Product Description
A nickel-chromium-molybdenum alloy with a rare-earth (cerium) addition. It combines good formability and weldability with exceptional resistance to oxidation and scaling at temperatures to 1920°F (1050°C). Used in gas turbines for sheet-metal fabrications such as combustion chambers and afterburners and in heat-treating furnaces.
STANDARD PRODUCT FORMS
Sheet, strip, plate, round bar, forging stock, extruded sections and wire.
MAJOR SPECIFICATIONS
None applicable.
LIMITING CHEMICAL COMPOSITION, %
Nominal
Ni ......................65
Cr ..................25.0
Mo .................10.0
Ce .................0.03
C ....................0.05
Ni ......................65
Cr ..................25.0
Mo .................10.0
Ce .................0.03
C ....................0.05
PHYSICAL CONSTANTS AND THERMAL PROPERTIES
Density, Ib/in3 ........................................................................0.309
g/cm3 .........................................................................8.54
Young's Modulus, 10 6 psi .....................................................30.5
GPa ...........................................................210
Coefficient of Expansion, 68 – 212°F, 10-6 in/in • °F........7.1
20 – 100°C, µm/m • °C .........12.7
g/cm3 .........................................................................8.54
Young's Modulus, 10 6 psi .....................................................30.5
GPa ...........................................................210
Coefficient of Expansion, 68 – 212°F, 10-6 in/in • °F........7.1
20 – 100°C, µm/m • °C .........12.7
TYPICAL MECHANICAL PROPERTIES

previous
next
previous
next
Key words:
Related Products
Online message
SHANGHAI KANGSHENG AVIATION MATERIALS TECHNOLOGY CO., LTD.
Address: No. 5999, Huyi Road, Waigang Town, Jiading District, Shanghai
Tel:13641813331
Technical support:13671903676
Emial:ksalloy@ksalloy.com
Copyright: 2022 Shanghai Kangsheng Aviation Materials Technology Co., Ltd.
Powered By:www.300.cn SEO