NICKEL ALLOYS

Inconel 718 | EN 2.4668

Inconel 718

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
Download Datasheet

EQUIVALENT STANDARDS

ASTM AISI EN DIN UNS IS
Alloy 718 Inconel 718 2.4668 NiCr19BnMo N07718 -

CHEMICAL PROPERTIES

C Mn Ni Cr Mo Si
0.05 0.35 52 19 3 0.35
Cu Ti Co P Al Nb
0.3 0.8 1 0.015 0.5 5

MECHANICAL PROPERTIES

YSRp02 TSRm A HRB
1030 1230 12 105

Available Forms Of Inconel 718 | EN 2.4668

SheetsSheets Hover Turn
CoilsCoils Hover Turn
Round PipesRound Pipes Hover Turn
FlangesFlanges Hover Turn
Hex BarsHex Bar Hover Turn
Round BarsRound Bar Hover Turn
FittingsFittings Hover Turn
Square BarsSquare Bars Hover Turn
Square Rectangle Pipes TubesShape Pipes Hover Turn

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