Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750

Product Details
Customization: Available
Standard: JIS, GB, DIN, BS, ASTM, AISI
Alloy: Alloy
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  • Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750
  • Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750
  • Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750
  • Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750
  • Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750
  • Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750
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Basic Info.

Model NO.
600
Type
Nickel Pipe
Powder
Not Powder
Trademark
FUSHUN
Origin
China
Production Capacity
5000tons/Year

Product Description

Introduce:
Fushun Metal is your high quality manufacturer of Nickel, Nickel-based, Copper-Nickel, Iron-Nickel Wire, Bar, Plate, Strip, Pipe and Forged products. We melt alloys in our EAF/VIM/VAR/LF/VOD furnaces and subsequent ESR refining processes can be employed for the most critical alloys. The ingots are then hot-worked by rolling or forging, followed by mechanical finishing such as peeling, turning, or cold working on one of our draw benches. According to customer request, we can employ special heat treatment procedures, drawing, straightening and sawing to length to achieve particular dimensions and tolerances. You also have the opportunity to specify both standard as well as modified chemical analyses.

INCONEL alloy X-750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic temperatures.

Application:
Inconel X-750 is used to fabricate flat springs and sheet metal stampings that are used in very high temperature applications such as jet engine parts, nuclear power plant
applications, heat-treating fixtures, forming tools, and extrusion dies.
•Gas turbine rotor blades, wheels and bolts
•Airframe thrust reversers and hot-air ducting systems
•Rocket engine thrust chambers
•Heat treat fixtures and cryogenic vessels, springs and fasteners

Standard and Grade:
INCONEL alloy X-750 is designated as UNS N07750 and W. Nr. 2.4669. The alloy is stated in NACE MR-01-75. Available product forms are sheet, strip, plate, round bar, flat bar, forging stock, hexagon, wire, tubing and extruded section. Specifications include the following:
Rod, Bar and Forging - ASTM/ASME SB637; ISO 9723-9725; SAE AMS 5667-5671 5747; EN 10269
Plate, Sheet and Strip - ISO 6208, SAE AMS 5542 and 5598.
Wire - BS HR 505, SAE AMS 5698 and 5699.

Chemical Component:

X-750 Ni(+Co) Cr Fe Ti Al No(+Ta) Si S Cu C Co
Min 70 14 5 2.25 0.4 0.7 -- --- -- -- --
Max -- 17 9 2.75 1 1.2 0.5 0.01 0.5 0.08 1



Physical Constants and Thermal Properties:
Thermal Properties:
Temperature,°F Mean Linear Expansion, in./in./°F x 10-6 from 70° F to Temperature Shown Thermal Conductivity, Btu/in./hr/sq ft/°F Specific Heat Btu/lb/°F Diffusivity, sq ft/hr Electrical Resistivity, ohm/circ mil/ft
-250 6.5 67 0.073 0.15 -
-200 6.6 70 0.08 0.143 -
-100 6.7 74 0.09 0.135 -
70 - 83 0.103 0.132 731
200 7 89 0.109 0.133 739
400 7.2 98 0.116 0.14 746
600 7.5 109 0.12 0.148 761
800 7.8 120 0.125 0.158 771
1000 8.1 131 0.13 0.169 783
1200 8.4 143 0.137 0.173 786
1400 8.8 154 0.151 0.172 775
1600 9.3 164 0.171 0.164 761
1800 9.8 - - - -
Temperature,°F Modulus of Elasticity, 103 ksi
Tension Torsion
Static Dynamic Static
80a 31 31 11
500 28.7 29.1 10.2
1000 25 26.7 9
1200 23 25.5 8.1
1350 21 24.4 -
1500 18.5 23.2 -
1600 - 22.1 -
1800 - 20 -

Effect of Heat Treatment on Room-Temperature
Resistivity of Hot-Rolled Bar
Heat Treatment Resistivity, ohm/circ mil/ft
As hot-rolled 759
2000°F/1 hr, A.C. 763
2100°F/1 hr, A.C.+1500°F/24 hr, A.C.+1300°F/20 hr, A.C. 724
1800°F/1 hr, A.C.+1350°F/8 hr,F.C. to 1150°F, hold at 1150°F for total time of 18 hr, A.C. 739

Mechanical Properties:
INCONEL alloy X-750 may be given any one of a variety of heat treatments. Each develops special properties and puts the product form in the best condition for its intended application. In all conditions, alloy X-750 is resistant to oxidation up to 1800°F. The most often used heat treatments have been incorporated by the Society of Automotive Engineers in their AMS specifications* for various product forms.

 
Product Form AMS Specifications Heat Treatment Remarks
Rods, bars and forgings 5667 1625°F/24 hr, AC, + 1300°F/20 hr, AC(Equalizing plus precipitation treatment). High strength and notch rupture ductility up to 1100°F.
Rods, bars and forgings 5670,5671,& 5747 1800°F anneal + 1350°F/8 hr, FC to 1150°F, Hold at 1150°F for total precipitation-treating time of 18 hr, AC (Solution treatment plus furnace-cool precipitation treatment). Increased tensile properties and reduced heat treating time for service up to about 1100°F.
Rods, bars and forgings - 1800°F anneal + 1400°F/1 hr, FC to 1150°F, Hold at 1150°F for total precipitation-treating time of 6 hr, AC (Solution treatment plus short furnace-cool precipitation treatment). Short furnace-cool aging. Achieves only slightly lower properties than does AMS 5670 and AMS 5671.
Rods, bars and forgings 5668 2100°F anneal + 1550°F/24 hr, AC, + 1300°F/20 hr, AC (Triple heat treatment). Maximum creep, relaxation and rupture strength above about 1100°F.
Sheet, strip and plate (Supplied in annealed condition) 5542 1300°F/20 hr, AC (Constant-temperature precipitation treatment). High strength to 1300°F.
Sheet, strip and plate (Supplied in annealed condition) 5598 1350°F/8 hr, FC to 1150°F, Hold at 1150°F for total precipitation-treating time of 18 hr, AC (Furnace-cool precipitation treatment). High strength up to 1300°F (Increased tensile properties to about 1100°F).
Sheet, strip and plate (Supplied in annealed condition) - 1400°F/1 hr, FC to 1150°F, Hold at 1150°F for total time of 6 hr, AC (Short furnace-cool precipitation treatment). Increased tensile properties and reduced heating time for service up to about 1100°F.
Seamless tubing 5582 1300°F/20 hr, AC (Constant-temperature precipitation treatment). High strength up to about 1300°F.
Wire, No. 1 temper 5698 1350°F/16 hr, AC (Constant-temperature precipitation treatment). For springs requiring optimum resistance to relaxation from about 700°F to 850°F and at low to moderate stresses to about 1000°F.
Wire, spring temper 5699 1200°F/4 hr, AC (Constant-temperature precipitation treatment). High strength up to about 700°F.
Wire, spring temper 5699 2100°F anneal + 1550°F/24 hr, AC + 1300°F/20 hr, AC (Triple heat treatment). For springs for service requiring maximum relaxation resistance at about 850°F to 1200°F.

Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750Inconel Alloy Sheet Plate 600 601 625 617 713c 627 718 X-750

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