Alloys and Properties
[Pages:10]TALAT Lecture 3501
Alloys and Properties
8 pages, 6 figures Basic Level
prepared by Klaus Siegert and Manfred Kammerer, Institut f?r Umformtechnik, Universit?t Stuttgart
Objectives: - To provide a background on aluminium alloys suitable for impact extrusion - To draw attention to raw material parameters which may affect the properties of
impact extruded parts
Prerequisites: - Basic knowledge about the formability of metals - Background in mechanical engineering
Date of Issue: 1994
EAA- Euro p ean Aluminium Asso ciatio n
3501 Alloys and Properties
Table of Contents: 3501 Alloys and Properties ..................................................................................2
3501.01 General Information on Alloys and Raw Materials ................................ 2 Aluminium Alloys for Impact Extrusion .................................................................2 Reference Values for the Strength of Aluminium Alloy Impacts............................3 Flow Curves and Fow Stresses ................................................................................4 Raw Materials, Blanks and Slugs ............................................................................5 Lubricants ................................................................................................................5 Tool Life as a Function of Amounts of Lubricant ...................................................6
3501.02 Literature: ................................................................................................... 8 3501.03 List of figures............................................................................................... 8
3501.01 General Information on Alloys and Raw Materials
Aluminium Alloys for Impact Extrusion Figure 3501.01.01 lists the different types of aluminium alloys used for impact extrusion together with an evaluation considering different aspects. All aluminium alloys of the non-heat-treatable and heat-treatable types can be impact extruded, especially when in their soft annealed state. (See also DIN 1712, part 3 and DIN 1725, part 1).
TALAT 3501
2
Aluminium Designation
Alloys
according to DIN 1712, p.3
Relative merit values1) under various aspects
Impact extrud-
Decorative Joining Remarks anodising process3)
for Impact and
ability 2)
DIN 1725, p.1
SL
Extrusion
Aluminium alloys for impact extrusion
1)Merit values, falling from 1 to 4;
Pure and high purity aluminium (DIN 1712, part3)
Al99.5 Al99.7 Al99.8 Al99.9
1
2
2 1 Main material for impacts
1
2
21
1
1
21
1
1
2 1 Chemical brightening possible
"-" = not suitable Non-heat-treatable alloys (DIN 1725, part 1)
2)Valuation is valid
for the original soft AlMn
2
-
21
annealed state
AlRMg0.5
2
1
2 2 Chemical brightening possible
3)S = weldability; L = suitability for brazing. Strength loss due to welding and
AlMg1
2
2
22
AlMg3
4
2
1-
AlMg2Mn0.3
3
3
1-
Heat-treatable alloys (DIN 1725, part 1)
soldering must be AlMgSi0.5
considered!
AlMgSi1
2
1
23
3
2
23
AlZn4.5Mg1
3
-
2 - Used only in artificially aged state
Source: Aluminium
AlCuMg1
4
-Zentrale e.V.
AlZnMgCu0.5
4
-
- - Only for parts with heavy wall thickness
-
- - which are used only in an aged state
alu Training in Aluminium Application Technologies
Aluminium Alloys for Impact Extrusion
3501.01.01
In order to obtain high quality impacts, it is important to use materials which exhibit a homogeneous fibre structure or a uniform fine-grained structure. A non-homogeneous structure affects not only the chemical and physical properties of the impacts but also their form. An unsymmetrical grain structure can have a large effect on flow stress which in turn might lead to excentricity of the part, warpage or uneven distribution of wall thicknesses.
Reference Values for the Strength of Aluminium Alloy Impacts
Figure 3501.01.02 tables reference values for the strength of aluminium alloy impacts. The aluminium alloys Al99,9, Al99,8. Al99,7 and Al99,5 are mainly used for manufacturing tubes and cans. The alloys AlMgSi0,5 and AlMgSi1 can be considered to be standard materials for impact extrusion. Care must be taken during the machining of the alloys AlZn4,5Mg1 and AlZnMgCu0,5, since the emulsions used can lead to corrosion.
TALAT 3501
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Reference Values for the Strength of Impacts
Attainable mechanical properties, not minimum values
1) By impact extruding directly after solution treatment and quenching ("freshly quenched" state) and then aging, 90% of the strength of the state "artificially aged" can be attained.
Source: Aluminium-Zentrale e.V.
Designation
Al99.5/ Al99 Al99.7/ Al99.8 Al99.9
AlMn
AlRMg0.5
AlMg1
AlMg3
AlMg2Mn0.3
AlMgSi0.5 1) AlMgSi1 1) AlZn4.5Mg1 AlCuMg1 AlZnMgCu0.5
State
annealed impact extruded annealed impact extruded annealed impact extruded annealed impact extruded annealed impact extruded annealed impact extruded annealed impact extruded annealed impact extruded annealed, imp. extr. artificially aged annealed, imp. extr. artificially aged artificially aged naturally aged artificially aged
Strength in N/mm?
Rm (B) Rp0.2 (0.2)
70
25
130
110
60
18
120
100
40
15
100
80
90
35
170
145
80
25
140
110
105
35
165
145
190
80
265
215
155
60
230
200
165
145
245
195
190
170
310
260
350
290
400
350
500
450
Elongation
A5 (%)
40 6
40 4
40 4
24 4
23 4
24 4
20 4
20 4 4
10 4
10 10 10
7
alu Training in Aluminium Application Technologies
Reference Values for the Strength of Impacts
3501.01.02
Flow Curves and Fow Stresses
Figure 3501.01.03 shows flow curves and flow stresses of some aluminium alloys (at left) and the effect of state of heat treatment of AlMgSi1-slugs on the flow behaviour (at right). Flow curves are needed for the calculation of forces for the impact extrusion process. For further flow curves, refer to the VDI guideline 3500.
Flow Curves and Flow Stresses
Flow stress, kf Flow stress, kf
Flow curves for various annealed aluminium alloys at room temperature
600 N/mm?
400
State: annealed = 5 x 10-4 s-1
AlMg3
AlCuMg
AlMgSi(Mn) 200
Al99.5
0
0
1
2
3
True strain
Source: J.Hardt
Flow stress as a function of heat treatment state of the slug
600 N/mm?
400
Artificially aged Naturally aged
Hot worked
200
Soft
AlMgSi1
RT
0
0
1
2
3
True strain
Source: H.G.Roczyn
alu Training in Aluminium Application Technologies
Flow Curves and Flow Stresses
3501.01.03
TALAT 3501
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Raw Materials, Blanks and Slugs
Figure 3501.01.04 gives information regarding the manufacturing of slugs and blanks, their required surface condition and their properties. Cold rolled sheets and rods or tubes from which blanks and slugs are obtained by blanking or sawing, respectively, are standardised in DIN 1745, part 1 and DIN 59604. Round rods of pure aluminium or aluminium alloys are extruded with so-called multiple extrusion dies, i.e. three or four die openings are arranged around the centre of the die. In a final step these rods are cold drawn to size and final dimensions. Since the material is pressed through the multiple die not only from the centre portion of the billet but also from its outer areas, such round rods may exhibit different grain sizes in any one cross-section. As a result, impact extruded parts can warp in unexpected amounts and wall thicknesses may vary. Therefore, care should be exercised, that only single-strand extruded rods are taken as base material for slugs and blanks.
Raw Materials; Blanks and Slugs
Manufacturing raw materials The raw material consists almost exclusively of stamped or sawed blanks and slugs available from extruders or stockists
Surface condition of raw material Blank, ground, tumbled, blasted
Requirements of raw material ! The weight of blanks or slugs is allowed to vary only within a narrow
tolerance range ! Minimum clearance between slugs and die: 0.3 to 0.4mm ! Maximum tolerance for round slugs and blanks is h11 (larger deviations in
diameter lead to positioning errors) ! A uniform grain size. Varying grain size can lead to variations in dimensions
Source: Schlosser; Brix
alu Training in Aluminium Application Technologies
Raw Materials; Blanks and Slugs
3501.01.04
Lubricants
Figure 3501.01.05 lists the different lubricants used and the methods of applying them. Because of environmental considerations, water-soluble lubricants like alkalinen soaps and liquid lubricants based on oil are being increasingly used. Zinc stearate and zinc behenate have nowadays to compete with
- Lubrimet GTT (Sapilub Ltd. Co. Wangen, Zurich) based on paraffin without chlorinated solvents and heavy metal soaps with optimal solubility in water,
- Glisapal SM-155 (Nu?baum Co., Matzingen), a water-soluble, solvent-free, powdery lubricant based on alkaline soaps, not suitable for anneal degreasing and solvent cleaning,
TALAT 3501
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- and liquid lubricants based on oil, like Bonderlube VP 4404/5 (Chemetall Co., Frankfurt), with sulphur compounds, but free from chloroparaffins and metal organic compounds or
- Multipress 9391 (Zeller and Gmelin Co., Eislingen), a fully synthetic oil.
In individual cases, coating layers serving as carriers for lubricants (aluminium, phosphate) are used.
Lubricants
Lubricants used ! Zinc stearate and zinc behenate (insoluble in water) ! Alkaline soaps (water soluble) ! Liquid lubricants based on oil (water soluble)
Methods of applying lubricants ! Spraying ! Coating ! Sprinkling, powdering ! Dipping ! Tumbling
Source: D.Schlosser
alu Training in Aluminium Application Technologies
Lubricants
3501.01.05
Tool Life as a Function of Amounts of Lubricant
Figure 3501.01.06 illustrates the influence of amount of lubricant used (g/m?) on tool life. As can be clearly seen, too little or too much lubrication reduces the tool life. If the lubricant used is insufficient, cold welding can occur between tool and work-piece. If too much lubricant is used, then the lubricant accumulation leads to defects in contour replication and to lubricant indentations in the tool. In these cases, the tool has to be cleaned very often. The surface roughness of slugs and blanks has an effect on the tool life. Experiments have shown that smooth slugs reduce the life of tools because the smooth slug surface offers hardly any cavities and pits in which the lubricant can be anchored.
TALAT 3501
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Tool Life as a Function of Amounts of Lubricant
Cold welding
failure
optimum
Contour defects
failure
Tool life
Source: D.Schlosser
alu Training in Aluminium Application Technologies
Relative lubricant amount in g/ m? Tool Life and Lubricant Amounts
3501.01.06
TALAT 3501
7
3501.02 Literature:
1) F.Ostermann: Technische Kaltflie?pre?teile aus Aluminium. In seminar volume "Gestalten und Fertigen von technischen Flie?pre?teilen aus Aluminium", Institut f?r Umformtechnik, Universit?t Stuttgart, 15.-16. June, 1992
2) D.Schlosser: Einflu?gr??en auf das Flie?pressen von Aluminium und Aluminiumlegierungen und ihre Auswirkung auf die Weiter- und Fertigbearbeitung der flie?gepre?ten Rohteile. In seminar volume "Gestalten und Fertigen von technischen Flie?pre?teilen aus Aluminium", Institut f?r Umformtechnik, Universit?t Stuttgart, 15.-16. June, 1992
3) D.Brix: Kaltflie?pressen von Leichtmetall - Qualit?t und Wirtschaftlichkeit. Draht 1975/5, p. 216-219
4) VDI-Richtlinie 3138: Kaltflie?pressen von St?hlen und Nichteisenmetallen, Grundlagen, part 1. Beuth-Verlag, Berlin, 1970
5) Aluminium-Zentrale e.V., Report No. 29 "Aluminium f?r technische Flie?pre?teile", D?sseldorf, 1982
3501.03 List of figures
Figure No. 3501.01.01 3501.01.02 3501.01.03 3501.01.04 3501.01.05 3501.01.06
Figure Title (Overhead) Aluminium Alloys for Impact Extrusion Reference Values for the Strength of Impacts Flow Curves and Flow Stresses Raw Materials; Blanks and Slugs Lubricants Tool Life and Lubricant Amounts
TALAT 3501
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