Inconel X-750

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Inconel X-750

Inconel X-750 UNS N07750 High Temperature Alloys tooling and aircraft structures

008615801826494

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8615801826494

Inconel X-750

description1

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INTRODUCTION

Inconel Alloy X-750 (UNS designation N07750) is a nickel-chromium alloy similar to Inconel 600 but made precipitation hardenable by additions of aluminum and titanium. It has good corrosion resistance and oxidation resistance below 980°C, high strength below 800°C, good relaxation resistance below 540°C, and also has good formability and welding performance. This alloy is mainly used to manufacture relaxation-resistant flat springs and coil springs for aircraft engines that operate below 800°C and require high strength. It can also be used to manufacture parts such as steam turbine blades.

Similar Grade

GB	UNS	DIN	W-Nr
GH4145	N07750	XCr15Fe7TiAl	2.4669

APPLICATION

Gas turbines
rocket engines
nuclear reactors
pressure vessels
tooling and aircraft structures

CHEMICAL COMPOSITION

Min

70.0

5.0

0.7

14.0

2.25

0.4

Max

9.0

1.2

17.0

0.08

1.0

0.5

0.015

0.01

3.75

1.0

0.5

1.0

PHYSICAL PROPERTIES

Grade	Density	Melting Point	Tensile strength,MPa	Yield strength,MPa	Elongation,%
Inconel X-750	8.28g/cm3	1390°C-1430 °C	855	427	40

Feature

Alloy X-750 has good resistance to corrosion and oxidation along with high tensile and creep rupture properties at temperature up to 1300°F (700°C).

Specification Standard

Rod,Bar	Pipe, Tube	Plate, Sheet, Strip	Pipe fittings	Forgings	Wire
ASTM B637 DIN 17752 ISO 9723	ASTM B163 B165,B829, B730 B751 DIN 17751 ISO 6207	ASTM B670 B906 DIN 17750 ISO 6208	ASTM B366	ASTM B564 ISO 9725 DIN 17754	ASTM B164 DIN 17753 ISO 9724