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

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

Name: Cold Drawn Hot Rolled High Temp Alloys Used For Manufacturing Aircraft Engines
Brand: KAIXIN
Price: 1 USD

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

Brand Name : KAIXIN

Model Number : KX-Alloy4099

Certification : ISO9001:2015

Place of Origin : China

MOQ : 200KG

Price : To negotiate

Payment Terms : T/T, L/C

Supply Ability : 50~80TONS per MONTH

Delivery Time : 45~60days

Packaging Details : Wooden Box, size as per guests request

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

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℃

Size : Negotiable

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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

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

Elongation after breaking/%

ЭП693

Delivery State

0.8－4.0

900

≧ 30

≧ 10

Productive Process

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

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

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

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

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

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