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Aluminum 7175 · temper

Aluminum 7175-T7454

Properties of the T7454 condition, compared with the other 7175 tempers.

High-strength Al-Zn-Mg-Cu die-forging temper: T74 two-step overage giving near-T6 strength with good SCC and exfoliation resistance, residual stress removed by cold restrike in the finish die.

CNC machiningSheet metalPremium cost $$$

What is 7175-T7454?

7175-T7454 is 7175 in the T7454 temper — high-strength Al-Zn-Mg-Cu die-forging temper: T74 two-step overage giving near-T6 strength with good SCC and exfoliation resistance, residual stress removed by cold restrike in the finish die. 7175-T7454 has a yield strength of 455 MPa (66 ksi) and a tensile strength of 525 MPa (76.1 ksi) — stronger than 92% of aluminum grades. Elongation at break is 11% and the elastic modulus is 71.7 GPa (10.4 Msi). 7175-T7454 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • Tough — resists crack growth — 38 MPa·√m (34.6 ksi·√in), better than 96% of aluminum grades
  • High strength — 455 MPa (66 ksi), better than 92% of aluminum grades
  • Polishes to a fine finish — 65/100, better than 82% of aluminum grades
  • Easy to machine — 72/100, better than 80% of aluminum grades

Limitations

  • Difficult to weld — 20/100, worse than 89% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7175-T7454 properties

Typical room-temperature values for 7175-T7454 — 37 properties are specific to this condition; the rest are grade-level values shared by every 7175 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7175-T7454 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 477°C (891 °F).

Density2.8 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature635°C1,175 °F

Mechanical14

7175-T7454 has a yield strength of 455 MPa (66 ksi) and a tensile strength of 525 MPa (76.1 ksi) — stronger than 92% of aluminum grades. Elongation at break is 11% and the elastic modulus is 71.7 GPa (10.4 Msi).

Elastic (Young's) Modulus71.7 GPa10.4 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)525 MPa76.1 ksi
Yield Strength (0.2% offset)455 MPa66 ksi
Elongation at Break11%
Reduction in Area25%
Compressive Strength460 MPa66.7 ksi
Shear Strength305 MPa44.2 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Fracture Toughness (K_IC)38 MPa·√m34.6 ksi·√in
Hardness, Brinell135 HB
Hardness, Vickers145 HV

Thermal6

7175-T7454 is rated for continuous service to 120°C (248 °F). It conducts heat at 155 W/m·K (89.6 BTU/hr·ft·°F), better than 71% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity155 W/m·K89.6 BTU/hr·ft·°F
Specific Heat Capacity865 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.4 µm/m·K13 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F

Electrical3

7175-T7454 conducts electricity at 40 % IACS, better than 72% of aluminum grades.

Electrical Conductivity40 % IACS
Electrical Resistivity4.3×10⁻⁸ Ω·m1.69 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (58/100), better than 57% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.78 V
Corrosion ResistanceGood58/100
Chemical Resistance SummaryGood in dry atmospheres and neutral organics; attacked by strong acids/alkalis, chlorides and mercury salts; T6 tempers are SCC-sensitive in the short-transverse direction, so T73/T74 overaged tempers are specified for exposed aerospace parts.

Sustainability4

Producing a kilogram of 7175-T7454 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 10%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,150 L/kg138 gal/lb
Typical Recycled Content10%

Manufacturability7

7175-T7454's machinability is very good (72/100, better than 80% of aluminum grades); weldability poor (20/100); formability poor (25/100).

MachinabilityVery good72/100
Machinability Rating (AISI 1212 = 100 %)70%
WeldabilityPoor20/100
Formability (cold)Poor25/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood65/100
Anodizing Responsegood — chromic/sulfuric and Type III hardcoat all work; clear coatings take a grey-tan tint from Zn/Cu, so dyed or hardcoat finishes are preferred

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 7175 tempers and conditions

7175 is also supplied in 12 other conditions. The full side-by-side table is on the 7175 overview.

Working with 7175-T7454

Is 7175 easy to machine?

Machines very well in T7x tempers with sharp polished carbide, high speed and flood coolant; expect long chips and use chip-breaking geometry.

Can 7175 be welded?

Not arc weldable for structure (hot-cracking, SCC in HAZ); join by riveting, bolting, adhesive bonding or friction stir welding with process qualification.

Can 7175 be formed, bent or molded?

Forge/hot work at ~380–440 °C; cold forming in T-tempers is very limited — form in O or W temper and re-heat-treat.

What surface finishes work on 7175?

Chromic/sulfuric anodize, Type III hardcoat, chemical conversion coating (Alodine) plus primer; avoid caustic etch overexposure on close-tolerance machined parts.

7175 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Zn5.1 – 6.15.6
Mg2.1 – 2.92.5
Cu1.2 – 21.6
Crgrain-structure control0.18 – 0.280.23
Ferestricted vs 7075 for toughness≤ 0.20.12
Sirestricted vs 7075≤ 0.150.08
Mn≤ 0.10.03
Ti≤ 0.10.03
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

7175-T7454 — frequently asked

What is 7175-T7454 used for?

7175-T7454 is typically used for aircraft structural fittings, helicopter rotor hubs, fuselage frames and bulkheads, landing gear components, wing and spar forgings and highly loaded machined brackets. In short: premium aerospace forging.

What is the yield strength of 7175-T7454?

7175-T7454 has a typical yield strength of 455 MPa (66 ksi) and a tensile strength of 525 MPa (76.1 ksi) — stronger than 92% of aluminum grades. Strength varies by condition: see the 13 listed tempers.

Is 7175-T7454 easy to machine?

Yes — machinability is rated very good (72/100, better than 80% of aluminum grades). Machines very well in T7x tempers with sharp polished carbide, high speed and flood coolant; expect long chips and use chip-breaking geometry.

Can 7175-T7454 be welded?

Not readily — weldability is rated poor (20/100). Not arc weldable for structure (hot-cracking, SCC in HAZ); join by riveting, bolting, adhesive bonding or friction stir welding with process qualification.

What surface finishes work on 7175-T7454?

Chromic/sulfuric anodize, Type III hardcoat, chemical conversion coating (Alodine) plus primer; avoid caustic etch overexposure on close-tolerance machined parts.

Can 7175-T7454 be formed, bent or molded?

Forge/hot work at ~380–440 °C; cold forming in T-tempers is very limited — form in O or W temper and re-heat-treat.

What is the maximum service temperature of 7175-T7454?

7175-T7454 is rated for continuous use to about 120°C (248 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 7175-T7454?

Yes — 7175-T7454 is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets)The Aluminum Association (2018)
  2. AMS 4149 — Aluminum Alloy 7175 Die Forgings and Rolled Rings, T74SAE International (2018)
  3. ASTM B247 — Aluminum-Alloy Die, Hand and Rolled Ring ForgingsASTM International (2020)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  5. MMPDS — Metallic Materials Properties Development and StandardizationBattelle/FAA (2019)
  6. ASM Handbook Vol. 13B — Corrosion: MaterialsASM International (2005)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.