Description
Incoloy A-286 /UNS S66286
GB GH2132 Material grades and equivalents
GB GH2132 / Incoloy A-286 / UNS S66286 / EN 1.4980/ AFNOR ZbNCT25/Gr.660
GB GH2132 Chemical composition:
Alloy |
% |
Ni |
Cr |
Mo |
B |
Fe |
Al |
Ti |
C |
Mn |
Si |
V |
S |
GH 2132 |
Min. |
24 |
13.5 |
1.0 |
0.001 |
1.9 |
0.1 |
||||||
Max. |
27 |
16 |
1.5 |
0.01 |
Rest |
0.35 |
2.35 |
0.08 |
2.0 |
1.0 |
0.5 |
0.03 |
GB GH2132 Physical properties:
Density |
7.93 g/cm3 |
Melting point |
1364-1424℃ |
GH2132 minimum mechanical properties in the room temperature:
Status |
Tensile strengthRm N/mm2 |
Yield strengthRP0.2N/mm2 |
ElongationA5 % |
GH2132 |
950 |
680 |
28 |
An alloy that is precipitation hardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The alloy’s high strength and excellent fabrication characteristics make it useful for various components of aircraft and industrial gas turbines. Applications include blades, vanes, shafts, tail cones, afterburners, springs, and fasteners. This alloy is also used for automotive applications.
GB GH2132 Application fields:
-
Jet engine, gas turbine and turbocharger components
-
High temperature fasteners, springs
-
High magnetic low temperature equipment
Specifications:
Rod, Bar, Wire and Forging Stock |
ASTM A 638;ASME SA 638;SAE AMS 5726;SAE AMS 5731;SAE AMS 5732;SAE AMS 5734;SAE AMS 5737;SAE AMS 5895;BS HR 51;BS HR 52;AECMA PrEn2171;AECMA PrEN2119;AECMA PrEN2172;AECMA PrEN2173;AECMA PrEN2174;AECMA PrEN2303;AECMA PrEN2304;AECMA PrEN2398;AECMA PrEN2399;AECMAPrEN3510 |
Plate, Sheet and Strip |
SAE AMS 5525;SAE AMS 5858;AECMA PrEN2175;AECMA PrEN241 |
Pipe & Tube |
SAE AMS 5731;SAE AMS 5732;SAE AMS 5734;SAE AMS 5737;SAE AMS 5895 |