Inconel 2.4669 Alloy X-750 Wire 0 1/16-0 3/32in N07750 Nickellegierung

Description

Inconel® 2.4669 alloy X-750 wire 1.5-2.5mm N07750 nickel alloy
Inconel® 2.4669 alloy X-750 wire 1.5-2.5mm N07750 nickel alloy
Do you need a different steel quality or dimensions? Please write to us. Our sales team makes an offer from stock program or delivery program :)
Length tolerance +/-2mm
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Technical specifications:
Brand:
Evek
Manufacturer number:
Not applicable
Type:
wire
Material:
nickel
Areas of application:
component for gas turbines; combustion chamber of rocket engines; highly heat-resistant springs, screws and fasteners (up to 650 °C)
Characteristics:
corrosion and oxidation resistance; high creep and heat resistance; very good relaxation resistance
Norm classifications:
Material number:
2.4669
Alloy:
X-750
US:
N07750
Further information:
Density:
8.28 g/cc
melting point:
1430°C
thermal conductivity:
12 W/m K
electr. Resistance:
1.21Ω•mm²/m
Description:
Production time - 2-3 weeks.
Preparation for shipment - 2-3 working days.
Look at the FAQ please.
2.4669 is a hardenable nickel-chromium-iron alloy. The nickel and chromium content is about 70% and 15% The main alloying elements are iron (approx. 7%) and titanium (approx. 2.5%). The proportion of aluminium, niobium, cobalt and manganese is approximately 4% in total. Alloy X-750 is resistant to corrosion and oxidation and exhibits high high-temperature strength at temperatures up to 700 °C.
Alloy X-750 is mainly used to make components for gas turbines. The material is also used for:
combustion chamber of rocket engines;
highly heat-resistant springs, screws and fasteners (up to 650 °C).
2.4669 provides the following properties:
corrosion and oxidation resistance;
high creep and heat resistance;
very good relaxation resistance.
documentation
Data sheet (German)
d — outside diameter
Listing and template services provided by inkFrog
Do you need a different steel quality or dimensions? Please write to us. Our sales team makes an offer from stock program or delivery program :) component for gas turbines; combustion chamber of rocket engines; highly heat-resistant springs, screws and fasteners (up to 650 °C) corrosion and oxidation resistance; high creep and heat resistance; very good relaxation resistance 2.4669 is a hardenable nickel-chromium-iron alloy. The nickel and chromium content is about 70% and 15% The main alloying elements are iron (approx. 7%) and titanium (approx. 2.5%). The proportion of aluminium, niobium, cobalt and manganese is approximately 4% in total. Alloy X-750 is resistant to corrosion and oxidation and exhibits high high-temperature strength at temperatures up to 700 °C. Alloy X-750 is mainly u