Ernifecr 2



ERNiFeCr-2

  • Strength, AWS 5.14 ERNiFeCR-2 filler metal can be used. Solution annealing of the alloy should be performed prior to aging to dissolve phases in the microstructure that may have formed during previous processing. If the material is hot finished, then the anneal temperature should be 1800°F. If the material is cold worked, then.
  • AWS 5.14 AWS ERNiFeCr-2 ASME SFA 5.14 UNS N07718 TYPICAL MECHANICAL PROPERTIES Tensile strength: 125,000 psi 860 MPa Yield strength: 91,000 psi 630 MPa Elongation: 27% AWS Chemical Composition Ni C Mn Fe S Si Cu 50.0-55.0 0.08 max 0.35 max Bal 0.015 max 0.35 max 0.30 max.

*Specification

ERNiFeCr-1. Specification AWS/ASME Spec 5.14 AWS Class ERNiFeCr-1 UNS N08065. Chemical Composition,%. Typical Welding Parameter & Mechanical Property. Feature Used for welding of nickel-chromium-molybdenum-copper alloys. Also can be used to overlay cladding where similar chemical composition is required. Application Application Used for welding of nickel-chromium-molybdenum.

AWS/ASME Spec 5.14

AWS Class ERNiFeCr-2

UNS N07718

*Chemical Composition,%

C

Mn

Si

Cr

S

P

Ni

Fe

Cu

Al

Mo

Ti

Nb+Ta

≤0.08

≤0.35

≤0.35

17-21

≤0.015

≤0.015

50-55

Rest

≤0.3

0.2-0.8

2.8-3.3

0.65-1.15

4.75-5.5

*Typical Welding Parameter & Mechanical Property

Ernifecr-2

Diameter

Process

Volt

Amps

Shielding Gas

In

mm

0.035

0.9

GMAW

26-29

150-190

Spray Transfer

100% Argon

0.045

1.2

GMAW

28-32

180-220

1/16

1.6

GMAW

29-33

200-250

1/16

1.6

GTAW

14-18

90-130

100% Argon

3/32

2.4

GTAW

15-20

120-175

100% Argon

1/8

3.2

GTAW

15-20

150-220

100% Argon

Tensile Strength MPa(ksi)

Yield Strength MPa(ksi)

Elongation %

AWS requirement

1140(165)

Not specified

Not specified

Typical results as welded

860(125)

630(91)

27

*Feature

Primarily for welding high strength aircraft components and liquid rocket components involving cryogenic temperatures.

Ernifecr

High heat input processes such as MIG welding often result in micro fissuring. This alloy can be age hardened to higher strengths.

*Application

Used for welding alloys 718, 706 and X-750.

Class: ERNiFeCr-2
AWS: A5.14

Conforms to Certification: AWS A5.14 | ASME SFA A5.14

Weld Process: GTAW Welding Process

AWS Chemical Composition Requirements
C = 0.08 maxCu = 0.30 max
Mn = 0.35 maxNi = 50.0 – 55.0
Fe = RemainderAl = 0.20 – 0.80
P = 0.015 maxTi = 0.65 – 1.15
S = 0.015 maxCr = 17.0 – 21.0
Si = 0.35 maxNb + Ta = 4.75 – 5.50
Mo = 2.80 – 3.30Other = 0.50 max

Available Sizes
.035 x 36
.045 x 36
1/16 x 36
3/32 x 36
1/8 x 36

Application
ERNiFeCr-2 (NA718) filler metal is used by gas tungsten arc welding process for Cr-Ni-Nb-Mo alloys. Use of high heat input process such as mig often results in micro-fissuring.

Deposited Chemical Composition % (Typical)
C = 0.04Si = 0.12Ni = 52.5
Mn = 0.25Cr = 19.0Nb/Ta = 5.0
Fe = BalanceMo = 3.0S = 0.009

Ernifecr-2

Deposited Charpy-V-Notch Impact Properties %
Not applicable

Recommended Welding Parameters for TIG, MIG, and SAW Welding of Nickel Alloys

ProcessDiameter of WireVoltage (V)Amperage (A)Gas
Tig.035 inches x 3612 – 1560 – 90100% Argon
.045 inches x 3613 – 1680 – 110100% Argon
1/16 inches x 3614 – 1890 – 130100% Argon
3/32 inches x 3615 – 20120 – 175100% Argon
1/8 inches x 3615 – 20150 – 220100% Argon

Note: Other shielding Gases may be used for Tig welding. Shielding gases are chosen taking Quality, cost, and Operability into consideration.

Note: Both agglomerated and fused fluxes can be used for submerged arc welding.

Note: The chemical composition of the flux mainly affects the chemistry of the weld metal and consequently its corrosion resistance and mechanical properties.