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Engineering · Heat Treatment

Heat treatment reference.

What each process does, when to use it, and how the typical alloys we machine respond. The guide for designers who need to spec heat treatment thoughtfully.

Why heat-treat

Same alloy, different part.

The same chemical composition can behave like soft butter or like a knife-edge — depending entirely on its thermal history. Heat treatment is how you tune properties to match the application: harder for wear, tougher for impact, more ductile for forming, more dimensionally stable for inspection.

The right heat treatment is usually decided early in the design phase — and called out explicitly on the drawing. Specifying "heat treat to 38–42 HRC" without naming the process leaves real ambiguity. Use the process names below.

The processes

Eight processes, distinct outcomes.

Process Goal Typical temp Cool from temp Best for
Annealing Soften, relieve all stress 705 – 870 °C Slow furnace cool Ferrous alloys before machining
Normalizing Refine grain, uniform structure 815 – 925 °C Air cool Castings, forgings, weldments
Stress relief Remove residual stress only 550 – 675 °C Slow Post-machining, post-welding
Hardening (quench) Form martensite, max hardness 815 – 870 °C Oil/water/polymer quench 4140, 4340, low-alloy steels
Tempering Trade hardness for toughness 150 – 650 °C Air cool Always after hardening
Solution treatment Dissolve precipitates uniformly Material-specific Water/air (alloy-specific) PH stainless, aluminum, Inconel
Precipitation aging Form strengthening precipitates 120 – 760 °C Air cool 17-4PH, 6061, 7075, Inconel 718
Case hardening Hard surface, tough core 850 – 950 °C + diffusion Oil quench, then temper Gears, shafts, low-carbon steels

Tempering curve · 4140 steel

Hardness drops as tempering temp rises.

Quenched 4140 hits ~57 HRC. That’s glass-brittle — useless without tempering. Each 100 °F of tempering trades roughly 1–5 HRC for toughness (about 3 HRC on average, steepest between 800–1000 °F). Pick the temper that gives the hardness AND toughness your application needs.

4140 hardness vs tempering temperature (1 hr soak, oil quench from 845 °C)
20 HRC 30 HRC 40 HRC 50 HRC 60 HRC 200 300 400 500 600 700 800 900 1000 1100 1200 Tempering temperature (°F) 57 56 54 52 50 47 44 40 35 31 28 Tools, dies Springs, blades Shafts, gears General machining Hardness (HRC)

Source: SAE AMS 6382, Carpenter datasheets. Other tempering times (2 hr, double-temper) shift the curve slightly. For 4340 or other Cr-Mo steels, the shape is similar with hardness 1–3 HRC higher across the range.

Solution treatment + aging

How precipitation-hardening alloys reach their strength.

Precipitation-hardening alloys (17-4PH, 6061, 7075, Inconel 718) follow a two-step thermal sequence: solution treat at high temperature (everything dissolves into solid solution), then age at moderate temperature (controlled precipitates form, locking strength in). Different aging temperatures for the same alloy yield different strength/ductility balances.

Material Solution temp Quench Common aging condition Result
17-4PH stainless 1040 °C Air or oil H900 — 482 °C, 1 hr UTS 1310 MPa, 44 HRC
17-4PH (tougher) 1040 °C Air or oil H1150 — 621 °C, 4 hr UTS 930 MPa, 33 HRC
Aluminum 6061 529 °C Water T6 — 175 °C, 8 hr UTS 310 MPa
Aluminum 7075 466 °C Water T6 — 121 °C, 24 hr UTS 572 MPa
Aluminum 7075 (SCC-resistant) 466 °C Water T73 — 107 °C/177 °C UTS 505 MPa, better SCC
Inconel 718 955 °C Air AMS 5663 — 720/620 °C UTS 1380 MPa
Ti-6Al-4V (STA) 955 °C Water STA — 540 °C, 4 hr UTS 1170 MPa

Process selection

Pick by what the part needs to do.

01

Need wear resistance

Through-hardened tool steel (A2, D2, S7) or surface-hardened low-carbon steel (carburized, nitrided). For corrosion + wear: hardened 17-4PH or 440C.

Hardness target — 50–62 HRC typical

02

Need impact toughness

Quenched and tempered alloy steel at moderate temper (4140 H, 4340). Avoid over-aging on PH alloys. Charpy V-notch is the right test.

Tempered above 540 °C / 1000 °F

03

Need fatigue resistance

Solution-treated and aged alloys. Avoid welds in fatigue zones. Surface-conditioning treatments (shot peen, ultrasonic peening) compound the gain.

Low residual surface stress; smooth finish

04

Need dimensional stability

Stress-relieve before final machining. For PH alloys, age before final tolerance grinding. For aluminum plate, T651 (stretch-relieved) is the right pick.

Stress relief 540–675 °C, slow cool

05

Need surface hardness with tough core

Carburize (low-carbon steel) or nitride (Cr-Mo alloy steel like 4140). Hardness 60+ HRC at the surface, core stays at the as-quenched-and-tempered hardness.

Case depth callout — typical 0.020–0.060″

06

Need maximum strength period

PH alloys at peak aging condition (17-4PH H900, 7075-T6, Inconel 718 STA). Note: peak strength = lowest ductility.

Lowest aging temp; full peak conditions

Watch out for

Heat treatment moves your part.

Every thermal cycle changes part dimensions. Quenching causes the most dramatic distortion (rapid, asymmetric thermal contraction). Aging is more predictable but still real. The general planning rules:

  • Rough machine before HT
    Leave 0.005–0.020″ stock on critical surfaces. Finish-machine or grind after HT.
  • Symmetric geometry distorts less
    Asymmetric clamping during quench amplifies distortion. Through-holes, flat plates, and thin-wall parts are the worst offenders.
  • Polymer quench beats water
    For 4140-class steels, polymer quench gives ~80% the hardness of water with ~½ the distortion. Worth specifying.
  • Aging is your friend
    PH alloys distort minimally during aging — ~0.0005″/inch dimensional change. Tighter tolerances can be held through aging vs. quenching.
  • Stress-relieve before tight tolerance ops
    Especially for thin-wall machining of plate stock. Aluminum plate that hasn't been stress-relieved (T6 vs T651) will spring after machining.

Spec syntax

How to call out heat treatment.

Don’t leave the spec ambiguous. Pick the AMS, MIL, or ASTM spec that matches your alloy and condition, and call out specific hardness/strength targets. Examples:

17-4PH per AMS 5643, condition H1025
→ Aged at 1025 °F. UTS 1070 MPa, 35–40 HRC.
4140 per AMS 6382, 28–32 HRC after tempering
→ Quench and tempered to a hardness window.
6061-T651 per AMS 4027
→ Solution treated, stretch-relieved, artificially aged.
Stress relieve at 595 °C ± 14 °C, 1 hr, slow cool
→ Process callout when no canonical AMS spec applies.

Technically reviewed by the True Precision Machining engineering team · Last reviewed June 2026

Standards referenced: AMS 6382, AMS 5643, AMS 5663, AMS 4027

Need help speccing heat treatment?

Send us your application and the property targets — we'll suggest the right alloy + condition combination and the standard spec to call out.

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