NICKEL ALLOYS
Inconel 718 | EN 2.4668
Description
Inconel 718 is an Nickel-Chromium alloy being precipitation hardenable and having high creep-rupture strength at high temperatures to about 700°C. It has higher strength than Inconel X-750 and better mechanical properties at lower temperatures than Nimonic 90 and Inconel X-750. It has exceptional weldability compared to the Nickel-base super alloys hardened by Aluminium and Titanium.
Applications of Inconel 718
- Jet Engine
- High-Speed Airframe Parts
- Aircraft Wheels
- Aeroplane Buckets
- High Temperature Bolts and Fasteners
- Aircraft engines
- Gas turbine components
- Offshore platforms
- Pipelines
- Reactor vessels
- Heat exchangers
- Steam generators
- Nuclear power plants
- Liquefied natural gas (LNG) storage
- Cryogenic fuel systems
- Chemical reactors
- Refineries
- Wellhead equipment
- Thrust reversers
- Pharmaceutical processing
- Food processing
- Aerospace cryogenic systems
- Distillation columns
- Power plant exhaust systems
- Cryogenic research facilities
Available Forms
