Inconel X-750 - ASTM B693
Inconel X-750 is a high temperature nickel alloy that is highly resistant to chemical corrosion and oxidation. It has high stress-rupture strength and low creep rates under high stresses at temperatures up to 1500°F. Alloy X-750 is the most common type of Inconel and is an excellent choice when designing a flat spring for extreme temperature environments.
Nominal Chemical and Physical Properties of Inconel X750:
Minimum Tensile Strength psi x 103 150
E - Modulus of Elasticity psi x 106 31
Maximum Operating Temperature 750-1100°F
Rockwell Hardness C30 Min
Inconel X750 is cold drawn and precipitation hardened after fabrication.
Inconel X750 is used to fabricate flat springs and sheet metal stampings that are used in very high temperature applications such as jet engine parts, nuclear power plant applications, heat-treating fixtures, forming tools, and extrusion dies.
Common Trade Names of Inconel X750:
AMS 5698, 5699
|Minimum Order Quantity||50 Kilogram|
|Size Diameter||0.5 to 200mm Thickness|
|Material Grade||Inconel X750|
|Type||Nickel Plate,Alloy Steel plate|
|Material||UNS N07752,UNS N07750,W Nr 2.4669|
|W.Nr.||W Nr 2.4669|
|Uns||UNS N07752,UNS N07750|
|Chemical Composition Limits|
|Weight %||Ni +(Co)||Cr||Fe||Ti||Al||Nb + (Ta)||Mn||Si||S||Cu||C||Co|
|70 min||14-17||5-9||2.25-2.75||0.40-1.0||0.70-1.2||1 max||0.50 max||0.01 max||0.50 max||0.08 max||1 max|
|UNS N07752 is available in billets for forging. UNS N0772 has limits of 0.05% on both Carbon and Cobalt|
Alloy X-750 is a nickel-chromium alloy which has been made precipitation-hardenable by the additions of aluminum and titanium. Alloy X-750 has good resistance to corrosion and oxidation along with high tensile and creep rupture properties at temperature up to 1300ºF (700ºC). Due to X-750's excellent relaxation resistance it is useful for applications as high-temperature springs and bolts, X-750 is also used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling and aircraft structures.
AMS 5667 - 1625°F/24hr, AC + 1300°F/20 hr, AC (Equalising plus precipitation treatment). AMS 5667 Rod, Bars and Forgings have high strength and notch rupture ductility up to 1100°F
AMS 5668 - 2100°F anneal + 1550°F/24 hr, AC, +1300°F/20hr, AC (triple heat treatment). AMS 5668 has maximum creep, relaxation and rupture strength above about 1100°F.
AMS 5670 - 1800°F anneal + 1350°F/8hr, FC to 1150°F. Hold at 1150°F for total precipitation-treating time 18 hr, AC (solution treatment plus furnace cool precipitation treatment). Due to the heat treatments AMS 5670, AMS 5671 and AMS 5747 have increased tensile properties and reduced heat treatment time service up to about 1100°F.
AMS 5542 - 1300°F/20hr, AC (Constant-temperature precipitation treatment). AMS 5542 has high strength up to 1300°F
AMS 5598 - 1350°F/8hr, FC to 1150°F, hold at 1150°F for total precipitation-treating time of 18hr, AC (furnace-cool precipitation treatment. AMS 5598 has high strength up to 1300°F (Increased tensile properties to about 1100°F).
With heat treatment 1400°F/1hr, FC to 1150°F hold at 1150°F for total time of 6hr, AC (short furnace-cool precipitation treatment).
Type: Rods , Bars ,Pellets
|Rod||ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269|
|Bar||ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269|
|Forging Stock||ASTM B 637, ASME SB 637, ISO 9723, ISO9724, ISO9725, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5747, EN10269|
|Plate||ISO 6208, AMS 5542 and AMS 5598|
|Sheet||ISO 6208, AMS 5542 and AMS 5598|
|Strip||ISO 6208, AMS 5542 and AMS 5598|
|Wire||BS HR 505, AMS 5698, AMS 5699|
|Other||UNS N07750, W.Nr 2.4669, Inconel X750 (tradename), UNS N07752|
|Minimum Order Quantity||50 Kilogram|
|Surface Finish||Finished Polished|
Aluminium alloy 6063 is a medium strength alloy commonly referred to as an architectural alloy. It is normally used in intricate extrusions.
It has a good surface finish, high corrosion resistance, is readily suited to welding and can be easily anodised. Most commonly available as T6 temper, in the T4 condition it has good formability.Applications of 6063 Aluminium
Aluminium alloy 6063 is used in:
In balustrading the rails and posts are normally in the T6 temper and formed elbows and bends are T4. T4 temper 6063 aluminium is also finding applications in hydroformed tube for chassis.Alloy Designations
Aluminium alloy 6063/6063A also corresponds to the following standard designations and specifications:
Table 1. Chemical composition for aluminium alloy 6063 and 6063A
|Element||6063 % Present||6063A % Present|
|Si||0.2 to 0.6||0.3 to 0.6|
|Fe||0.0 to 0.35||0.15 to 0.35|
|Cu||0.0 to 0.1||0.1|
|Mn||0.0 to 0.1||0.15|
|Mg||0.45 to 0.9||0.6 to 0.9|
|Zn||0.0 to 0.1||0.0 to 0.15|
|Ti||0.0 to 0.1||0.1|
The most common tempers for 6063 aluminium are: