; and the average crystallite diameters obtained by the Scherrer's equation were 7 nm, and 27 nm, respectively.
- the crystallite size could be adjusted in the level of nanometers (10 ⁇ 9 m to 10 ⁇ 6 m) and micrometers (10 ⁇ 6 m to 10 ⁇ 3 m).
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and further, if necessary, an ageing treatment is conducted thereafter at a prescribed temperature.
- the alloy material with the afore-mentioned composition is cast-molded, then, if necessary, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, and then the material is processed to a prescribed form, wherein if necessary, the material is aged before or after this process.
- the solution treatment may be done in the temperature range of 600 to 2700° C.
- the ageing treatment may be done in the temperature range of 150 to 500° C.
- Especially preferable conditions are the temperature range of 500 to 1550° C. for the solution treatment, and the temperature range of 300 to 800° C. for the ageing treatment. Processing efficiency during the time of processing is arbitrary, while the preferable range thereof is the same as that of the first embodiment.
- Gd gadolinium
- rare earth metals other than gadolinium (Gd), alkaline earth metals, silicon (Si), boron (B), aluminum (Al), iron (Fe), zirconium (Zr), copper (Cu), tin Sn, indium (In), nickel (Ni), cobalt (Co), vanadium (V), and chromium (Cr)
- the metal alloys used in the embodiments are not particularly restricted. Any ingredient other than the above-mentioned function-enhancing additives may be used without specific restrictions provided that it is used in a usual metal alloy.
- the above-mentioned function-enhancing additives are effective also in an existing general metal alloy.
- the same embodiments of the metal alloys shall be applied.
- an alloy material with the foregoing composition is cast-molded, and then, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature. Thereafter, if necessary, the material is aged at prescribed temperature.
- the processed metal alloy an alloy material with the afore-mentioned composition is cast-molded, the material is solution-treated in which rapid cooling is conducted after heating to a prescribed temperature, the material is processed to a prescribed form, and further, the material is aged before or after the foregoing process.
- gadolinium solely only an appropriate amount of a function-enhancing additive that is composited with other element is added to a metal alloy (including high-purity alloy) having a face-centered cubic lattice, a body-centered cubic lattice, or a close-packed hexagonal lattice, not only superior high-function characteristics but also superior hardness, Young's modulus, tensile strength, heat-resistance, and workability than ever may be obtained, even in a cast-molded alloy that is not processed.
- a metal alloy including high-purity alloy
- gadolinium (Gd) is the most effective element to achieve a high function; and in addition, its effect to enhance heat resistance is eminent. Especially, by adding gadolinium (Gd), remarkablely high Young's modulus and elastic limit can be obtained. As can be seen above, gadolinium (Gd) is highly effective to enhance hardness, Young's modulus, and tensile strength; and in addition, eminent enhancement of function characteristics can be obtained. Furthermore, adding amount is small and volume-occupation rate is low; and thus, characteristics unique to a metal alloy can be utilized.
- Gd gadolinium
- Gd gadolinium
- the fine crystallite high-function metal alloy member of the present invention can enhance function characteristics, so that this has strength together with high resisting force, Young's modulus, electrical conductivity, thermal conductivity, softening point, and the like; and in addition, this is not brittle because of the high tensile strength thereof. This is suitable for reduction in the size and weight because of its excellent mechanical characteristics and physical characteristics. This is sustainable. In addition, this has excellent processability and workability.
- the fine crystallite high-function metal alloy member of the present invention has enhanced functions with superior characteristics including hardness, tensile strength, Young's modulus, resisting force, heat resistance, electrical conductivity, and thermal conductivity; and in addition, this has elongation and the like, so that this is easily processed with good workability. Accordingly, this is different from conventional metal alloy members. Furthermore, an important feature thereof resides in that these characteristics can be adjusted in accordance with preference of a user.
- the most significant feature of the present invention resides in that important functional characteristics of the high-function metal alloy of the foregoing elements can be enhanced so that a unique metal alloy having the characteristics thereof adjusted in accordance with preference of a user can be obtained.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Conductive Materials (AREA)
- Adornments (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2011138909A JP2012251235A (ja) | 2011-06-06 | 2011-06-06 | 微細結晶子高機能金属合金部材とその製造方法 |
| JP2011-138909 | 2011-06-06 | ||
| PCT/JP2012/060518 WO2012169285A1 (ja) | 2011-06-06 | 2012-04-10 | 微細結晶子高機能金属合金部材とその製造方法 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20140212324A1 true US20140212324A1 (en) | 2014-07-31 |
Family
ID=47295856
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/124,212 Abandoned US20140212324A1 (en) | 2011-06-06 | 2012-04-10 | Fine crystallite high-function metal alloy member and method for manufacturing same |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20140212324A1 (enExample) |
| EP (1) | EP2719780A4 (enExample) |
| JP (1) | JP2012251235A (enExample) |
| CN (1) | CN103748243A (enExample) |
| WO (1) | WO2012169285A1 (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10851439B2 (en) * | 2017-10-19 | 2020-12-01 | The Boeing Company | Titanium-based alloy and method for manufacturing a titanium-based alloy component by an additive manufacturing process |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103258687B (zh) * | 2013-04-24 | 2015-04-22 | 浙江理工大学 | 一种突跳式温控器 |
| KR101677146B1 (ko) * | 2015-03-17 | 2016-11-17 | 한국생산기술연구원 | 듀플렉스 스테인리스강 및 그 제조방법 |
| CN106893882B (zh) * | 2015-12-18 | 2019-02-05 | 北京有色金属研究总院 | 一种铜钆中间合金的制备方法 |
| US11674193B2 (en) | 2017-05-25 | 2023-06-13 | Sumitomo Electric Industries, Ltd. | Canted coil spring and connector |
| CN110144482B (zh) * | 2019-06-24 | 2020-03-24 | 昆明理工大学 | 一种稀土增强钯合金及其制备方法 |
| CN111763844B (zh) * | 2020-05-20 | 2021-12-17 | 上杭县紫金佳博电子新材料科技有限公司 | 一种键合金带及其制备方法 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08157983A (ja) * | 1994-11-30 | 1996-06-18 | Kuwayama Kikinzoku:Kk | Au高純度の硬質Au合金製装飾部材 |
| DE69618944T2 (de) * | 1995-04-07 | 2002-10-31 | Kazuo Ogasa | Verfahren zur Herstellung einer hochreinen Goldlegierung |
| JP3328130B2 (ja) * | 1995-04-07 | 2002-09-24 | 小笠 和男 | 高純度硬質金合金およびその製造方法 |
| DE69715885T2 (de) * | 1996-06-12 | 2003-06-05 | Kazuo Ogasa | Verfahren zur Herstellung von einer hochreinen Hartgoldlegierung |
| JP2001049364A (ja) * | 2000-07-03 | 2001-02-20 | Kazuo Ogasa | 硬質貴金属合金部材とその製造方法 |
| AU2003211455A1 (en) * | 2002-03-01 | 2003-09-16 | Kazuo Ogasa | Hard metal alloy member and method for manufacture thereof |
| WO2008072485A1 (ja) * | 2006-11-24 | 2008-06-19 | Kazuo Ogasa | 高性能弾性金属合金部材とその製造方法 |
| JP2009030146A (ja) * | 2007-07-26 | 2009-02-12 | Kazuo Ogasa | 高性能弾性金属合金部材とその製造方法 |
-
2011
- 2011-06-06 JP JP2011138909A patent/JP2012251235A/ja active Pending
-
2012
- 2012-04-10 WO PCT/JP2012/060518 patent/WO2012169285A1/ja not_active Ceased
- 2012-04-10 CN CN201280037682.2A patent/CN103748243A/zh active Pending
- 2012-04-10 EP EP12796739.6A patent/EP2719780A4/en not_active Withdrawn
- 2012-04-10 US US14/124,212 patent/US20140212324A1/en not_active Abandoned
Non-Patent Citations (3)
| Title |
|---|
| Machine-English translation of Japanese patent Publication No. 2009-030146, Ogasa Kazuo,February 12, 2009 * |
| Machine-English translation of Japanese patent publication No. 4417115 (B2), February 2, 2010 * |
| Machine-English translation of WO 2008/072485 A1, Ogasa Kazuo, June 19, 2008 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10851439B2 (en) * | 2017-10-19 | 2020-12-01 | The Boeing Company | Titanium-based alloy and method for manufacturing a titanium-based alloy component by an additive manufacturing process |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103748243A (zh) | 2014-04-23 |
| JP2012251235A (ja) | 2012-12-20 |
| EP2719780A1 (en) | 2014-04-16 |
| EP2719780A4 (en) | 2014-12-31 |
| WO2012169285A1 (ja) | 2012-12-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20140212324A1 (en) | Fine crystallite high-function metal alloy member and method for manufacturing same | |
| JP4230218B2 (ja) | 硬質貴金属合金部材およびその製造方法 | |
| TWI521074B (zh) | 電子/電氣機器用銅合金、銅合金薄板及導電構件 | |
| JP6389561B2 (ja) | 金とチタンの軽い貴金属合金、及びこのような金とチタンの軽い貴金属合金で作られた計時器又は宝飾類用の部品 | |
| TW201211282A (en) | Copper alloy sheet and manufacturing method for same | |
| JPWO2002002834A1 (ja) | 硬質貴金属合金部材およびその製造方法 | |
| JP6801163B2 (ja) | 自動車及び電機電子部品用銅合金材及びその製造方法 | |
| TW200426232A (en) | Cu-Ni-Si alloy and production method thereof | |
| JP4620173B1 (ja) | Cu−Co−Si合金材 | |
| JPWO2008072485A1 (ja) | 高性能弾性金属合金部材とその製造方法 | |
| JP2019507252A5 (enExample) | ||
| WO2010096239A1 (en) | Tarnish resistant low gold and low palladium yellow jewelry alloys with enhanced castability | |
| JP5297855B2 (ja) | 銅合金板材およびその製造方法 | |
| JP5610789B2 (ja) | 銅合金板材および銅合金板材の製造方法 | |
| JP2001003125A (ja) | ニッケルフリー白色銅合金材 | |
| JP2000328157A (ja) | 曲げ加工性が優れた銅合金板 | |
| JP5438296B2 (ja) | 宝飾品用Pt合金 | |
| JP4417115B2 (ja) | 硬質金属合金部材とその製造方法 | |
| WO2006013672A1 (ja) | 金合金 | |
| US9005522B2 (en) | Silver alloy | |
| JP5767484B2 (ja) | 銀ベース合金 | |
| TW201233819A (en) | Cu-co-si-zr alloy material and method for producing same | |
| JP2010031310A (ja) | ホワイトゴールド合金 | |
| JPH06264166A (ja) | 耐食性、切削性及び加工性が優れた銅基合金 | |
| JPH04362148A (ja) | 装飾用金合金 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: THREE-O CO., LTD., JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:OGASA, KAZUO;REEL/FRAME:032260/0061 Effective date: 20140122 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |