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Cold Drawn Hot Rolled High Temp Alloys Used For Manufacturing Aircraft Engines

Product Details

Place of Origin: China

Brand Name: KAIXIN

Certification: ISO9001:2015

Model Number: KX-Alloy4099

Payment & Shipping Terms

Minimum Order Quantity: 200KG

Price: To negotiate

Packaging Details: Wooden Box, size as per guests request

Delivery Time: 45~60days

Payment Terms: T/T, L/C

Supply Ability: 50~80TONS per MONTH

Get Best Price
Highlight:

Hot Rolled high temp alloys

,

Cold Drawn high temp alloys

,

ISO9001 high temperature nickel alloys

Features:
1000℃ Features: The Alloy Has A High Thermal Force, Can Be Used For A Long Time Below 900℃ And The Highest Working Temperature Can Reach 1000℃
Shape:
Wire, Strip, Rod, Tube, Plate
Alloy Type:
Precipitate-hardened Nickel Based Alloy
Raw Materials:
NI Rem,CR 17-20%,CO 5-8%
Executive Standard:
GB/T1992,GOST
Delivery State:
Sosoloid
Application:
Used For Manufacturing Aircraft Engines, Processing Adjustable Nozzle Shells And Processing Cylinders
Size:
Negotiable
Features:
1000℃ Features: The Alloy Has A High Thermal Force, Can Be Used For A Long Time Below 900℃ And The Highest Working Temperature Can Reach 1000℃
Shape:
Wire, Strip, Rod, Tube, Plate
Alloy Type:
Precipitate-hardened Nickel Based Alloy
Raw Materials:
NI Rem,CR 17-20%,CO 5-8%
Executive Standard:
GB/T1992,GOST
Delivery State:
Sosoloid
Application:
Used For Manufacturing Aircraft Engines, Processing Adjustable Nozzle Shells And Processing Cylinders
Size:
Negotiable
Cold Drawn Hot Rolled High Temp Alloys Used For Manufacturing Aircraft Engines

KX ЭП693 Light Rod Plate Structural Operating Temperature Range For High Temperature Alloy

 

Product Description and Application

     

ЭП693 is also known as "P 693," "N" 68 manas ona (R) "n" (R)

ЭП693 is a high alloying nickel-based aging alloy, which is strengthened with cobalt, tungsten, aluminum, titanium and etc elements, so that the alloy has a high thermal force, which can be used for a long time below 900℃and the highest working temperature can reach 1000℃. The alloy has stable microstructure and satisfactory performance in cold and hot processing and welding process, which is suitable for high temperature plate bearing welding structural parts such as aeroengine combustion chamber and afterburner. Large plate structural parts made of this alloy can be directly used after solution treatment without aging treatment.

 

Process Performance and Requirements

 

  • Product Fusion Process

 

Vacuum Induction Furnace(VIM) and Electroslag Remelting Furnace(ESR)

 

  • Product Chemical Composition 

 

 

Grade

 

C Mn Si P S Ni Cr Ti AI CO Fe W Mo Mg B Ce
ЭП693

0.08

0.4

0.5

0.015

0.015

Rem

17.0

~

20.0

1.0

~

1.5

1.7

~

2.4

5.0

~

8.0

2.0

5.0

~

7.0

3.5

~

4.5

0.01

0.005

0.02

 

  • Product Heat Treatment Institution

 

Test Temperature °C

Heat Treatment or Condition

Tensile Strength

Mpa

Elongation after breaking %

Room Temperature Delivery State ≤1130 ≥35
900°C Delivery status + time limitation ≥295 ≥23
Recommended solution treatment institution: 1080~1140°C(maximum 1160°C), air cooling or rapid cooling; Aging treatment: 900±10°C, heat preservation for 5h, air cooling

 

  • Product High Temperature Durability

 

Grade Test State and Heat Treatment institution Plate Thickness/mm

Test Temperature

/℃

Test Stress/MPa

Test Time

/h

Elongation after breaking/%
ЭП693 Delivery State 0.8-4.0 900 98 ≧ 30 ≧ 10

 

  • Productive Process

 

Cold Drawn Hot Rolled High Temp Alloys Used For Manufacturing Aircraft Engines 0

 

  • Professional Customization

Cold-drawn Wire ¢0.3~¢18mm(Delivery in rolls or trays)
Hot-Rolling Wire ¢5.5~¢20mm(Delivery in rolls)
Strip thickness 0.1~4.5*width 6~350mm(Supply in rolls or straight strips)
Smooth Forged Rod on a Lathe

¢60~350mm,L800-2500mm

Hot-rolled Burnishing ¢20~80mm,L1000-5000mm
Cold Drawn and Burnishing ¢2.5~18mm,L1000-8000mm
Seamless Tube ¢1~275mm,wall thickness 0.2~30,L1000-8000mm

 

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