PROPRIETARY Custom 465 Stainless Stainless steels

Material group: Ferrous Alloys / Stainless steels
Country / Standard: PROPRIETARY

Data updates

Latest Update: 2016-01
Total number of updates: 3
Update History
2015-01 2014-07

This material has 439 properties — only a subset is shown here.

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PROPRIETARY Custom 465 Stainless Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
C
VALUE
≤ 0.02
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
11.00 – 12.50
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Fe
VALUE
Balance
UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Mo
VALUE
val1
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UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
Ni
VALUE
val1
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UNIT
%
CAS NUMBER
7440-02-0
CRITERIA
P
VALUE
val1
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UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6

Carpenter Technology Corporation, Product Data Sheets,

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PROPRIETARY Custom 465 Stainless Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
190 — 215 GPa
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Electrical Resistivity
0.771 — 0.946 Ω∙mm²/m
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Thermal Conductivity
14.07 — 15.83 W/(m∙°C)
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Density
val1
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kg/dm³
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Electrical Conductivity
val1
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S/m
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Poisson Coefficient
val1
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This material has 439 properties — only a subset is shown here.

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PROPRIETARY Custom 465 Stainless Heat Treatments


  • Solution Annealed: Heat to 982°C ± 8°C, hold one hour at heat and cool rapidly. Sections up to 304.8 mm can be quenched in a suitable liquid quenchant. Sections over 304.8 mm should be cooled rapidly in air. For optimum aging response, solution annealing should be followed by refrigerating to -73°C, holding eight hours, then warming to room temperature (CT). Subzero cooling should be performed within 24 hours of solution annealing. Custom 465 stainless normally will be supplied from the mill in the solution annealed/cold treated condition (annealed/CT), ready for the one-step hardening treatment. Billet product will be provided in the hot finished condition. Aged (Condition H900, H950, H1000, H1050 and H1100): The high strength levels are derived from a single age hardening step consisting of heating to a selected temperature between 482/621°C and holding for four to eight hours. A water or oil quench is suggested for optimum toughness. Slower cooling methods are not preferred, and are likely to result in reduced toughness. Aging temperature will depend upon the desired combination of strength, toughness and stress corrosion cracking resistance. While the alloy does develop maximum strength after a 482°C age, it is not recommended because toughness is significantly degraded compared to aging at higher temperatures. The best combination of properties is obtained after aging at 482°C and above and quenching in a suitable liquid, the severity of which should in part be based on the geometry and complexity of the part being aged. Condition H1150M: While the alloy typically will be machined in the annealed/CT condition, optimum machinability can be achieved by overaging to the H1150M condition. Material is heated to 760°C ± 8°C for two hours, air cooled, then reheated to 621°C ± 8°C for four hours and air cooled. If this practice is used, parts must be reannealed at 982°C, cold treated at -73°C and aged at a selected temperature.

PROPRIETARY Custom 465 Stainless Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
951 — 2089 MPa
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Elongation, A
val1
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%
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Rockwell Hardness (HR)
val1
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Yield Strength, Rp0.2
val1
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MPa
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Impact Energy
val1
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J
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Reduction of Area
val1
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%
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PROPRIETARY Custom 465 Stainless International Equivalent Materials


Showing 3 of 12 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit

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  • 12Cross References

  • 10Composition
  • 255Mechanical Properties
  • 71Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • 51Stress-Strain
  • -Formability
  • 4Fatigue
  • 15Fracture
  • -Creep

  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology

  • -Corrosion
  • 16Ageing
  • -Weatherability
  • -Irradiation

  • 4Total Suppliers