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A2N01 Heat Resistant Aluminum Plate High Temperature Strength Aerospace

A2N01 Heat Resistant Aluminum Plate High Temperature Strength Aerospace

Strength Aerospace Aluminum Plate

2A80 Aluminum Plate

Aluminum Plate T652

Place of Origin:

CHINA

Brand Name:

JBHD

Certification:

ISO,SGS

Model Number:

A2N01 Aluminum Sheet

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Product Details
Name:
2A80 LD8 A2N01 2618 Aerospace Aluminum Plate
Shape:
Plate,sheet,panel
Standard:
GB/T 3191-2010
Temper:
T651 T652
Stock:
In Stock
Application:
Aircraft Impellers Aircraft Pistons Aircraft Rings
Payment & Shipping Terms
Minimum Order Quantity
1 ton
Price
Negotiable
Packaging Details
Standard seaworthy export packing or as customer demands
Delivery Time
7-15 work days
Payment Terms
T/T, Western Union, L/C, MoneyGram
Supply Ability
10000 Tons per Month
Product Description

High Temperature Strength Aerospace Aluminum Plate A2N01 Heat Resistant

 

Aluminum and its alloys are today considered one of the most practical of metals for a variety of reasons. Its low cost, light-weight, and modern appearance are among the primary reasons for its widespread use. It is non-sparking, electrically conductive, thermally conductive, non-magnetic, reflective, and chemically resistant. It is popular in the construction, marine and aircraft industries because of its ease of fabrication, non-toxicity, strength (pound-for pound), and resistance to the corrosive atmospheres of industry and marine environments. Anodizing increases this corrosion resistance and also permits iridescent finishes in different colors. Some alloys are slightly corrosive and so are cladded with a thin layer of aluminum for added protection.

 


Alloy:2A80 LD8 A2N01 2618

Temper :T4,T6,T351

 

Features:

1. Heat-resistant wrought aluminum.

2. Slightly lower plasticity under thermal state,

3. Heat treatment can be strengthened,

4. High temperature strength

 

Application of 2A80 LD8 A2N01 2618 Aerospace aluminum plate

1. Aero-Engine Compressor blades,

2. Aircraft impellers

3. Aircraft pistons

4. Aircraft rings

2A80 LD8 A2N01 2618 Aluminum Chemical Composition Limit

Cu Mg Mn Fe Si Zn Ti Ni other Al
1.9~2.5 1.4~1.8 0.20 1.0~1.6 0.5~1.2 0.3 0.15 0.9~1.5 0.15 remainder


2A80 LD8 A2N01 2618 aluminum Mechanical properties

Tensile Strength

 

Yield Strength

 

Elongation

 

477~485 (Mpa) 361~385 (Mpa) 13~14.5(%)

 

2A80 LD8 A2N01 2618 Aerospace aluminum plate specification

Alloy Series Alloy Tempe

Thickness

 

Width

 

Length

 

2 series 2A80 LD8 A2N01 2618 T4,T6,T351 4~12mm 1000~2600mm 2000-24000mm
2 series 2A80 LD8 A2N01 2618 12~260mm 1000~3800mm 2000~38000mm

 

2A80 LD8 A2N01 2618 Aerospace aluminum plate in aerospace

Item Alloy Temper Application
1 2A80 LD8 A2N01 2618 T4,T6,T351

1. Aero-Engine Compressor blades

2. Aircraft impellers

3. Aircraft pistons

4. Aircraft rings

 

Specification

ABM 1-1006

AIMS 03-02-021

AIR 9048

ASN-A 3355

BAEM 1103

DAN 422

MEP02-020


WL 3.1924

 


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Company Introduction
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A2N01 Heat Resistant Aluminum Plate High Temperature Strength Aerospace 8

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