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Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

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Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial
Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

Large Image :  Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

Product Details:
Place of Origin: China
Brand Name: Superalloys
Certification: ISO 9001 and RoHS
Model Number: GH3030/ Nimonic 75
Payment & Shipping Terms:
Minimum Order Quantity: 50KG
Price: USD 25~50 / KG
Packaging Details: Wooden case
Delivery Time: 25-30 days
Payment Terms: T/T, Western Union, L/C
Supply Ability: 50000

Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

Description
Shape: Bar Condition: Soft And Hard
Diameter: 5-150 Density (g/cm3): 8.4
Melting Point (℃): 1374~1420 Feature: Good Resistance To Oxidation
High Light:

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 Nimonic 75 Sheet High Temp Alloy Bar GH3030 for Fasteners Of Aviation Industrial

 

 

Application:

 

This alloy be used for turbine engine combustor components operating below 800 degrees Celsius and in 1100 degrees Celsius under load requirements antioxidant but small high temperature components.

High temperature alloy cold drawn rod is cold drawn into a diameter of 8 ~ 45mm circular edge length of 8 ~ 30mm square, inscribed circle diameter of 8 ~ 36mm simple hexagonal cross section superalloy bars, used in the manufacture fasteners in aviation industrial and other industries.

 

Physical properties

 

>Density (g/cm3): 8.4

>Melting point (℃): 1374~1420

 

Feature: At 800 degrees Celsius with a satisfactory heat resistance and high ductility, and has good resistance to oxidation, thermal fatigue, cold stamping and welding performance. For single-phase austenitic alloys course after solution treatment and stable organization.

 

Description:

Chemical composition(%)

 

Grade

C

Si

Mn

Ti

S

Ni

Cr

Cu

Fe

GH3030

≤0.12

≤0.8

≤ 0.7

0.15~0.35

≤0.015

Bal.

19~22

≤0.2

≤1.5

 

 

 

 

 

Yield Strength (Mpa)

Tensile Strength (Mpa)

Elongation, %

Hardness, HB

GH3030

Solution treatment

270

650

≤30

 

 

 

 

 

 

 

 

 

 

 

If you have any questions, pls write email to us: zlz@tankii.com

Looking forward to your inquiry!

 

Contact Details
Shanghai Tankii Alloy Material Co.,Ltd

Contact Person: tankii

Tel: +8615000002421

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