• Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
  • Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
  • Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
  • Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
  • Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
  • Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /

Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /

Application: Industrial
Standard: GB, ASTM
Purity: >99.5%
Alloy: Alloy
Powder: Not Powder
Transport Package: Wooden
Customization:
Gold Member Since 2016

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Manufacturer/Factory

Basic Info.

Model NO.
XD-288
Origin
Jiangsu Baoying
HS Code
7505120000
Production Capacity
500ton/Year

Product Description

 GH3039 is a single-phase austenitic solid solution strengthened alloy with moderate thermal strength and good thermal fatigue properties below 800°C, and good oxidation resistance below 1000°C.

Long-term use is stable in structure, and also has good cold formability and welding performance.

Parts of aero-engine combustion chamber and afterburner suitable for long-term use below 850°C.

The alloy can be used to produce plates, bars, wires, tubes and forgings.

Single-phase austenitic solid solution strengthened alloy
Material grade GH3039 (GH39)
Similar grades ЗИ602, ХН75МБГЮ

Material Technical Standards

GJB 1952-1994 "Specification for high temperature alloy cold-rolled sheet for aviation"
GJB 2297-1995 "Specification for cold drawn (rolled) seamless pipes of high temperature alloys for aviation"
GJB 2612-1996 "Specification for cold drawing of high temperature alloys for aviation"
GJB 3165-1998 "Specification for hot-rolled and forged bars of superalloys for aerospace load-bearing parts"
GJB 3317-1998 "Specification for high-temperature alloy hot-rolled sheet for aviation"
GJB 3318-1998 "Specification for Cold Rolled Strips of High Temperature Alloys for Aviation"
GB/T15062-1994 "General Purpose Superalloy Tube"

Chemical composition

Table 1-1
   C             Cr             Ni           Al               Ti                Mo            Nb
≤0.08   19.0~22.0   margin  0.35~0.75  0.35~0.75  1.80~2.30  0.90~1.30

   Fe       Si         S          Mn        P
≤3.00  ≤0.80  ≤0.012   ≤0.40   ≤0.02

Note: Ce is allowed in the alloy. Cu=0.20% in the alloy.

Heat treatment system
Solution treatment of hot-rolled and cold-rolled sheets and strips: 1050~1090ºC, air cooling. Solution treatment of rods and pipes: 1050~1080ºC, air-cooled or water-cooled.

Specifications and Supply
Can supply various specifications of hot-rolled sheet, cold-rolled sheet, strip, bar, wire, pipe, and forgings. Sheets, strips and tubes are solution treated and pickled for delivery. The wire rod is supplied in the cold working state or the solid solution state and the bar is delivered without heat treatment.

Melting and casting
The alloy is smelted by electric arc furnace, electric arc furnace or non-vacuum induction furnace plus electroslag remelting or vacuum arc remelting and vacuum induction furnace plus electroslag or vacuum arc remelting process.

Application overview
The aero-engine combustion chamber and afterburner parts made of this alloy have good performance after long-term production and use tests.

Physical and chemical properties

Thermal performance

2.1.1. Thermal conductivity

table 2-1

θ/°C                100   200   300  400  500  600   700   800  900
λ/(W/(m·C))    13.8  15.5 17.2  18.8 20.5 21.8  23.4  25.1 26.8

2.1.2. Specific heat capacity

Table 2-2.

θ/°C              150   200  300  400  500  600  700  800
c/(J/(kg.K))    544  574   636  645  762  779  921 1047

2.1.3, GH30 linear expansion coefficient

Table 2-3

θ/°C            20~100  20~200  20~300  20~400  20~500  20~600  20~700  20~800  20~900  20~1000
α/10-6C-1      11.5      12.4       13.2        13.5      13.8        14.3       14.9       15.3       15.8        16.4

Density ρ=8.3g/cm3

Electrical properties   Room temperature resistivity  ρ=1.18*10-6Ω.m

alloy magnetic  Alloy non-magnetic

Metallographic structure
The alloy is single-phase austenite in the solid solution state, and contains a small amount of Ti(CN), NbC and M23C6 carbides.

Process performance requirements
1. The alloy has good plasticity in hot working process and good deformation performance. The forging heating temperature is 1170ºC, and the final forging is 900ºC.
2. The average grain size of the alloy is closely related to the deformation degree and final forging temperature of the forging.
3. The alloy can be welded by argon arc welding, spot welding or seam welding, and its welding performance is excellent, and the tendency of argon arc welding to crack is small.
4. After heat treatment, the oxide scale on the surface of the parts can be removed by sand blowing or pickling.

 Company Profile

Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
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Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
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Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
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 Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /Gh3039 / Single-Phase Austenitic Solid Solution Strengthened Alloy / Master Alloy / Mother Alloy / Gh39 /
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Our products sales all over the world as well. From the following two websites you can also get more information about our company:
http://xingda-alloy.en.made-in-china.com
http://xingda-alloy.en.made-in-china.com
 
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