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

Brand Name:KAIXIN
Certification:ISO9001:2015
Model Number:KX-Alloy4099
Minimum Order Quantity:200KG
Delivery Time:45~60days
Payment Terms:T/T, L/C
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Address: The North East of Danlv Bridge, Aerospace Industry Park, Lvcheng Town,Danyang City,Jiangsu Province
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Product Details

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


CMnSiPSNiCrTiAICOFeWMoMgBCe
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 TemperatureDelivery State≤1130≥35
900°CDelivery 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

GradeTest State and Heat Treatment institutionPlate Thickness/mm

Test Temperature

/℃

Test Stress/MPa

Test Time

/h

Elongation after breaking/%
ЭП693Delivery State0.8-4.090098≧ 30≧ 10

  • Productive Process


  • Professional Customization

Cold-drawn Wire¢0.3~¢18mm(Delivery in rolls or trays)
Hot-Rolling Wire¢5.5~¢20mm(Delivery in rolls)
Stripthickness 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

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

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

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