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Curing - precision, stability and performance for your components

When hardening metals (precipitation or age hardening), a finely dispersed precipitation structure is created through targeted Heat treatment. This increases strength, yield strength and hardness and improves dimensional stability. Listemann supplies process-reliable solutions from sample production to series production.

The most important facts in brief

What is curing?

Hardening is a multi-stage Heat treatmentin which artificial ageing takes place after solution annealing and quenching. In this phase, very fine particles precipitate in the metal matrix (e.g. Mg₂Si, η′, Cu-rich phases). This microstructure blocks dislocations – the strength increases, toughness and dimensional stability remain adjustable.

Your advantages through curing

  • Significantly higher yield strength/strength with adjustable toughness

  • Dimensional and dimensional stability, reduced residual stresses

  • Weight reduction through thinner-walled, yet high-strength components

  • Reliability in operation (fatigue, corrosion under voltage)

  • Process reliability and traceability from batch to batch

Curing with Listemann

Design and manufacturing tips from Listemann

  • Determine alloy & condition selection at an early stage, e.g. heat treatment condition H925 for material 17-4PH

  • Design geometry & wall thicknesses for uniform through-heating; avoid sharp notches

  • Plan fixing/straightening for dimension-critical components

  • Coordinate subsequent processes (e.g. shot peening, coating, corrosion protection) with the curing plan

  • Define inspection planning (random samples, target values, release criteria) before the start of series production

Quality assurance by Listemann

  • Incoming goods & batch inspection (chemistry, microstructure, dimensions)

  • Temperature and time monitoring with multipoint thermocouples and data loggers

  • Documented oven qualification (uniform heating, calibration)

  • Mechanical tests (tensile, hardness, notched bar impact), dimensional inspection and microstructure analysis

  • Traceability back to the material batch and process parameters

Areas of application

stress-relief annealing aluminum air travel

Aviation & Aerospace

Structural and engine parts, connecting elements

Heat treatment Hardening Electronics & e-mobility

Automotive /
E-Mobility

Chassis and crash components, transmission components, shafts

hardening process hardening aluminum plant engineering mechanical engineering

Mechanical and plant engineering

High-strength housings, gear wheels, tool inserts

Medical Technology

Medical technology and sensor technology

Steel components with a defined strength/toughness balance

Formenbau Werkzeugbau

Tool & die-making

Temperature-resistant components

Additive manufacturing LMD

Additive manufacturing

Heat treatment for property adjustment and stress reduction

Materials and processes at a glance

Metallic hardening (precipitation hardening/aging)

Suitable alloys:

  • Hardenable stainless steels: precipitation hardening (e.g. 17-4PH and 15-5PH)
  • Maraging steels (Ni-martensitic hardenable)

  • Nickel and copper alloys with precipitation hardening system

  • Aluminum alloys: Al-Cu-Mg (2xxx), Al-Mg-Si (6xxx), Al-Zn-Mg-Cu (7xxx)

Procedure:

  • Solution annealing
    Dissolution of the curing-relevant elements and homogenization of the matrix.
  • Quenching
    Rapid cooling (e.g. air, oil, polymer, water) to “freeze” the dissolved state.

  • Artificial ageing (precipitation hardening)
    Isothermal holding for controlled precipitation formation (e.g. T6/T7 states for Al or H900-H1150 at 17-4PH).

  • Optional steps
    Relaxing/tempering, straightening/fixing, surface finish and final inspection.

Goals:

  • Strength/toughness balance
  • Dimensional stability
  • Targeted residual stress states

Frequently asked questions

Conventional hardening (austenitizing + quenching + tempering) produces a martensitic structure, especially in unalloyed/low-alloy steels. Precipitation hardening uses the finest precipitates in hardenable alloys (Al, PH steels, maraging, Ni/Cu) – the mechanism is microstructurally different.

For aluminium e.g. T6/T651/T7, for 17-4PH often H900-H1150, for maraging defined aging temperatures with subsequent mass stabilization.

By means of adapted ramps, suitable quenching media, symmetrical heating and fixtures; subsequent straightening/relaxing if necessary.

Tensile test (Rp₀,₂/Rm/A), hardness, microsection/SEM, dimensional and surface testing, optional residual stress measurement.

Areas of application

Project check

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