Inconel 713C/Inconel K418

Inconel 713C/Inconel K418

Model No.:

Inconel 713C, Alloy 713C,Inconel K418

Introduction:

Available Shapes:Rod Bar,pipe,Other Fittings

Product Detail

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Inconel 713C/Inconel K418

Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). 

Inconel 713C Chemical Compositons:

Alloy

%

Ni

Cr

Fe

Mn

Si

Mo

Zr

Ti

Cu

Co

Al

C

S

713C

Min.

Bal

12.0

-

-

-

3.8

0.05

0.5

-

1.8

5.5

-

-

Max.

14.0

2.5

0.25

0.5

5.2

0.15

1.0

0.5

2.8

6.5

0.20

0.015

Inconl 713C Physical properties

Density

7.913 g/cm³

Melting point

1260℃-1288℃

Inconel 713C Mechinabity Physical                     

  • High-speed tungsten-cobalt or molybdenum-tungsten-vanadium toolsCutting lubricants:

  • Chlorinated, sulfurized fatty mineral oil

  • Rich emulsion of 10 parts water and 1 part soluble oil

  • Aluminum oxide

  • Vitrified bond of medium or soft hardness and medium open structure

  • Use 1 pound of sal soda with 25 gallons of water, or chemically active grinding coolant

Inconel 713C Weledablity                                                   

  • Inconel 713C can be used in applications using very low restraint

  • Use Inco-Weld A electrode

  • Flash-butt weld

  • Inconel 713C is also good for hydrogen-atmosphere brazing with normal high-heat brazing alloy with electroplated mating surfaces

Inconel 713C Applications 

Inconel 713C is most commonly used for jet engine gas turbine blades.


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