GH4202

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1. Introduction to GH4202 Materials

      GH4202 is a Ni-Cr-based precipitation hardened deformation high-temperature alloy with a temperature of -253-800 degrees Celsius. The alloy is added with tungsten and molybdenum elements for solid solution strengthening, aluminum and titanium elements are added to form an aging reinforced phase, and a small amount of boron and cerium elements are added to purify and strengthen the grain boundaries. The alloy has good comprehensive mechanical properties and stable structure. The alloy has high corrosion resistance and oxidation resistance, as well as good oxygen-rich corrosion resistance. This alloy is a typical multi-purpose high temperature alloy material.

2. GH4202 chemical composition

合金 % C Cr アル W フェ 铈 What B S P そして ムン
GH4202 最小値 17.0 マージン 1.0 2.2 4.0 4.0
最大値 0.08 20.0 1.5 2.6 0.07 5.0 5.0 4.0 0.01 0.01 0.010 0.015 0.60 0.50

3. GH4202 physical properties

Density g/cm³ マグネティック Thermal conductivity/w/(mk)100-800℃ Resistivity ℃)/(Ω.mm2/m)100℃ Specific heat capacity ℃)/kg/(kg.k)℃25-800℃ Linear expansion coefficient/(10-6/k)20-700℃
8.36 none 12.2-28.8 14.8
Temperature 0/℃ 20 600 700  
Elastic modulus E/GPa 216 182 173

 4. GH4202 Mechanical Properties

タイプ Heat treatment Temperature 0/°C 引張強さ

ΣbMPa≥

Elongation A/%≥ Section shrinkage Z/%≥
Round stick 固溶体状態 20 930 16 18

V. GH4202 application fields

      The new high-thrust liquid rocket engine has dozens of components such as turbine rotor, rectifier gate, turbine ball shell, corrugated pipe and gas pipeline, and is in good use.

      It is promoted and applied to aviation, nuclear energy, petroleum and chemical industries, and requires high corrosion resistance and chemical resistance to heat-resistant bearing parts and welded parts.

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