UNS N07718 Inconel 718 Nickel Alloy Fasteners Hex Nut M5-M64 DIN
555 ISO 4034
1.Inconel 718 description
INCONEL alloy 718 (UNS N07718/W.Nr. 2.4668) is a high-strength,
corrosion-resistant nickel chromium
material used at -423° to 1300°F. Typical composition limits are
shown in Table 1. The age-hardenable
alloy can be readily fabricated, even into complex parts. Its
welding characteristics, especially its
resistance to postweld cracking, are outstanding. The ease and
economy with which INCONEL alloy 718
can befabricated, combined with good tensile, fatigue, creep, and
rupture strength, have resulted in its use
in a wide range of applications. Examples of these are components
for liquid fueled rockets, rings, casings
and various formed sheet metal parts for aircraft and land-based
gas turbine engines, and cryogenic
tankage. It is also used for fasteners and instrumentation parts
2. Fasteners Specification:
3.Fasteners package method
Often small hardware, fasteners and other parts are packaged in
bags and displayed in bins or on hangers.
Bagging is the most effective way to package and organize small
parts, while also being the most flexible
and affordable. In order to better protect the products during transportation, we
will pack the packed
products in wooden cases.
4.Fasteners Application
A fastener (US English) or fastening (UK English) is a hardware
device that mechanically joins or affixes two
or more objects together. In general, fasteners are used to create
non-permanent joints; that is, joints that
can be removed or dismantled without damaging the joining
components. Welding is an example of creating
permanent joints. Steel fasteners are usually made of stainless
steel, carbon steel, or alloy steel.
5.Inconel 718 Fasteners
Nickel content above includes cobalt. Iron content as remainder.
Developed in the early 1960’s, IN718 is still
considered the material of choice for the majority of aircraft
engine components with service temperatures
below 1200°F (650°C). Inconel 718 is a precipitation-hardenable
nickel-chromium alloy containing also
significant amounts of iron, niobium, and molybdenum along with
lesser amounts of aluminum and titanium.
It combines corrosion resistance and high strength with outstanding
weldability including resistance to
postweld cracking. The alloy has excellent creep-rupture strength
at temperatures to 1300°F (700°C).
Applications: Aerospace, gas turbines, rocket motors, spacecraft, space
shuttles, nuclear reactors,
pumps, turbo pump seals, and tooling.
Forms: round, flat, extruded section, pipe, tube, forging stock, plate,
sheet, strip and wire.
6.Delivery:
Port:
Tianjin/Shanghai/Ningbo
Lead Time :
| Quantity(Pieces) | 1 - 100 | >100 |
| Est. Time(days) | 10 | To be negotiated
|
Why Choose Us
1.One-Stop Service,One Single Source.
2.No MOQ.
3.Best quality,competitive price
4.Fast Reply.
5.On-Time Delivery.
6.Professional sales and technical team .
