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GH2132

 

GH2132 Oxidation-resistant Alloy Steel
1. Standard: GB/T14992-2005
2. Size: 0.4 ~ 4 * 1000 * 2000 mm
3. Chemical Composition: 
Ni: 24-27; Cr:13.5-16; Fe: balance ; Mo:1.0-1.5; P0.015 ; V:0.10-0.50; C:0.08; Mn:0.35; Si:0.35; S:0.002; Cu:0.3; Al:0.35; Ti:1.9-2.35
Application:Aircraft engine High-temperature load-bearing components such as turbine disks, compressor disk , rotor blades and fasteners.
4.Mechanical Properties:
Density: 7.99 g/cm3
Melting Point:1364-1424 C
Coefficient of Thermal Conductivity (/(W/m•C) ): 14.20 (100C).
Linear Expansibility (a/10-6C-1 ): 15.70 (20~100C )
Heat Treatment: Solution Treatment
Tensile Strength( b/MPa ):  930 MPa (at 20 C), 
Yield Strength:  590 Mpa    
Elongation( 5 /%):  15% (at 20 C),  
Hardness:341 HBS
5. Production Time: 50~60 days after getting your firm order
6. Payment Terms:T/T or L/C at sight.

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