Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar

Product Details
Customization: Available
Product Type: Rod
Material: Nife
Manufacturer/Factory, Group Corporation
Diamond Member Since 2024

Suppliers with verified business licenses

Audited Supplier

Audited by an independent third-party inspection agency

  • Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
  • Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
  • Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
  • Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
  • Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
  • Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
Find Similar Products
  • Overview
  • Product Description
  • Detection
  • Processing
  • Packaging & Shipping
  • Company Profile
  • FAQ
Overview

Basic Info.

Model NO.
Haynes 244 Bar/rod
PCD
112mm
ET
42mm
Hole
5
Key Words
Haynes 244 Supplier
Diameter
3-300mm
Length
as Your Requirments
Surface
Black, Bright, Polished, Pickling
MOQ
100kgs
Sample
Free-Sample
Technique
Cold Rolled, Hot Rolled
Condition
Annealed;Heat Treatment;
Stock
in Stock
Transport Package
Wooden Package
Specification
haynes 244
Trademark
LORK
Origin
China
HS Code
7505120000
Production Capacity
50000kg/Month

Product Description

Product Description

 

Introduction

LORK is a super alloy manufacturer with 20 years of manufacturing experience.
 

HAYNES 244 alloy is a new Ni-Mo-Cr-W alloy developed for static parts in advanced gas turbine engines which require low thermal expansion at temperatures up to 1400°F (760°C). It offers a higher maximum use temperature than other low thermal expansion alloys currently available, including a 100-200°F (55-110°C) improvement over HAYNES 242 alloy. The alloy is age-hardenable by formation of Ni2 (Cr,Mo,W) domains, which are structurally similar to the strengthening domains in 242 alloy. Judicious alloying with tungsten increased the thermal stability of these domains and lowered the coefficient of thermal expansion. Other important properties such as oxidation resistance and low-cycle fatigue performance are comparable or better than those of 242 alloy.

 Haynes 244 Application
HAYNES 242 alloy combines properties which make it ideally suited for a variety of component applications in aero and industrial gas turbine engines. It may be used for seal rings, containment rings, duct segments, casings, fasteners, rocket nozzles, pumps, and many others. In the chemical process industry, 242 alloy will find use in high-temperature vapor-containing processes as a consequence of its excellent resistance to that environment. The alloy also displays excellent resistance to high-temperature fluoride salt mixtures. The high strength and fluorine environment-resistance of 242 alloy has also been shown to provide for excellent service in fluoroelastomer process equipment, such as extrusion screws.


Heat Treatment

 
HAYNES 244 alloy is furnished in the annealed condition, unless otherwise specified. The alloy is usually annealed in the range of 2000-2100°F (1093-1149°C), depending upon specific requirements, followed by an air cool (or more rapid cooling) before aging. A water quench is recommended for heavy section components. Aging is performed by holding at 1400°F (760°C) for 16 hours, furnace cooling to 1200°F (649°C) and holding for 32 hours, followed by air cool.


Haynes 244 Chemical Composition

 
Nickel Balance
Aluminum 0.5 max.
Carbon 0.03 max.
Chromium 8
Iron 2 max.
Manganese 0.8 max.
Molybdenum 22.5
Tungsten 6




Haynes 244 Mechanical Properties

 
Test Temperature Yield Strength, 0.2% Offset Ultimate Tensile Strength Elongation Reduction of Area
°F °C ksi MPa ksi MPa % %
RT RT 121.2 836 195.0 1345 34 37
200 93 116.3 802 190.3 1312 39 41
400 204 110.3 761 181.6 1252 39 45
600 316 107.9 744 175.4 1209 41 44
800 427 100.0 689 170.4 1175 41 46
1000 538 99.3 685 164.2 1132 38 43
1100 593 97.5 672 156.3 1078 32 32
1200 649 93.8 647 141.4 975 21 24
1300 704 84.8 585 125.6 866 18 20
1400 760 67.2 463 105.0 696 44 37
1500 816 37.1 256 72.0 463 106 70
1600 871 34.8 240 54.1 354 124 84
1700 927 38.2* 263* 42.4* 208* 161* 89*
1800 983 24.0 165 30.4 210 141 94
Available Sizes And Specifications
Haynes 244 available sizes and specifications
Grade Haynes 244
Nickel plate Thickness: 0.3mm - 150.0mmWidth: 1000mm - 3000mm
Nickel strip/ nickel foil Thickness: 0.02mm - 16.0mm
Width: 5mm - 3000mm
Nickel coil Thickness: 0.3mm - 16.0mm
Width: 1000mm - 3000mm
Nickel pipe Outside diameter: 6mm - 1219mm
Thickness: 0.5mm - 100mm
Nickel Capillary Pipe Outside diameter: 0.5mm - 6.0mm
Thickness: 0.05mm - 2.0mm
Nickel bar Diameter: Ф4mm - Ф600mm
Nickel wire rod Diameter:Ф0.01mm - Ф6mm

Detection


Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar

Processing

Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
 

Packaging & Shipping


Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar
Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar

Company Profile


Lork Custom Age Hardening Treatment AMS 5544/ASTM B435/ASME Sb-435 Super Alloy Rod for Aircraft Engine Parts Haynes 244 Alloy Bar

FAQ


Q1: Do you accept the trial order ?
A1: Yes,if we have the exactly size in stock.we can delivery even 1 piece/meter .

Q2: Can I have free sample before making orders?

A2: Yes,we can supply free sample as requirement,but buyer needs to pay the freight charges ,the freight fee will return to buyer after making order.

Q3: How do you control the quality ?
A3: MTC and PMI will be sent before shipment,any 3rd party inspection if need .

Q4: How about your delivery time ?
A4: Generally delivery time is 15 working days .

Q5: How can I quickly get the price list ?
A5: Directly click "chat now" or send us email with detail specifications,you will get the official price list in 1 hour .

Send your message to this supplier

*From:
*To:
*Message:

Enter between 20 to 4,000 characters.

This is not what you are looking for? Post a Sourcing Request Now
Contact Supplier