IE41814B1 - Aluminium based alloy - Google Patents

Aluminium based alloy

Info

Publication number
IE41814B1
IE41814B1 IE228775A IE228775A IE41814B1 IE 41814 B1 IE41814 B1 IE 41814B1 IE 228775 A IE228775 A IE 228775A IE 228775 A IE228775 A IE 228775A IE 41814 B1 IE41814 B1 IE 41814B1
Authority
IE
Ireland
Prior art keywords
alloy
aluminium
based alloy
calcium
aluminium based
Prior art date
Application number
IE228775A
Other versions
IE41814L (en
Original Assignee
Euratom
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.)
Filing date
Publication date
Application filed by Euratom filed Critical Euratom
Publication of IE41814L publication Critical patent/IE41814L/en
Publication of IE41814B1 publication Critical patent/IE41814B1/en

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Metal Rolling (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Forging (AREA)

Abstract

1452646 Superplastics aluminium based alloy EUROPEAN ATOMIC ENERGY COMMUNITY 11 Aug 1975 [13 Nov 1974] 49059/74 Heading C7A Superplastics Aluminium alloy of composition:- The alloy may be prepared by melting calcium and aluminium together in the absence of oxygen and subsequently working e.g. rolling or drawing at a temperature above 270‹C preferably in vacuum or an inert atmosphere.

Description

This invention relates to an aluminium based alloy. Such alloys may possess superelastic or superplastic properties at certain temperatures.
Some metallic alloys are called superplastic because of 5 their capability, when heat treated, to undergo elongations of the order of more than 500% without necking and to shape-form under the action of very small loadings. These alloys can be quickly vacuum formed in a single operation Starting from sheets and complex shapes can be easily achieved.
According to the present invention there is provided an aluminium based alloy consisting of from 5 to 10% by weight of calcium and not more than 1% by weight of impurities, the remainder being aluminium. The alloy preferably comprises 7.6% by weight of calcium and not more than 1% by weight of impurities, the remainder being aluminium. This alloy has a melting point of 616°C.
The present invention also relates to a method of preparing an aluminium based alloy comprising melting calcium and aluminium together in the absence of oxygen to produce an aluminium based alloy comprising from 5 to 10% by weight of calcium and not more than 1% by weight of impurities, the remainder being aluminium.
The alloy is subjected to mechanical treatment such as rolling or drawing at a temperature higher than 27O°C.
The mechanical treatment is conveniently carried out in the absence of oxygen.
The aluminium based alloys prepared by the method of the present invention have superplastic properties preferably superplastic properties under vacuum or an inert atmosphere at temperatures of from 350 to 550°C as follows :2 Properties in superplastic condition Elongation Load Temperature Optimum temperature Deformation rate Optimum Deformation rate 500-550% 0.25-1.00 kg/mm^ 35O-55O°C 400°C 0.5-0.02 cm/min. 0.2 cm/min One method of preparing an aluminium based alloy will now be described.
The melting of the components took place under vacuum or an inert atmosphere because of the nature of the components In particular calcium metal oxidises readily in the presence of oxygen. Starting from commercially pure aluminium and calcium (purity 99-99.8%) ingots were formed by melting the components together. Furthermore under vacuum or an inert atmosphere rolling or drawing of the ingots took place at temperatures higher than 27O°C in order to obtain sheets with a thickness varying from 0.5 to 3 mm.
The mechanical properties at room temperature and normal pressure of the aluminium based alloy product are: Tensile strength (S) 25-33 kg/mm^ Elongation (E) ^10% Other principal characteristics of the alloy described above may be summarised as follows :a) large deformation occurred without necking up to a maximum value of 1000%, b) the alloy had low forming stresses at moderate temperatures, c) the possibility to form the metal readily and to obtain any desired shape without the need of very high stresses or temperatures was recognised. d) conservation of the original properties after vacuum 5 forming and/or other operations, e) the alloy may be welded using standard techniques. Moreover it can be anodised by usual methods in order to give a decoration finish and to enhance the corrosion resistance. f) the corrosion behaviour of the alloy prepared as described in comparable to that of aluminium.

Claims (7)

CLAIMS:
1. An aluminium based alloy consisting of from 5 to 10% by weight of calcium and not more than 1% by weight of impurities, the remainder being aluminium. 5
2. An alloy as claimed in claim 1 comprising 7.6% by weight of calcium.
3. An alloy as claimed in claim 1 and substantially as hereinbefore described.
4. A method of preparing an aluminium base alloy as claimed x 0 in claim 1 comprising melting calcium and aluminium together ln the absence of oxygen to produce an aluminium based alloy, and subjecting the alloy to mechanical treatment at a temperature higher than 27O°C.
5. A method as claimed in claim 4 wherein the mechanical 15 treatment is carried out in the absence of oxygen.
6. A method as claimed in claim 4 and substantially as hereinbefore described.
7. An alloy whenever prepared by a method as claimed in any one of claims 4 to 6.
IE228775A 1974-11-13 1975-10-21 Aluminium based alloy IE41814B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4905974A GB1452646A (en) 1974-11-13 1974-11-13 Aluminium based alloy

Publications (2)

Publication Number Publication Date
IE41814L IE41814L (en) 1976-05-13
IE41814B1 true IE41814B1 (en) 1980-03-26

Family

ID=10450967

Family Applications (1)

Application Number Title Priority Date Filing Date
IE228775A IE41814B1 (en) 1974-11-13 1975-10-21 Aluminium based alloy

Country Status (9)

Country Link
BE (1) BE835463A (en)
DE (1) DE2548171A1 (en)
DK (1) DK489775A (en)
FR (1) FR2291283A1 (en)
GB (1) GB1452646A (en)
IE (1) IE41814B1 (en)
IT (1) IT1052188B (en)
LU (1) LU73791A1 (en)
NL (1) NL7512969A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
LU82002A1 (en) * 1979-12-17 1980-04-23 Euratom PROCESS FOR MAKING OBJECTS FORMED FROM A SUPERPLASTIC ALLOY MORE DUCTILE
US20190316241A1 (en) * 2016-07-12 2019-10-17 Nippon Light Metal Company, Ltd. Aluminum alloy plastic working material and production method therefor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1935245A (en) * 1932-01-23 1933-11-14 Calloy Ltd Process for the reduction of alkaline earth metals and the production of alloys of aluminium
DE1133562B (en) * 1960-06-09 1962-07-19 Sueddeutsche Kalkstickstoff Process for the production of calcium-aluminum alloys

Also Published As

Publication number Publication date
DE2548171A1 (en) 1976-05-26
IT1052188B (en) 1981-06-20
NL7512969A (en) 1976-05-17
BE835463A (en) 1976-03-01
IE41814L (en) 1976-05-13
DK489775A (en) 1976-05-14
FR2291283A1 (en) 1976-06-11
LU73791A1 (en) 1976-06-11
GB1452646A (en) 1976-10-13
FR2291283B1 (en) 1981-01-23

Similar Documents

Publication Publication Date Title
US4844746A (en) Method of producing a tantalum stock material of high ductility
US3497402A (en) Stabilized grain-size tantalum alloy
EP2388346A1 (en) Production of fine grain niobium products by micro-alloying and ingot metallurgy
CN109338187B (en) Low-cost high-strength and high-toughness wrought magnesium alloy capable of being extruded at high speed and preparation method thereof
US2892742A (en) Process for improving the workability of titanium alloys
ES475808A1 (en) Al-Mn Alloy and process of manufacturing semifinished products having improved strength properties
JPH0572452B2 (en)
JPH08295969A (en) High strength titanium alloy suitable for superplastic forming and production of alloy sheet thereof
US2768915A (en) Ferritic alloys and methods of making and fabricating same
IE41814B1 (en) Aluminium based alloy
GB928407A (en) Improvements in the production of titanium base alloys
US4428778A (en) Process for producing metallic chromium plates and sheets
US5019183A (en) Process for enhancing physical properties of aluminum-lithium workpieces
CN113549788A (en) Double-state high-strength plastic-zirconium alloy and preparation method thereof
US3843416A (en) Superplastic zinc/aluminium alloys
US4507156A (en) Creep resistant dispersion strengthened metals
US4381954A (en) Method of increasing the ductility of articles formed from superplastic alloy and article
US4820354A (en) Method for producing a workpiece from a corrosion- and oxidation-resistant Ni/Al/Si/B alloy
US3287110A (en) Non-ferrous alloy and method of manufacture thereof
US4067753A (en) Process for the manufacture of shaped parts from multi-component silver-copper alloys
JP2729011B2 (en) TiAl-based intermetallic compound alloy having high strength and method for producing the same
JPH03197630A (en) Method for hot-working intermetallic compound ti-al base alloy
CA1084819A (en) Process for the manufacture of shaped parts from multi-component silver-copper alloys
JPS62103335A (en) Ultra-high-purity metallic niobium
JPH0116910B2 (en)