MONEL
INCONEL
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AEETHER

INCOLOY
HASTELLOY
UNS N06002

Hastelloy Alloy
X

W.Nr. 2.4665
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Introduction
Main Standards
Chemical Composition
Data Sheet
Applications
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Introduction

logo of solid solution strengthened alloy

Solid Solution
Strengthened Alloy

Nickel
Chromium
Iron
Molybdenum
Corrosion
Resistance
84
Mechanical
Behavior
70
Purity
84

High Temperature Characteristics

Strength &
Stability

Oxidation
Resistance

Carburization
Resistance

Sulfidation
Resistance

Nitriding
Resistance

Carbonitriding
Resistance

Resistance to
Molten Salts

Overview

As a leading supplier & manufacturer in China, AEETHER supply cost-effective Hastelloy X Products.

HASTELLOY® X alloy (UNS N06002 (W86002) is a nickel-chromium-iron-molybdenum alloy that possesses an exceptional combination of oxidation resistance, fabricability and high-temperature strength. It has also been found to be exceptionally resistant to stress-corrosion cracking in petrochemical applications. X alloy exhibits good ductility after prolonged exposure at temperatures of 1200, 1400, 1600°F (650, 760 and 870°C) for 16,000 hours.

HASTELLOY® X alloy has excellent forming and welding characteristics. It may be forged or otherwise hot-worked, providing it is held at 2150°F (1177°C) for a time sufficient to bring the entire piece to temperature. As a consequence of its good ductility, HASTELLOY® X alloy is also readily formed by cold-working. All hot- or cold- worked parts should be annealed and rapidly cooled in order to restore the best balance of properties. The alloy can be welded by a variety of techniques, including gas tungsten arc (GTAW), gas metal arc (GMAW), shielded metal arc (SMAW), and resistance welding.

HASTELLOY® X® alloy is available in the form of plates, sheets, strips, billets, bars, wires, pipes, tubes, and covered electrodes. Applications include P2O5 evaporator tubes.

Heat-Treatment

Wrought forms of HASTELLOY® X alloy are furnished in the solution heat-treated condition unless otherwise specified. X alloy is typically solution heat-treated at 2150°F (1177°C) and rapid cooled. Bright annealed products are cooled in hydrogen. Annealing at temperatures lower than the solution heat- treating may cause precipitation of secondary phases, which may affect the alloy’s strength and ductility.

Useful for Aircraft, Furnace and Chemical Process Components

X alloy has wide use in gas turbine engines for combustion zone components such as transition ducts, combustor cans, spray bars and flame holders as well as in afterburners, tailpipes and cabin heaters. It is recommended for use in industrial furnace applications because it has unusual resistant to oxidizing, reducing and neutral atmospheres. Furnace rolls of this alloy were still in good condition after operating for 8,700 hours at 2150°F (1177°C). HASTELLOY® X alloy is also used in the chemical process industry for retorts, muffles, catalyst support grids, furnace baffles, tubing for pyrolysis operations and flash drier components.

Specifications

HASTELLOY® X is covered by ASME Section VIII, Division 1. Plate, sheet, strip, bar, forging, tubing, pipe, and fittings are covered by ASME specifications SB 366, SB 435, SB 572, SB 619, SB 622, and SB 626 and ASTM specifications B 366, B 435, B 572, B 619, B 622, and B626. The UNS number for the alloy is N06002. DIN designations are No. 2.4665 and NiCr22Fe18Mo. Sheet, strip, and plate are also covered by AMS specification 5536, and billet and bar are covered by AMS 5754.

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Main Standards

ASTM B622
Seamless Pipe & Tube
ASTM B619
Welded Pipe & Tube
ASTM B626
Welded Pipe & Tube
ASTM B366
Fittings
ASTM B472
Billet, Rod and Bar
ASTM B572
Billet, Rod and Bar
ASTM B435
Plate, Sheet and Strip
SAE AMS 5754
Billet, Rod, Bar and Forging
SAE AMS 5536
Plate, Sheet and Strip
AWS A5.14 ERNiCrMo-2
Filler Metal
AWS A5.11 ENiCrMo-2
Welding Electrode

Chemical Composition

Data Sheet

Physical Properties

Density g/cm3 8.22
lb/in.3 0.297
Melting Range °F 2300 - 2470
°C 1260 - 1355
Poisson’s Ratio 0.32
Magnetic Permeability 200 oersted 1.002

Mechanical Properties

Test Temperature Yield Strength
(0.2% Offset)
Tensile Strength Elongation
°F °C ksi MPa ksi MPa %
Plate
70 21 49.3 340 110.2 760 48.9
1000 538 32.5 224 87.6 604 60.2
1200 649 30.7 212 80.9 558 63.5
1400 760 31.6 218 61 421 74.5
1600 871 27.4 189 37 255 98.1
1800 982 13.6 94 20 138 98.1
2000 1093 6.5 45 10.4 72 95.3
Sheet
70 21 54.5 376 113.5 783 46.5
1000 538 36.7 253 91 628 53.6
1200 649 34.9 241 84.2 580 65.5
1400 760 33.8 233 61.6 424 95.6
1600 871 28 193 36.5 251 117.9
1800 982 12.8 88 18.9 130 81.5
2000 1093 6.2 43 9.5 65 50.6
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Applications

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