Super Alloy MP 159™ (UNS R30159)

Topics Covered

Introduction
Chemical Composition
Physical Properties
Mechanical Properties
Thermal Properties
Other Designations
Fabrication and Heat Treatment
     Cold Working
     Annealing
     Aging
Applications


Introduction

Super alloys contain many elements in a variety of combinations to obtain desired results. These alloys are good for use at high temperatures and severe mechanical stress, and also in cases where high surface stability is needed. Super alloys provide good creep and oxidation resistance.

Strengthening of super alloys is performed by work hardening, solid-solution hardening, and precipitation hardening methods. MP 159™ is a multiphase cobalt-nickel-chromium alloy with ductility, corrosion resistance, and ultra-high strength.

The following datasheet will provide more details about super alloy MP 159™.

Chemical Composition

The following table shows the chemical composition of MP 159™.

Element Content (%)
Cobalt, Co 35.7
Nickel, Ni 25.5
Chromium, Cr 19
Iron, Fe 9
Molybdenum, Mo 7
Titanium, Ti 3
Niobium, Nb 0.6
Aluminum, Al 0.2

Physical Properties

The physical properties of MP 159™ are outlined in the following table.

Properties Metric Imperial
Density 8.33 g/cm³ 0.301 lb/in³
Melting point 1427°C 2600°F

Mechanical Properties

The mechanical properties of MP 159™ are provided below.

Properties Metric Imperial
Tensile strength (annealed 1052°C) 848 MPa 123000 psi
Yield strength (at strain 0.200%, annealed 1052°C) 400 MPa 58000 psi
Elastic modulus (at 232°C/450°F,annealed) 208 GPa 30200 ksi
Shear modulus (at 232°C/450°F,annealed) 75.8 GPa 11000 ksi
Elongation at break (cold worked 48%) 12% 12%
Reduction of area 46% 46%

Thermal Properties

The thermal properties of MP 159™ are given below.

Properties Metric Imperial
Thermal expansion co-efficient (at 25-100°C/77-212°F) 14.3 µm/m°C 7.94 µin/in°F

Other Designations

Equivalent materials to MP 159™ are:

  • AMS 5841
  • AMS 5842
  • AMS 5843

Fabrication and Heat Treatment

Cold Working

MP 159™ is ductile in nature and capable of being cold worked using conventional methods.

Annealing

MP 159™ can be annealed at 1177°C (2150°F) and then rapidly air cooled.

Aging

The optimum hot tensile strength of the MP 159™ is enhanced by cold working (45-50% reduction of area) and aging at 663°C (1225°F) for 4 hours, which is then followed by air cooling.

Applications

MP 159™ is mainly used in gas turbine hot section components that are operated in high temperature environment of up to 649°C (1200°F).

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