Nimonic 80/90, Used for Plate of Turbine Engine

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Basic Info

Payment Type:	T/T or L/C

Product Description

Product specifications:

The alloy belong to the basic Ni high temperature alloy through using aging strengthen
With taller Co and diversified chemical element, has higher strength of extension and capability of resisting creepage in 815-870° C, favourable resistance to oxidation and corrosion resisting, higher fatigue strength and well forming property and weldability at the condition of existing alternately impact repeatedly in cold and hot environment
Used for the plate of turbine engine, blade, high temperature fastener, clamp seal ring and elastic element

Chemical composition:

C: ≤0.13
Cr: 18-21
Co: 15-21
Al: 1.0-2.0
Ti: 2.0-3.0
Mn: ≤0.40
Si: ≤0.80
P: ≤0.015
S: ≤ .015
Pb: ≤0.0025
Cu: ≤0.2
B: ≤0.02
Fe: ≤1.5
Ni: balance

Available products and specifications:

Nimonic alloy 90 is designated as UNS NO7090 and Werkstoff Number 2.4632
Standard product forms are sheet, strip, plate, round bar, flat bar, forging stock, wire and extruded section
Rod, bar, wire and forging stock: BS HR2, HR501, HR502 and HR503, SAE AMS 5829, AECMA PrEN 2295, 2296, 2297, 2400, 2401, 2669 and 2670
Plate, sheet and strip: BS HR202, AECMA PrEN 2298
Pipe and tube: BS HR402, AECMA PrEN 2299

Our company and other products:

We have been specialized in production of alloy with a superior combination of heat resistance and high corrosion resistance
Our most competitive prodcuts such as: alloy 400, 625, 718, C276, C22, C4, 800, titanium alloy, as Inconel 600, 625, incoloy, Monel and more
If you are interested in our products or want to do OEM with us, please feel free to contract us

The alloy belong to the basic Ni high temperature alloy through using aging strengthen

With taller Co and diversified chemical element, has higher strength of extension and capability of resisting creepage in 815-870° C, favourable resistance to oxidation and corrosion resisting, higher fatigue strength and well forming property and weldability at the condition of existing alternately impact repeatedly in cold and hot environment

Used for the plate of turbine engine, blade, high temperature fastener, clamp seal ring and elastic element

C: ≤0.13

Cr: 18-21

Co: 15-21

Al: 1.0-2.0

Ti: 2.0-3.0

Mn: ≤0.40

Si: ≤0.80

P: ≤0.015

S: ≤ .015

Pb: ≤0.0025

Cu: ≤0.2