Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate

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

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  • Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
  • Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
  • Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
  • Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
  • Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
  • Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
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Overview

Basic Info.

Carbon Content
Low Carbon
PCD
100mm
ET
15mm
Hole
6
Key Words
GB /T 14992-2005 H10150 Alloy
Thickness
4mm - 600mm
Width
1000mm-3000mm
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
GB /T 14992-2005 H10150
Trademark
LORK
Origin
China
HS Code
7219350000
Production Capacity
50000kg/Month

Product Description

Product Description

 

Introduction

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

GH6783 is a Co-Ni-Fe based precipitation hardening ferromagnetic oxidation resistant low expansion deformation high temperature alloy with a service temperature of less than 750ºC. The alloy is strengthened by adding a large amount of aluminum and niobium elements, and precipitating γ'-Ni3 (Al, Nb) dispersion strengthening phase and blocky β-NiAl phase during aging. The alloy can reach a complete oxidation resistance level at 750ºC, and has excellent room temperature and high temperature mechanical properties, low thermal expansion coefficient and low density. The fine grain size can be controlled by precipitating β-NiAl phase during thermal deformation. The micro-alloyed alloy has excellent hot working properties and cold forming process properties. Hankai's main supply products include bars, cakes, rings, cold-rolled sheets and strips.


GH6783 Applications
 

GH6783 high-temperature alloy has been used to manufacture gap control components such as sealing rings, bearing rings and casings of advanced aircraft engines.
Bolts and other fasteners and bearing shafts and other components serving at medium and high temperatures in ground gas turbines,
Air guide tubes of rocket engines, etc.
Compared with other low expansion high-temperature alloys GH2907 and GH2909, the excellent oxidation resistance and low density of GH6738 alloy are the main characteristics of this alloy. The alloy has excellent performance and structural stability below 700ºC, but poor thermal stability above 750ºC.


GH6783 Chemical Composition, %
 
C Cr Ni Co Ta Fe Ti
≤0.03 2.5~3.5 26~30 Bal ≤0.05 24~27 ≤0.4
Al Nb B Mn Si P S Cu
5~6 2.5~3.5 0.003~0.012 ≤0.5 ≤0.5 ≤0.015 ≤0.005 ≤0.5

GH6783 Mechanical Properties

Form Condition Tensile (Ksi) 0.2% Yield (Ksi) Elongation % Hardness (HRB)
Bar Hot finished 60-85 15-45 55-35 45-80
Bar Cold drawn 55-75 15-30 55-40 45-70
Plate Hot rolled 55-80 15-40 60-40 45-75
Sheet Annealed 5-75 15-30 55-40 70 max
Pipe Annealed 55-75 12-30 60-40 70 max
GH6783 Specifications

GH6783 
GH783 
Inconel783

UNS R30783

 
Available sizes and specifications
GH6783 available sizes and specifications
Grade GH6783
Nickel plate Thickness: 0.3mm - 150.0mm
Width: 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 GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate

Processing

Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
 

Packaging & Shipping


Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate
Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate

Company Profile


Lork Custom GB /T 14992-2005 H10150 Solid Solution Strengthened Iron-Based Alloy Sheet for Aircraft Engine Parts Gh1015 Super Alloy Plate

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 .

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