Age-hardenable, nickel-base superalloy Inconel X-750 (UNS N07750) alloy Manufacturer

Inconel X-750 (UNS N07750) alloy is an age-hardenable, nickel-base superalloy with a very good strength at temperatures up to about 1600°F (870°C). It is widely used as a wrought material for forged and fabricated parts in aerospace and industrial applications.

Products Details

Inconel X-750 (UNS N07750) alloy is an age-hardenable, nickel-base superalloy with a very good strength at temperatures up to about 1600°F (870°C). It is widely used as a wrought material for forged and fabricated parts in aerospace and industrial applications. Its strength is somewhat less than that for Inconel 718 alloy up to about 1400°F (760°C), and lower than that for Inconel R-41 alloy at higher temperatures. Alloy X-750 can be cold-formed in the annealed condition, and may also be hot-formed at temperatures of about 1900°F (1040°C) or above. Weldability is somewhat limited by susceptibility to strain age-cracking under conditions of heavy restraint. The alloy exhibits good resistance to oxidizing combustion gas environments at temperatures up to about 1600°F (870°C).Inconel X750 Alloy Product Forms and Standards
Bar Forging Sheet/Strip Wire
ASTM B637 ASTM B637 AMS 5542 AMS 5598 AMS 5698 AMS 5699
Tensile Strength (σb/MPa) Yield Strength (σp0.2/MPa) Elongation (σ5/%)
912 551 25
The Inconel X-750 nickel alloy is similar to Inconel alloy 600 but made precipitation hardenable by adding aluminum and titanium and thereby shows excellent resistance to high temperature corrosion and oxidation along with high tensile and creep-rupture strength, relaxation resistance as well as good fabricating and welding properties.The alloy X-750 also has outstanding mechanical properties down to cryogenic temperatures. With such properties, the nickel-chromium alloy is mainly used for high-temperature springs and bolts, gas turbine blades, rocket engines, abrasion wheels, high pressure vessels, etc.

Nickel:

70 Balance

Chromium:

16

Iron:

8

Titanium:

2.5

Niobium* + Tantalum:

1

Aluminum:

0.8

Cobalt:

1 max.

Manganese:

0.35 max.

Silicon:

0.35 max.

Carbon:

0.08 max.

Test Temperature

Approximate Initial Stress to Produce Rupture in:

10 h

100 h

1000 h

°F

°C

ksi

MPa

ksi

MPa

ksi

MPa

1100

600

120

825

85

585

71

490

1200

650

80

550

66

455

50

345

1300

705

61

420

45

310

29

200

1400

760

41

285

26

180

15

105

1600

815

24

165

14

97

7.4

51

1700

870

12.5

86

6.6

46

-

-

1800

925

6.5

45

-

-

-

-

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