High-strength 2xxx and 7xxx aluminum alloys combine low density with demanding machining behavior: thermal distortion, adhesion, built-up edge, work hardening, cutting heat, and rapid tool wear. This guide covers carbide and DLC tool choices, rake, clearance and inclination angles, wear limits, high-speed cutting, feed selection, cooling, and aging treatments. Tables provide rapid-milling, end-milling, ball-nose, and 7055 example parameters while preserving the source’s tool grades, diameters, speeds, feeds, and depths of cut. Two unusual source values remain visible and are flagged for verification rather than silently corrected.
High-strength aluminum alloys are generally defined here as alloys with tensile strength above 480 MPa. They are primarily Al-Cu-Mg and Al-Zn-Mg-Cu alloys: the 2xxx duralumin series and the 7xxx ultra-high-strength series. The former has slightly lower static strength but a higher service temperature. Properties vary greatly with composition, melting and solidification practice, processing, and heat treatment.
Advances in alloy design, heat treatment, and microstructural control have steadily raised performance. Fifth-generation ultra-high-strength alloys with an engineering application base have progressed from roughly 600 MPa to about 750–800 MPa, and some research materials exceed 800 MPa.
Laboratory strength has surpassed 1 GPa. A study published in 2026 used severe plastic deformation by high-pressure torsion to refine A2024 grains to about 130 nm. Micro-tensile tests produced about 1,010 MPa tensile strength, 820 MPa 0.2% yield strength, and approximately 13% elongation at fracture. This indicates that advanced microstructural control can give conventional high-strength alloys the potential to reach 1 GPa.
These results rely mainly on special processes and microscale specimens and differ significantly from industrial plate, forgings, and extrusions. For practical engineering alloys, 750–800 MPa remains a more representative ultra-high-strength range; values above 1 GPa indicate the direction of advanced experimental research.
With low density, high strength, good machinability, and good weldability, these alloys are important in aerospace, marine, and civilian industries. The 7xxx alloy 7055 combines high specific strength, low density, weldability, and plastic formability and is widely used in aerospace and marine applications.
Machining Characteristics
Cutting readily generates thermal distortion, adhesion, and built-up edge.
A high coefficient of thermal expansion makes clamping and machining distortion likely, reducing dimensional accuracy.
High strength, specific stiffness, and hardness produce substantial plastic deformation during cutting and rapid tool wear.
Considerable cutting heat raises the cutting-zone temperature and aggravates tool wear.
Work hardening occurs readily.
Ways to Improve Machinability
Controllable factor
Recommended practice
Tool material
Select materials combining hardness, strength, toughness, wear resistance, oxidation resistance, and anti-adhesion properties, such as CoroMill 290 carbide, ZCC Cutting Tools KMG407, or a DLC-coated tool.
Tool design and geometry
Use high-speed solid end mills for pocket milling, primarily three-flute designs.
Keep the cutting edge sharp with a rake angle γ0 of about 10°.
Reduce friction and work hardening with clearance angle α0 > 8°–10°.
Strengthen the edge and control temperature with inclination angle λs = 30°–40°.
Set the wear limit VB at one-half the value used for a general-purpose tool.
Increase chip space appropriately in tools with enclosed chip pockets.
Cutting conditions
Use high-speed cutting in general: 800–3,000 m/min and 8,000–50,000 r/min spindle speed.
Avoid excessive feed, which overloads the cut, and feed that is too small, which makes the edge work within the hardened layer left by the preceding pass.
Cutting fluid and cooling
Use fluid with good cooling, lubrication, and penetration.
Direct the nozzle at the cutting zone; high-pressure or mist cooling is preferred.
Workpiece heat treatment
T6 aging, T6I4 aging, and retrogression aging can change machining behavior.
Note: The parameters above are recommendations from ZCC Cutting Tools.
Choosing Machining Parameters
High-strength aluminum alloys are primarily machined by milling.
Rapid Milling Parameters
Tool
Grade
v (m/min)
fz (mm), LH geometry
ae (mm)
Square-shoulder mill
YD101
300
0.08–0.4
≤0.5D
YD201
300
0.08–0.4
≤0.5D
Note: D is tool diameter; LH is the chip-breaker geometry.
End-Milling Parameters
Tool grade
Tool diameter D (mm)
1
2
3
4
5
6
8
10
12
14
16
18
20
AL-2E
Speed (r/min)
40,000
32,000
21,000
16,000
13,000
10,600
8,000
6,500
5,300
4,600
4,000
3,500
3,200
Feed (mm/min)
500
750
1,100
1,250
1,100
1,000
1,100
1,250
1,300
1,350
1,350
1,350
1,350
Maximum depth of cut
Side milling: ae = 0.1D, ap = 1.5D; slotting: ae = 1D, ap = 0.5D.
AL-3W
Speed (r/min)
—
—
—
—
—
10,600
8,000
6,500
5,300
4,600
4,000
3,500
3,200
Feed (mm/min)
—
—
—
—
—
1,900
1,900
1,850
1,700
1,650
1,600
1,550
1,500
Maximum depth of cut
Side milling: ae = 0.25D, ap = 1.5D; slotting: ae = 1D, ap = 1D.
Notes: These are ZCC Cutting Tools recommendations for side milling. For slotting, use 50%–70% of the listed speed and 40%–60% of the listed feed.
Ball-Nose Milling Parameters
Tool grade
Tool diameter D (mm)
φ2
φ3
φ4
φ5
φ6
φ8
φ10
φ12
AL-2B
Speed (r/min)
40,000
26,500
20,000
16,000
13,000
10,000
8,000
6,600
Feed (mm/min)
2,000
1,950
1,950
1,950
2,000
2,450
2,200
2,050
Maximum depth of cut
ae = 0.2D, ap = 0.1D.
Note: These parameters are recommendations from ZCC Cutting Tools.
Milling Example
Milling cutter
Workpiece
Tool material
v (m/min)
af (mm/tooth)
ap (mm)
γ0 (°)
Three-flute rapid mill
7055
KMG407
5
0.08
2
0–5
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