Mar-M 247(Ni-Co-W-Cr-Ta)


1. Introduce

– A nickel-base superheat-resistant alloy with polycrystalline solidification

– Alloys developed for applications requiring high strength at high temperatures up to about 1000℃

* Mar M : Cast polycrystalline nickel-based super heat-resistant alloy

* Mar : Ni-based alloys with improved high temperature strength by adding alloying elements such as Co, Cr, Ta, etc.

2. Property

– High strength, low thermal conductivity, creep and oxidation resistance, corrosion resistance, excellent work hardenability

ElementImpact
NiProvides excellent strength and corrosion resistance
CoPrecipitation strengthening element, provides strength, creep properties
WSolid solution strengthening element, provides high temperature creep properties
CrProvides corrosion resistance, oxidation resistance
TaProvides high temperature strength

[Mar-M 247 Chemical Composition (%)]

NiCrCAl
66.16 ~ 68.248.00 ~ 8.500.06 ~ 0.095.40 ~ 5.70
SiMnCoW
Max. 0.25Max. 0.109.00 ~ 9.509.30 ~ 9.70

[Mar-M 247 Mechanical Properties]

Tensile Strength
(Mpa)
Yield Strength
(Mpa)
Elongation
(%)
Anealed125075020

[Mar-M 247 Physical Properties]

Density
(g/㎤)
Melting Range
(℃)
7.801240 ~ 1330

3. Available Form

– Bar, Rod

– Sheet, Plate, Strip

– Wire, Coil

4. Application & Product

– Aerospace

ApplicationProduct
AerospaceCombustors, Turbine engine parts, High pressure turbine blades and vanes, Rotors, Disks, Turbocharger wheels, Turbopump turbine nozzles, Turbopump impellers

(1) Combustors / (2) Turbine engine parts / (3) Rotors

(4) Disks / (5) Turbocharger wheels / (6) Turbin blades

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