US1871607A - Aluminium alloy - Google Patents

Aluminium alloy Download PDF

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Publication number
US1871607A
US1871607A US489224A US48922430A US1871607A US 1871607 A US1871607 A US 1871607A US 489224 A US489224 A US 489224A US 48922430 A US48922430 A US 48922430A US 1871607 A US1871607 A US 1871607A
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United States
Prior art keywords
whole
per cent
alloy
aluminium
aluminium alloy
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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US489224A
Inventor
Hall Horace Campbell
Bradbury Tennyson Fraser
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
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Rolls Royce PLC
Priority date (The priority date 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 date listed.)
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Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
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Publication of US1871607A publication Critical patent/US1871607A/en
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon

Definitions

  • the object of this invention is to make a light aluminium alloy having a higher resistance to corrosionthan any such alloy previously known which can be satisfactorily cast, forged or extruded, and this without sacrificing hardness and strength orby sacrificing but little of these qualities.
  • Nickel from 0.5 to 2.5 per cent of the whole.
  • Silicon from 0.5 to 5.0 per cent of the whole.
  • Titanium up to 0.5 per cent of the whole.
  • Chromium from .01 to 0.2 per cent of the whole.
  • An alloy compounded as above has a greater resistance to corrosion than for example, that claimed in our application for Letters Patent No. 401,970 now United States Patent No. 1,7 82,300 but at the same timepossesses about 80 per cent of the hardness and strength of that alloy.
  • this alloy has a higher resistance to corrosion than any previously known light allo of aluminium that it is possible to cast to orce and to extrude satisfactorily due largely to the presence of chromium and to the small copper content associated with the chromium, it is lighter than the aluminium alloys commonly in use which contain copper or zinc with or without other constituents, it
  • the alloy is made in manner common in is capable of being cast, forged or extruded foundry practice, that is to say,'to molten commercial aluminium are added alloys rich in one or more of the other constituents other than magnesium, which is last added in the metallic state.
  • the alloy is cleaned and deoxidised prior to being cast by the addition of sodium.
  • sodium may be added by wrapping a piece of metallic sodium (preferably) not exceeding- 0.1 per cent of the alloy to be treated in a piece of sheet aluminium or aluminium foil the whole being plunged below and held below the surface of the molten alloy until the sodium is diffused.
  • Titanium up to 0.5 per cent of the whole.
  • Chromium from ;01 to 0.2 per cent of the whole.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Electroplating And Plating Baths Therefor (AREA)
  • Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
  • Prevention Of Electric Corrosion (AREA)

Description

Patented Aug. 16, 1932 UNITED STATES PATENT OFFICES- EOBACE CAMPBELL HALL, OF LITTLEOYER DERBY, AND TENNYSON FRASER BRAD- BURY, OF DERBY, ENGLAND, ASSIGNORS '10 ROLLS ROYCE LIMITED, OF DERBY,
I ENGLAND ALUMINIUM ALLOY No Drawing. Application filed October 16, 1930, Serial No. 489,224, and in Great Britain October 24,1929.
It is common knowledge that aluminium and aluminium alloys are liable to corrosion when exposed to the air.
The object of this inventionis to make a light aluminium alloy having a higher resistance to corrosionthan any such alloy previously known which can be satisfactorily cast, forged or extruded, and this without sacrificing hardness and strength orby sacrificing but little of these qualities.
According to this invention we make an alloy by compounding the elements and that in the relative quantlties within the ranges set out below.
Magnesium'from 0.1 to 4 per cent of the whole.
Nickel from 0.5 to 2.5 per cent of the whole.
"Iron from 0.3 to 1.5 per cent of the whole.
Silicon from 0.5 to 5.0 per cent of the whole.
Titanium up to 0.5 per cent of the whole.
anganese up to 0.2 per cent of the whole.
Chromium from .01 to 0.2 per cent of the whole.
Copper up to 0.5 per centof the whole.
Aluminium the remainder except for traces only of other elements.
An alloy compounded as above has a greater resistance to corrosion than for example, that claimed in our application for Letters Patent No. 401,970 now United States Patent No. 1,7 82,300 but at the same timepossesses about 80 per cent of the hardness and strength of that alloy.
Further this alloy has a higher resistance to corrosion than any previously known light allo of aluminium that it is possible to cast to orce and to extrude satisfactorily due largely to the presence of chromium and to the small copper content associated with the chromium, it is lighter than the aluminium alloys commonly in use which contain copper or zinc with or without other constituents, it
so The alloy is made in manner common in is capable of being cast, forged or extruded foundry practice, that is to say,'to molten commercial aluminium are added alloys rich in one or more of the other constituents other than magnesium, which is last added in the metallic state.
Preferably the alloy is cleaned and deoxidised prior to being cast by the addition of sodium. Such sodium may be added by wrapping a piece of metallic sodium (preferably) not exceeding- 0.1 per cent of the alloy to be treated in a piece of sheet aluminium or aluminium foil the whole being plunged below and held below the surface of the molten alloy until the sodium is diffused.
What we claim is V f 'An aluminium alloy formed by compounding the elements and that in the relative quan- Igitlies respectively within the ranges set out e ow 1lllagnesium from 0.1 to 0.4 per cent of the w ole. Nickel from 0.5 to 2.5 per cent of the whole.
Iron from 0.3 to 1.5 per cent of the whole.
Silicon from 0.5 to 5 per cent of the whole.
Titanium up to 0.5 per cent of the whole.
Manganese up to 0.2 per cent of the whole.
Chromium from ;01 to 0.2 per cent of the whole.
Copper up to 0.5 per cent of the whole.
Aluminium the remainder except for traces only of other elements,
In testimony whereof we have hereto affixed our signatures.
HORACE CAMPBELL HALL.
TENNYSON FRASER BRADBURY. 7
US489224A 1929-10-24 1930-10-16 Aluminium alloy Expired - Lifetime US1871607A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1871607X 1929-10-24

Publications (1)

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US1871607A true US1871607A (en) 1932-08-16

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4833123B1 (en) * 1969-05-16 1973-10-12
DE2423597A1 (en) * 1973-05-17 1974-11-28 Alcan Res & Dev IMPROVED ALUMINUM ALLOY PRODUCTS AND METHODS FOR MANUFACTURING THEREOF
DE2551294A1 (en) * 1974-11-15 1976-05-26 Alcan Res & Dev PROCESS FOR MANUFACTURING IMPROVED METAL ALLOY PRODUCTS
JPS5163479A (en) * 1974-10-04 1976-06-01 Pechiney Aluminium
US4571368A (en) * 1983-01-17 1986-02-18 Atlantic Richfield Company Aluminum and zinc sacrificial alloy
US4619712A (en) * 1981-11-10 1986-10-28 Mitsubishi Light Metal Industries Limited Superplastic aluminum alloy strips and process for producing the same
US5023051A (en) * 1989-12-04 1991-06-11 Leggett & Platt Incorporated Hypoeutectic aluminum silicon magnesium nickel and phosphorus alloy

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4833123B1 (en) * 1969-05-16 1973-10-12
DE2423597A1 (en) * 1973-05-17 1974-11-28 Alcan Res & Dev IMPROVED ALUMINUM ALLOY PRODUCTS AND METHODS FOR MANUFACTURING THEREOF
JPS5163479A (en) * 1974-10-04 1976-06-01 Pechiney Aluminium
JPS5512179B2 (en) * 1974-10-04 1980-03-31
DE2551294A1 (en) * 1974-11-15 1976-05-26 Alcan Res & Dev PROCESS FOR MANUFACTURING IMPROVED METAL ALLOY PRODUCTS
US4619712A (en) * 1981-11-10 1986-10-28 Mitsubishi Light Metal Industries Limited Superplastic aluminum alloy strips and process for producing the same
US4571368A (en) * 1983-01-17 1986-02-18 Atlantic Richfield Company Aluminum and zinc sacrificial alloy
US5023051A (en) * 1989-12-04 1991-06-11 Leggett & Platt Incorporated Hypoeutectic aluminum silicon magnesium nickel and phosphorus alloy

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