♦ Thead Size: M10-M120
♦ Length: according to clients drawing or specifaction
♦ Application for : Steam turbine generating equipment
♦ Grade: A Class
Haynes® 25 (L-605) is a cobalt based alloy that combines good forming and excellent high temperature properties. The alloy is resistant to oxidation and carburization to 1900 °F. Alloy 25 can only be hardened significantly by cold working. Cold working will increase creep strength up to 1800 °F and stress rupture strength uo to 1500 °F. Strain aging at 700 - 1100 °F improve creep and stress rupture strengths below 1300 °F.
Alloy |
% |
Ni |
Cr |
Co |
Mn |
Fe |
C |
Si |
S |
P |
W |
Haynes 25 |
Min. |
9.0 |
19.0 |
balance |
1.0 | - | 0.05 | - | - | - |
14.0 |
Max. |
11.0 |
21.0 | 2.0 | 3.0 | 0.15 | 0.4 | 0.03 | 0.04 | 16.0 |
Density
|
9.13 g/cm³
|
Melting point
|
1330-1410 ℃
|
Status
|
Tensile strength
Rm N/mm² |
Yield strength
Rp 0. 2N/mm² |
Elongation
As % |
Brinell hardness
HB
|
Solution treatment
|
960
|
340
|
35
|
≤282
|
AMS5759, AMS5537, ASTM F90, AMS 5796
Bar/Rod | Forgings | Strip/Coil | Sheet/Plate | Pipe/Tube |
AMS5759, ASTM F90 | AMS 5759 | AMS5537 | AMS5537 | GE B50T26A |
1. Medium endurance and creep strength below 815.
2. Excellent oxidation resistance below 1090℃.
3. Satisfactory forming, welding and other technological properties.
Haynes 25 has given good service in many jet engine parts. Some of these include turbine blades, combustion chambers, afterburner parts, and turbine rings. The alloy has also been used successfully in a variety of industrial furnace applications including furnace muffles and liners in critical spots in high temperature kilns.