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  • Home
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  • materials
    • Stainless Steel
      • 430 / 1.4016
      • 420 / 1.4021
      • 420 / 1.4034
      • 431 / 1.4057
      • 440B / 1.4112
      • 420F / 1.4197
      • 304 / 1.4301
      • 305 / 1.4303
      • 304L / 1.4307
      • 301LN / 1.4318 / UNSS30153
      • 316l-14404/
      • 316l-14435
      • 316L / 1.4435WCQ
      • 1.4435/1.4441WCQ+
      • 316LVM / 1.4441
      • 444 / 1.43521N
      • 321-14541
      • 13-8-ph-14534
      • XM-12 / 1.4545 / 15-5 PH
      • 17-4 PH / 1.4542
      • 316Ti / 1.4571
      • 309 / 1.4828
      • 314 / 1.4841
    • Special Stainless Steel
      • P2000 / 1.4452
      • 318LN / 1.4462
      • SUPER DUPLEX S32760 / F55 / 1.4501
      • 6Mo / 1.4529
      • Alloy 904L / 1.4539
      • Alloy 254 SMO / 1.4547 / UNS S31254
      • Alloy 31 / 1.4562
      • Alloy 24 / 1.4565
      • Alloy 800H / 1.4876
    • Nickel Alloys
      • Alloy 201 / 2.4068
      • Alloy 400 / 2.4360
      • Alloy C22 / 2.4602
      • Alloy 59 / 2.4605
      • Alloy C4 / 2.4610
      • Alloy 602CA / 2.4633
      • Alloy X / 2.4656 / UNS N06002
      • Alloy 617 / 2.4663
      • Alloy 718 / 2.4668
      • Nivaflex / 2.4782
      • Alloy C276 / 2.4819
      • Alloy 601 / 2.4851
      • Alloy 625 / 2.4856
      • Alloy 825 / 2.4858
    • Titanium Alloys
      • Ti Gr 1 / 3.7025
      • Ti Gr 2 / 3.7035
      • Ti Gr 4 / 3.7065
      • TiGr5 / Ti6AI4V / AMS4911
      • Ti Gr 23 / 3.7165ELI
      • Ti Gr 7 / 3.7235
      • Ti Gr 9 / 3.7194
      • Titan Grade 12 / 3.7105 / UNS N53400
      • 367 / Ti6AL7Nb
      • Titan-15Mo
      • Ti6Al2Sn4Zr6Mo / Ti-Gr-6-2-4-6
      • Ti 6Al-6V-2Sn
    • Exotic Metals
      • P900 / 1.3816
      • Cronidur 30 / 1.4108
      • Zirconium / Zr 702
      • MP35N / NiCoCrMo
      • 5832-4 / CoCrMo
      • Nitinol
      • Tantalum
      • Tungsten
      • REX-734
      • X35 ST +
      • CuBe 2 Pb – AM173
      • Kovar (Nilo®, Alloy K) / 1.3981 / UNS K94610
      • Invar 36 (FeNi36) / 1.3912
      • Invar 42® (alloy 42, Nilo 42®) / 1.3917 / UNS K94100
      • Bronze CuAl AMPCO18®
  • Industries
    • Medical Technology
    • Plant and Apparatus Construction
    • Titanium in Aerospace
    • Titanium in Defence and Protection
    • Titanium for Mechanical Workshops
    • Titanium Semi-Finished Products in the Automotive Industry
    • Titan in Hydrogen Technology
    • Supplier of Semi-Finished Products for Surface Technology
    • Titanium Semi-Finished Products for Daily Life
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13-8-ph-14534

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  • Application
  • Composition
  • Application
  • Composition

13-8 PH / 1.4534

13-8 PH is a martensitic precipitation-hardening stainless steel. This alloy is double melted in a Vacuum Induction Furnace followed by Consumable Electrode Vacuum Melt (VIM-VAR); or in some instances the 2nd melt is by Electro slag Re-melting (ESR) as specified by the consumer. This Alloy exhibits excellent strength, high hardness, superior toughness, combined with good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. 13-8 PH steel provides a wide range of properties through a single precipitation hardening heat treatment.

 This Alloy can be welded providing the use of an inert gas shielding ,Helium is preferred. Corrosion resistance is similar to 304 Stainless, with the greatest resistance in the fully hardened conditions.

Main fields of application of 1.4534

Applications include aircraft structural parts, landing gear components, shafts, valves, fittings and fasteners. Also used for components in the petrochemical industry.

Chemical composition of 1.4534

Cr12,25 - 13,25Si≤ 0,10
Ni7,5-8,5Mn0,10
Ai0,8-1,35P0,01
C≤ 0,05S0,008
Mo2,00-2,50N0,010
Ti0,10

Heat treatment

The key properties of Precipitation Hardened steels comes from the heat treatments , below is a short table showing the types of mechanical results obtainable through heat treatment.

Mechanical Properties

conditionTensile0.2% YieldElongationReduction of areaHardness BrinelHardness Rockwell
H950175.000205.0001054363C45 min
H1000 220.000190.0001050C45 min
H1025205.000175.0001150
H1050185.000165.0001250C40 min
H1100150.000135.0001450C34 min
H1150135.00090.0001450C30 min

Alloy 13-8PH Precipitation Hardening Alloy is produced in the annealed condition. This is also referred to the solution heat treated condition, or Condition A. Solution treat from 1675 to 1725°F (910 to 940°C) for 15 to 30 minutes at temperature. Air cool or oil quench to below 60°F (15°C) to effect complete transformation to martensitic. Aging is normally carried out from 950 to 1150°F(510 to 620°C), depending upon the desired final properties. Heat treatment is usually performed in air. Reducing atmospheres should not be used because of the potential for hydrogen contamination.

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