NIMONIC 86-SHANGHAI KANGSHENG AVIATION MATERIALS TECHNOLOGY CO., LTD.

NIMONIC 86

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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

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

TYPICAL MECHANICAL PROPERTIES