ASTM B729 UNS N08020/N08024 SMLS
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ASTM B729 UNS N08020/N08024 SMLS

Nickel-based alloy tube is an alloy composed of nickel and other elements (such as drill, chromium, iron, etc.), which has excellent corrosion resistance, high strength and high temperature stability, so it is also known as "corrosion resistant alloy tube". In low temperature, moderate and high temperature environment, the performance of nickel-based alloy pipe is very stable, with good oxidation resistance, corrosion resistance and heat resistance, greatly improving the service life of the pipeline system.
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Gnee Steel (Tianjin) Co., Ltd. is one of the most professional astm b729 uns n08020/n08024 smls manufacturers and suppliers in China. Welcome to wholesale customized astm b729 uns n08020/n08024 smls at competitive price from our factory. Good service and quality products are available.

 

N08020/N08024 Products Description

Let me introduce you to ASTM B729 UNS N08020/N08024 SMLS.

Alloy 20, also known as Carpenter 20, is a nickel-iron-chromium austenitic alloy developed for maximum resistance to acid attack, particularly sulfuric acid. In chemical media such as chloride, phosphoric acid, and nitric acid, the alloy has good resistance to complete corrosion, pitting corrosion, and crack corrosion. In addition, the alloy contains niobium, which is stable against sensitization and intergranular corrosion. Alloy 20 contains 33% nickel and shows some resistance to chloride stress corrosion cracking. This material is commonly used to solve the stress corrosion cracking (SCC) problem in 316 L stainless steel.

 

N08024 and aluminum alloy have the characteristics of light weight, high compressive strength, strong temperature resistance, corrosion resistance and so on. In the aerospace industry, it is used to manufacture aircraft engines and integral airframes. When it is used to replace other metal materials in aviation engineering, it can not only extend the service life of the airport, but also alleviate its net weight, and further improve its navigation characteristics, so it is one of the/promising structural raw materials in the aerospace industry and the space and space industry.

 

N08020/N08024 Chemical Composition
Grade UNS C≤ Mn≤ P≤ S≤ Si≤ Ni Cr Mo Cu
Alloy 20 N08020 0.07 2 0.045 0.035 1 32.0-38.0 19.0-21.0 2.0-3.0 3.0-4.0
Alloy 24 N08024 0.03 1 0.035 0.035 0.5 35.0-40.0 19.0-21.0 3.5-5.0 0.5-1.5

 

N08020/N08024 Mechanical Property
Mechanical properties Tensile, min, ksi[MPa] Yield, min, ksi[MPa] Elongation, %(min)
Alloy 20 80[551] 35[241] 30

 

Mechanical properties YIELD
RP0.2 (MPA)
TENSILE
RM (MPA)
IMPACT
KV/KU (J)
ELONGATION
A (%)
REDUCTION IN CROSS SECTION ON FRACTURE
Z (%)
AS-HEAT-TREATED CONDITION BRINELL HARDNESS (HBW)
Alloy 24 452 (≥) 296 (≥) 33 34 44 Solution and Aging, Annealing, Ausaging, Q+T,etc 241

 

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