DAIKOWT 718

GTAW
  • NICKEL ALLOYS
718

Description

High-strength nickel-based alloy 718 rod
Rod for welding alloy 718, with age-hardenable deposit offering mechanical properties comparable to the base material. The final properties depend on the post-weld heat treatment. Its excellent corrosion resistance makes it suitable for use in applications such as liquid fuel rocket components, rings, casings, stamped sheet metal parts for aircraft and land-based gas turbine engines, cryogenic tanks, and cladding in the oil and gas industry.
Specifications
EN ISO 18274
S Ni 7718
AWS A5.14
ERNiFeCr-2
Shielding
I1
Positions
PA, PB, PC, PD, PE, PF
Current
DC-
Packaging Type
5kg carton tube

Pren

27.4
Chem. Comp. %
DEFAULT
C
0.07
Mn
0.1
Ni
52
Cr
17.5
Nb
5
Al
0.4
P
0.008
S
0.001
Mo
3
Si
0.15
Cu
0.05
Fe
20.5
Ti
0.9
Mechanical Properties
min
variant
Tensile strength Rm MPa
1140 Age-hardened condition*
720
Yield strength Rp0.2 MPa
0
500
Elongation A (L0=5d0) %
0
60
Impact Charpy ISO-V
-
80J @ -196°C
Impact Charpy ISO-V
-
-
Welding Parameters
1.6 mm
2.4 mm
Ampere
80A - 120A
130A - 160A
Voltage
10V - 13V
14V - 18V
Packaging
Ø 1,0÷4,0mm
Ø 1,0÷4,0mm
Packaging Type
product.packaging_types.product.packaging_types.product.packaging_types.5kg carton tube
product.packaging_types.product.packaging_types.product.packaging_types.5kg carton tube
718
Description

Application

The subfamily 718 is specifically designed for welding the base metal alloy 718, ensuring exceptional corrosion resistance under various environmental conditions. The weld metal can be subjected to age-hardening treatment, thus granting it considerable mechanical properties that are closely influenced by post weld heat treatment (PWHT). It is commonly employed in tungsten arc welding processes of Cr-Ni-NB-Mo alloys, as the use of high heat input processes like GMAW can often cause microfissures. This alloy finds its main application in welding high-strength aerospace components, liquid fuel rocket parts, rings, casings, and various formed sheet elements for gas turbine engines used in land-based vehicles and aircraft, as well as in cryogenic tanks. It is also utilized for fasteners, instrumentation components, and for cladding and overlay of parts in the oil and gas industry. The temperature range of use spans from -250 °C to 700 °C.

Alloy Type

The nominal composition (wt. %) of filler metal of this classification is 52 Ni, 18 Fe, 19 Cr, 5 Nb plus Ta, 3 Mo, and 1 Ti.

Microstructure

Fully austenitic microstructure with Nb- and Ti-rich carbides.

Materials

Suitable for welding Cr-Ni-Nb-Mo alloy and 718, 706, and X-750 alloys.
  • EN W.Nr.: 2.4668 (NiCr19Fe19Nb5Mo3), 2.4669 (NiCr15Fe7TiAl)
  • ASTM: B637, 5589
  • UNS: N07718, N09706, N07750

Welding & PWHT

Before performing welding or heating any nickel-based alloy, it is essential to thoroughly clean the base metal. Oil, grease, paints, lubricants, marking pencils, temperature-indicating materials, thread compounds, and other similar materials may contain sulfur or lead, which can cause cracking or embrittlement of the base or filler metal during welding or heating. Welding of nickel-based and fully austenitic steels requires particular attention to minimize heat input, interpass temperature, and dilution with the base metal. It is advisable to maintain a low heat input, with a maximum of 1.5 kJ/mm, and an interpass temperature not exceeding 100 °C.

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