Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate

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Customization: Available
Surface Treatment: Polishing
Shape: Sheet
Manufacturer/Factory, Group Corporation
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  • Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
  • Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
  • Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
  • Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
  • Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
  • Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
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  • Overview
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Overview

Basic Info.

Model NO.
Hastelloy X Sheet/Plate
Color
Bronze
Material
Nickel
Key Words
Hastelloy X Plate/Sheet
Thickness
2mm - 100mm
Length
as Your Requirments
Diameter Tolerance
H9, H11, H13, K9, K11, K13 etc
Sample
Free-Sample
Surface
Lack, Peeled, Polishing, Bright, Sand Blast, Hl
MOQ
100kgs
Stock
in Stock
Transport Package
Wooden Package
Specification
Hastelloy X
Trademark
LORK
Origin
China
HS Code
7219350000
Production Capacity
50000kg/Month

Product Description

Product Description

Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X PlateBest New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate

Introduction

HASTELLOY X is a wrought nickel base alloy with excellent high temperature strength and oxidation resistance. All of the product forms are excellent in terms of forming and welding. Although HASTELLOY X is primarily noted for heat and oxidation resistance it also has good resistance to chloride stress-corrosion cracking and has good resistance to carburization, excellent resistance to reducing or carburizing atmospheres. Alloy X is one of the most widely used nickel base superalloys for gas turbine engine components.

AMS 5754 has no yield or tensile strength requirements, but it does require a hardness maximum and stress rupture minimums. Strong and Oxidation Resistant to 2200 Deg. F (1200 Deg. C) - HASTELLOY X is a solid solution strengthened grade has good strength and oxidation resistance up to 2200 Deg. F (1200 Deg. C).


Composition

The chemical composition of HASTELLOY(r) X alloy is outlined in the following table.

Element Content (%)
Cr, Chromium 20.5-23
Fe, Iron 17-20
Mo, Molybdenum 8-10
Mn, Manganese 1 max
Si, Silicon 1 max
Ti, Titanium 0.15 max
Co, Cobalt 0.5-2.5
Al, Aluminum 0.5 max
Cu, Copper 0.5 max
C, Carbon 0.05-0.15
P, Phosphorus 0.04 max
S, Sulfur 0.03 max
W, Tungsten 0.2-1
B, Boron 0.008 max
Ni, Nickel Remainder
 
 


Grade Specification

Grade UNS DIN EN AMS ASTM JIS
Hastelloy X

N06002

2.4665
2.4603
  AMS 5588
AMS 5587
AMS 5754
AMS 5536
AMS 5798
ASTM B435
ASTM B572
ASTM B619
ASTM B366

ASTM B622
ASTM B626
-


 

Physical Properties

The following table shows the physical properties of HASTELLOY(r) X alloy.

Properties Metric Imperial
Density 8.220 g/cm³ 0.297 lb/in³
Melting point 1316°C 2400°F


Mechanical Properties

The mechanical properties of HASTELLOY(r) X alloy are displayed in the following table.

Properties Metric Imperial
Tensile strength 755 MPa 109.5 Ksi
Yield strength 385 MPa 55.9 Ksi
Elastic modulus 205 GPa 29.8 psi
Reduction of area 22% 22%
Hardness, Rockwell B (converted from Brinell hardness) 87 87


Thermal Properties

The thermal properties of HASTELLOY(r) X alloy are given in the following table.

Properties Metric Imperial
Thermal expansion co-efficient 13.0 µm/m°C 7.2 µin/in°F
Thermal conductivity 9.1 W/mK 63 BTU in/hr.ft².°F




Characteristics

Resistance to oxidation
The outstanding oxidation resistance of HASTELLOY X is illustrated below. Tests were conducted by exposing samples to dry air at 2000 Deg. F. and to dry air pressurized to 300 psi at 1750 Deg. F. Two criteria for evaluating oxidation resistance are weight change and depth of corrosion penetration. HASTELLOY X excels in both respects due to the formation of a protective, tenacious oxide film.

Reaiatance to carburization and nitrding
HASTELLOY X also resists carburization and nitriding, two common conditions which often lead to early failure in high-temperature alloys. After 100 hours in petroleum coke, four other materials were completely penetrated by carburization; whereas, Alloy X specimens showed no carburization at all. Of ten materials evaluated in an atmosphere of hydrogen, nitrogen and ammonia at 1100 Deg. F. and 25,00 psi for 64 days, Alloy X had a nitride case less than one-fourth as thick as the closest competitive material without intergranular attack.




Technology

Cold Working

HASTELLOY(r) X alloy can be readily cold worked and requires a large amount of forming pressure due its high stiffness characteristic. Solution annealing can be performed after this alloy is cold worked.

Welding
Welding processes suitable for HASTELLOY(r) X alloy include shielded metal arc welding, resistance welding and TIG or MIG. Usage of a corresponding filler metal is recommended whereas post heating and preheating are not recommended.

Forging
Conventional methods are used for hot forging HASTELLOY(r) X alloy.

Forming
Standard processing and tooling methods are used for forming different product forms of HASTELLOY(r) X alloy.

Machinability
Conventional methods are used for machining HASTELLOY(r) X alloy.

Hardening
HASTELLOY(r) X alloy can be hardened by cold working and to a limited extent by aging. This alloy cannot be hardened by the standard heating methods.

Heat Treatment
HASTELLOY(r) X alloy is mostly solution annealed at 1177°C (2150°F) and then cooled rapidly.

Aging
HASTELLOY(r) X alloy is first solution heat treated and then aged at 649-871°C (1200-1600°F). Increase in hardness and strength can be obtained when this alloy is under the aging temperature for prolonged hours.

 
 

Hastelloy X Standards

Seamless Pipe & Tube Welded Pipe & Tube Fittings Billet, Rod and Bar Forgings Plate, Sheet and Strip
ASTM B622 AMS 5588
ASTM B619
ASTM B366 AMS 5754
ASTM B572
AMS 5754 AMS 5536
ASTM B435



Applications

HASTELLOY X finds use in petrochemical process equipment and gas turbines in the hot combustor zone sections. Also used for structural components in industrial furnace applications because of the excellent oxidation resistance.

HASTELLOY X is recommended especially for use in furnace applications because it has unusual resistance to oxidizing, reducing, and neutral atmospheres. Furnace rolls made of this alloy were still in good condition after operating for 8700 hours at 2150 Deg. F. Furnace trays, used to support heavy loads, have been exposed to temperatures up to 2300 Deg. F. in an oxidizing atmosphere without bending or warping. Alloy X is equally suitable for use in jet engine tailpipes, afterburner components, turbine blades, nozzle vanes, cabin heaters, and other aircraft parts.

Gas turbine combustion cans and ducting, heat-treating equipment.

Alloy X has wide use in gas turbine engines for combustion zone components such as transition duct, 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 resistance to oxidizing, reducing and neutral atmospheres. Furnace rolls of this alloy were still in good condition after operating for 8,700 hours at 2150 degrees F (1177 degrees C). HASTELLOY X is also used in the chemical process industry for retorts, muffles, catalyst support grids, furnace baffles, tubing for pyrolysis operations and flash drier components.

Useful Properties for Aircraft and Furnace Parts - HASTELLOY X is recommended especially for use in furnace applications because it has unusual resistance to oxidizing, reducing, and neutral atmospheres. Furnace rolls made of this alloy were still in good condition after operation for 8,700 hours at 2150 Deg. F (1177 Deg. C).

 

Surface Treatment

 

Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
 
 

Processing

Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
 

Packaging & Shipping


Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate
Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate

Company Profile


Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate

FAQ

Best New Products N06002/2.4665/AMS 5587/ASTM B619 Nickel Alloy Sheet for Jet Engine Tailpipes Aerospace Materials Hastelloy X Plate

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