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PRODUCT DATA of AA2017-T4 |
Material | AA2017-T4 |
General Information | This is a heat treatable (age-hardening) alloy of intermediate strength and good ductility |
Precautions | Typical data from the Aluminium Association (AA). Not for design |
Chemical Composition | Al-4Cu-0.6Mg0.7Mn-0.5Si-0.1Cr |
EXPERIENCE IN PRACTICE |
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Development Status | Commercial Product |
Equivalent Designations | AlCuMgSi; UNS A92017; NF A-U46, AA 2017 |
PHYSICAL PROPERTIES |
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Crystal Structure | Face centered cubic (fcc) |
Specific Gravity | 2.79 |
Magnetic Properties | Nonmagnetic |
ELASTIC PROPERTIES |
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Tensile Modulus | 75 GPa Data Quality: Typical Data |
Bulk Modulus | 27 GPa Data Quality: Typical Data |
MECHANICAL PROPERTIES |
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Ultimate Tensile Strength | 427 MPa Data Quality: Typical Data |
Proof Stress (0.2%) | 276 MPa Data Quality: Typical Data |
Elongation | 22 % Data Quality: Typical Data |
Fatigue Limit | 124 MPa Data Quality: Typical Data |
Hardness | 105 HB Data Quality: Typical Data |
Shear Strength | 262 MPa Data Quality: Typical Data |
THERMAL PROPERTIES |
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Thermal Conductivity | 134 W/m.K |
Thermal Expansion Coefficient | 23.6 μstrain/°C |
Specific Heat | 0.88 J/g.K |
Melting Range | 513 to 641 °C |
RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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General Corrosion Status | Requires specific corrosion protection |
Stress Corrosion Status | Low Resistance to SCC: Table 3 Data Quality: Design Data |
EMF vs SCE | -0.61 V |
Bimetallic Corrosion | Can be used in a non-controlled environment with: Al+alloys, Cd, Sn-Pb alloys, Sn, Pb Can be used in a clean room environment with: as above and Mg, Ni, Monel, Inconel, Ni-Mo alloys, 300 series SS, 400 series SS, Ti and Ti alloys, Zn, Be Needs specific measures: All others Test:ECSS-Q-ST-70C Rev.1 table 5.1 Data Quality: Design Data |
Machinability | Machinability is very good for this alloy in the T4 temper. In the annealed condition machinability is less good. Thus it is best to perform machining with the alloy in the T4 condition. Use of oil lubricants is recommended for all machining operations. |
Welding | The alloy may be welded, however welding heat will reduce corrosion resistance. In general welding should be avoided unless heat treatment after welding is possible to restore corrosion resistance. Inert gas welding and resistance welding are the methods that should be used and the alloy is sensitive to cracking so fixturing needs to be such as to reduce any strain during welding. |
Aging | This alloy is age hardenable and that occurs naturally at room temperature. |