US2116274A - Aluminium alloy - Google Patents
Aluminium alloy Download PDFInfo
- Publication number
- US2116274A US2116274A US110553A US11055336A US2116274A US 2116274 A US2116274 A US 2116274A US 110553 A US110553 A US 110553A US 11055336 A US11055336 A US 11055336A US 2116274 A US2116274 A US 2116274A
- Authority
- US
- United States
- Prior art keywords
- aluminium alloy
- aluminium
- alloys
- alloy
- iron
- 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.)
- Expired - Lifetime
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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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
Definitions
- This invention relates to an.aluminium alloy or beryllium does not appreciably modify the containing main and auxiliary elements, the properties of the alloy so that alloys containing 5 ai l t consisting of 2 t 5% magnesium, one or more of the above elements are considered 6 to 14% -zinc, 0.2 to 2.0% nickel, 0.01 to 1.5% equivalent'alloys to each Other'. iron, 0.1 to 1.0% silicon and the rest substantially As m be e from the above example, the new aluminium keeping the condition that the conalloy has a f great tensile strength. and F tent of silicon is always greater than that of iron, great 3 9?
- auxiliary elements consisting of a metal known alumlmum p selected from the group of 0.1 to 1.5% man- As to i q actlon of elements of the ganese, a few percentage of cobalt, molybdenum, new P It supposefd as f w? A part of vanadium, tungsten, titanium lithium and berylmagnesium combme wlth smegmto form 15 lium
- the object of the invention is to obtain an magnesmm slhclde and another part of magnesium may be alloyed with a part of zinc and alumimum alloy whlchhas a tenslle.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Soft Magnetic Materials (AREA)
- Prevention Of Electric Corrosion (AREA)
- Laminated Bodies (AREA)
Description
Patented May 3, 1938 I it I UNITED STATESPATENT OFFICE ALUMINIUM ALLoY.
Yonosuke -Matuenaga, Naka-ku, Yokohama, Japan .No Drawing. Original application May 8, 1936,
Serial No. 78,723. Divided and this. application November 12, 1936, Serial No. 110,553. In Japan May 13, 1935 1 Claim. '(Gl. 75-146) This application is a divisional from appli- It is acknowledged from repeated experiments cants copending application Serial No. 78,723, that addition of a few percentage'of cobalt; mofiled May 3, 193 lybdenum, vanadium, tungsten, titanium, lithium.-
This invention relates to an.aluminium alloy or beryllium does not appreciably modify the containing main and auxiliary elements, the properties of the alloy so that alloys containing 5 ai l t consisting of 2 t 5% magnesium, one or more of the above elements are considered 6 to 14% -zinc, 0.2 to 2.0% nickel, 0.01 to 1.5% equivalent'alloys to each Other'. iron, 0.1 to 1.0% silicon and the rest substantially As m be e from the above example, the new aluminium keeping the condition that the conalloy has a f great tensile strength. and F tent of silicon is always greater than that of iron, great 3 9? which are hardly obtainable m '10 while the auxiliary elements consisting of a metal known alumlmum p selected from the group of 0.1 to 1.5% man- As to i q actlon of elements of the ganese, a few percentage of cobalt, molybdenum, new P It supposefd as f w? A part of vanadium, tungsten, titanium lithium and berylmagnesium combme wlth smegmto form 15 lium The object of the invention is to obtain an magnesmm slhclde and another part of magnesium may be alloyed with a part of zinc and alumimum alloy whlchhas a tenslle. a part of aluminium to form various three ele- Strength and great elongation especially when mental alloys of difierent percentage Further subjected under heat treatment nickel may be alloyed with iron. These chemical Example of th oy Showing Percentages of compounds and alloys may crystal out in the the elements employed and also tensile strength ain element, viz., aluminium and may be uniand elongation when the, alloys are subjected formly distributed therein. Further, when manunder a mode of tempering-and annealing is ganeseis employed, this manganese not only acts given as follows: as reducing agent, but also hinders the growth of particles of zinc-manganese-aluminiun:i alloys Example "7-- I% 11% and also of nickel-iron alloy so that the dis- M 2.5 2.5 tribution of the alloy may be promoted. Z11 9.0 9.0 what I'claim is:- N 0.5 1.0 An aluminium alloy containing 2 to 5% mag- F 0.2 0.2 nesium, 6 to 14% zinc, 0.2 to 2% nickel, 0.0l to Si 0.6 0.6 1.5% iron, .1 to 1% silicon, the silicon content M v 0.8 0.8 being always greater than the iron content, .1 to A1 Rest Rest 1.5% manganese and the rest aluminium. Tensile strength l:g./cm. 58.5 60.3 Elonzatlon 15 12 YONOSUKE MATUENAGA.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US110553A US2116274A (en) | 1936-05-08 | 1936-11-12 | Aluminium alloy |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US78723A US2090895A (en) | 1935-05-13 | 1936-05-08 | Aluminium alloy |
US110553A US2116274A (en) | 1936-05-08 | 1936-11-12 | Aluminium alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2116274A true US2116274A (en) | 1938-05-03 |
Family
ID=26760863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US110553A Expired - Lifetime US2116274A (en) | 1936-05-08 | 1936-11-12 | Aluminium alloy |
Country Status (1)
Country | Link |
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US (1) | US2116274A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE938444C (en) * | 1939-12-20 | 1956-02-02 | Ver Leichtmetall Werke Ges Mit | Stress corrosion resistant aluminum alloys |
DE972684C (en) * | 1939-02-22 | 1959-09-17 | Vaw Ver Aluminium Werke Ag | Use of aluminum alloys for the manufacture of parts subject to stress corrosion |
-
1936
- 1936-11-12 US US110553A patent/US2116274A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE972684C (en) * | 1939-02-22 | 1959-09-17 | Vaw Ver Aluminium Werke Ag | Use of aluminum alloys for the manufacture of parts subject to stress corrosion |
DE938444C (en) * | 1939-12-20 | 1956-02-02 | Ver Leichtmetall Werke Ges Mit | Stress corrosion resistant aluminum alloys |
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