Dec 04, 2025 Leave a message

Nickel Alloy Inconel X 750 Bright Plate For Heat-Treating Fixtures Forming Tools Extrusion Dies Rocket-Engine Thrust Chambers

1. What is Inconel X-750, and what are its key properties?


Answer:
Inconel X-750 is a nickel-chromium alloy strengthened by precipitation hardening. Its key properties include:

High mechanical strength at elevated temperatures

Excellent creep and stress-rupture resistance

Good corrosion and oxidation resistance in high-temperature environments

Stability under thermal cycling, making it ideal for aerospace, nuclear, and industrial applications.

 


2. What is the chemical composition of Inconel X-750?


Answer:

Element Typical Content (%)
Nickel (Ni) 70 min
Chromium (Cr) 14–17
Iron (Fe) Balance (~7–17)
Cobalt (Co) ≤1.5
Titanium (Ti) 0.7–1.2
Aluminum (Al) 0.4–0.75
Manganese (Mn) ≤0.5
Silicon (Si) ≤0.5
Carbon (C) ≤0.08
Niobium + Tantalum (Nb + Ta) 0.3–1.15
This composition ensures high-temperature strength, hardness, and corrosion resistance.  

 

3. What are the mechanical properties of Inconel X-750 bright plate?


Answer:

Tensile Strength (MPa): 860–1400 (depends on heat treatment)

Yield Strength (MPa): 520–1100

Elongation (%): 10–25

Hardness (HRC): 28–40

Creep Resistance: Excellent up to ~1200°F (649°C)
These properties make it suitable for load-bearing and high-stress applications at elevated temperatures.

 


4. Why is Inconel X-750 suitable for heat-treating fixtures, forming tools, and extrusion dies?


Answer:

Maintains dimensional stability under thermal cycling

Resists oxidation and carburization at high temperatures

Can be solution treated and aged to achieve desired strength and hardness

Withstands repeated mechanical stress, making it ideal for forming, extrusion, and die applications

 


5. Why is Inconel X-750 used in rocket-engine thrust chambers?


Answer:

Exceptional strength-to-weight ratio at high temperatures

Corrosion and oxidation resistance under extreme thermal and chemical conditions

Maintains structural integrity under thermal shock and cyclic loading

Its precipitation-hardening capability allows customization of strength for aerospace requirements

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