Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate

Product Details
Customization: Available
Surface Treatment: Polishing
Shape: Sheet
Manufacturer/Factory, Group Corporation
Diamond Member Since 2024

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  • Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
  • Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
  • Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
  • Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
  • Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
  • Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
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  • Overview
  • Product Description
  • Surface Treatment
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  • Company Profile
  • FAQ
Overview

Basic Info.

Model NO.
Hastelloy S Sheet/Plate
Color
Bronze
Material
Nickel
Key Words
Hastelloy S 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 S
Trademark
LORK
Origin
China
HS Code
7219350000
Production Capacity
50000kg/Month

Product Description

Product Description

Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S PlateWholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate


Introduction

HASTELLOY® S alloy (UNS N06635) is a nickel-base, high-temperature alloy with a unique combination of properties. It has excellent thermal stability, low thermal expansion and excellent oxidation resistance to 2000°F (1093°C). In addition, the alloy has good high-temperature and thermal fatigue strength. S alloy retains its strength and ductility after aging at temperatures of 800 to 1600°F (427 to 871°C).

S alloy was developed for applications involving severely cyclical heating conditions where components must be capable of retaining their strength, ductility, and metallurgical integrity after long-time exposure. It is used extensively as seal rings in gas turbine engines where its low thermal expansion coefficients is also important.

All wrought forms of S alloy are supplied in the solution heat treated condition unless otherwise specified. The standard heat-treatment is 1950°F (1066°C) followed by cooling in air or hydrogen. Since the alloy is very stable, cooling rates from slow-fumace cooling to rapid ice-brine quenching have virtually no effect on the mechanical properties.

HASTELLOY® S alloy can be readily forged and, because of its excellent ductility, can be cold worked. It can be welded by both manual and automatic welding methods including gas tungsten arc (GTAW), and gas metal arc (GMAW). Forging should be performed from 2100°F (1145°C) to 1600°F (871°C) up to the final 20 percent cross-section reduction. The final 20 percent reduction should be done from about 1900°F (1038°C) to 1500°F (816°C).


Composition

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

 
Weight %
Nickel 67 Balance
Cobalt 2 max.
Chromium 16
Molybdenum 15
Iron 3 max.
Silicon 0.4
Manganese 0.5
Carbon 0.02 max.
Aluminum 0.25
Boron 0.015 max.
Lanthanum 0.02
Tungsten 1 max.
 


Grade Specification

Grade UNS DIN EN AMS ASTM JIS
Hastelloy S

N06635

 
 
AMS 5711
AMS 5838
AMS 5873
  -


 

Physical Properties

The following table shows the physical properties of Hastelloy S.

Properties Metric Imperial
Density 8.75 g/cm³ 0.316 lb/in³
Melting point 1360°C 2480°F


Mechanical Properties

The mechanical properties of Hastelloy S are given in the following table.

Properties Metric Imperial
Tensile strength (@ 1093°C/1999°F, thickness 1.10-1.60 mm/0.0433-0.0630 in.) 110 MPa 16000 psi
Yield strength (@ 1093°C/1999°F, thickness 1.10-1.60 mm/0.0433-0.0630 in., 0.2% offset) 52 MPa 7540 psi
Elastic modulus 212 GPa 30700 ksi
Elongation at break (@ 982°C/1800°F, thickness 1.10-1.60 mm/0.0433-0.0630 in., in 50.8 mm) 46% 46%
Charpy Impact (V Notch; solution heat-treated, not aged) 190 J 140 ft-lb


Thermal Properties

The thermal properties of Hastelloy S are displayed in the following table.

Properties Metric Imperial
Thermal expansion co-efficient (@ 20-93°C/68- 99°F) 11.5 µm/m°C 6.39 µin/in°F
Thermal conductivity (@ 200°C/392°F) 14.0 W/mK 97.2 BTU.in/hr.ft².°F
 


Technology

Machinability
Hastelloy S has good machining characteristics. Tooling is required to avoid work hardening and chatter.

Forming
Hastelloy S can be formed using conventional methods.

Welding
Hastelloy S is welded using metal inert gas and tungsten inert gas welding methods.

Heat Treatment
Hastelloy S is heat treated by annealing at 1066°C (1950°F) followed by cooling in air.

Forging
Hastelloy S is forged at 872 to 1149°C (1600 to 2100°F).

Hot Working
Hastelloy S can be hot worked at 872 to 1149°C (1600 to 2100°F).

Cold Working
Hastelloy S can be easily cold worked.

Annealing
Hastelloy S is annealed at 1066°C (1950°F) followed by cooling in air.

Aging
Hastelloy S is aged at 538 to 872°C (1000 to 1600°F) in order to restores its ductility and strength.

Hardening
Hastelloy S can be hardened by cold working.


Applications

 

Use in Gas Turbine Engines

Hastelloy S is widely used in gas turbine engines because of its outstanding high-temperature performance and minimal thermal expansion. The alloy is valued for maintaining strength and structural integrity under the cyclical heating typical in gas turbines, making it ideal for components like seal rings, which benefit from its thermal stability and oxidation resistance. This ensures reliable performance and longevity, critical for the efficiency and safety of gas turbine operations.

Use in Chemical Processing

In chemical processing, Hastelloy S is preferred for equipment that faces corrosive environments and high temperatures. Its excellent resistance to pitting and crevice corrosion makes it ideal for reactors, heat exchangers, and pipes handling aggressive chemicals, ensuring the safety and efficiency of chemical processes. The alloy's ability to withstand harsh environments without degrading is crucial for maintaining operational integrity and reducing maintenance costs.

Use in Pharmaceutical Industry

The pharmaceutical industry requires materials that resist corrosion and maintain hygiene. Hastelloy S meets these needs with its broad corrosion resistance and high-temperature stability, making it ideal for pharmaceutical manufacturing equipment where product purity and contamination prevention are crucial. The alloy's durability and reliability allow it to withstand the rigorous cleaning and sterilization processes common in this industry, ensuring consistent performance and safety in pharmaceutical production.
 

Surface Treatment

 

Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
 
 

Processing

Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
 

Packaging & Shipping


Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate
Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate

Company Profile


Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate

FAQ

Wholesale High Quality AMS 5838/N06635 Nickel Alloy Sheet for Gas Turbine Engines Aerospace Materials Hastelloy S Plate

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