Wednesday, 30 November 2016

Inconel X750 alloy/ UNS N07750/ W.Nr. 2.4669 Metallography

The Metallography of Inconel X750 alloy


Metallography Characteristic:


Inconel alloy x750, which contains aluminum and titanium, is made precipitation-hardenable by the combination, during heat treatment, of thest elements with nickel to form gamma prime (γ), the intermetallic compound Ni3(Al, Ti).

When alloy x750 is solution-treated at 2100℉,the number of dislocations and crystal defects are reduced, and γ and soluble carbides go into solution. For best results, the material should be in a fairly heavily worked condition prior to the treatment to ensure rapid and complete recrystallization. Once the material has been solution-treated, it should not be subjected to any cold work since it will generate new dislocations and thus impair rupture properties.

Creep resistance of alloy x750 stems from the uniform dispersion of intragranular γ; whereas rupture properties are more closely related to grain-boundary area microstructure. During the 1550℉/24 hr stabilization treatment of the triple heat treatment, fine γ appears in the grain interiors and M23C6 is precipitated in the grain boundary;adjacent to the grain boundary is a zone denuded of γ. On precipitation treating (1300℉/20 hr),γ has precipitated in this denuded zone. γ particles arrest the motion of moving dislocations, thereby increasing tensile and creep-rupture properties.

During M23C6 transformation at 1550℉, the carbon is essentially stabilized, without leaving chromium-depleted areas at the grain boundaries. This stabilization improves the resistance of nickel-chromium alloys to attack by certain corrosive media.

By Lowering the precipitation temperature from 1350℉ to 1150℉, as described for certain specific heat treatments, additional γ can be caused to nucleate in smaller particles, increasing the hardening effect and thereby improving tensile properties.





Tuesday, 29 November 2016

Inconel X750 alloy/ UNS N07750/ W.Nr. 2.4669 characteristic properties

The Characteristic Properties of Inconel X750 alloy


Inconel x750 characteristic properties:

Inconel alloy X750/ UNS N07750/ W.Nr. 2.4669 is a precipitation hardenable nickel-chromiun alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300℉. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300℉, heat-treated material has useful strength up to 1800℉. Alloy X750 also has excellent properties down to cryogenic temperatures.

Inconel X750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Other applications are heat treating fixtures, forming tools, extrusion dies, test machine grips and large pressure vessels.

For springs and fasterners, inconel alloy X750 is used from sub-zero to 1200℉




Monday, 28 November 2016

The Mechanical Properties of Inconel 718 alloy

The Mechanical Properties of Inconel 718 alloy


Inconel alloy 718 is produced under the NACE MR0175 which requires the solution annealed and aged material to meet a max. hardness value of 40 Rockwell C. It is typically solution heat treated at 1850-1900℉ and aged at 1450℉ for six to eight hours and air cooled.


The mechanical properties of inconel 718

ConditionCold worked solution
annealed & aged
Hot worked,
solution
annealed &
aged
Hot worked, solution
annealed & aged
Diameter, in. (mm)0.5(12.7) to
3(76.2)
inclusive
0.5(12.7) to
8(203.2)
inclusive
8(203.2) to
10(254),
inclusive
Tensile Strength,
ksi(Kg/cm2)
min.150(10545)150(10545)150(10545)
Yield Strength
(0.2% Offset),
ksi (Kg/cm2)
min.120(8436)120(8436)120(8436)
max.140(9842)140(9842)140(9842)
Elongation in
2in.(50.8mm)
or 4D%, min
min202020
Reduction
of Area, %
min252525
Impact Strength,
ft.lb(kg.m)
min.
average
40(5.55)40(5.55)40(5.55)
Hardnessmin303030
max404040



Tuesday, 22 November 2016

The Electrical and Thermal Properties of Inconel 617

The eletrical and thermal properties of inconel 617 alloy/UNS N06617/W.Nr.2.4663a


Eletrical and Thermal Properties of Inconel 617

TemperatureElectrical ResistivityThermal ConductivityCoefficient of ExpansionSpecific Heat
°Fohm·circ·mil/ftBtu-in/ft2-h-F10-6in./in./°FBtu/lb-°F
7873694-0.1
20074810170.104
4007571137.20.111
6007641257.40.117
8007701377.60.124
10007791497.70.131
120079316180.137
14008071738.40.144
16008031858.70.15
180082419790.157
2000-2099.20.163
°CµΩ-mW/m·℃µm/m-J/kg·℃
201.22213.4-419
1001.24514.711.6440
2001.25816.312.6465
3001.26817.713.1490
4001.27819.313.6515
5001.2920.913.9536
6001.30822.514561
7001.33223.914.8586
8001.34225.515.4611
9001.33827.115.8636
10001.37828.716.3662

Monday, 21 November 2016

The Mechanical Properties of Inconel 617 alloy

The Mechanical Properties of Inconel 617/ UNS N06617/ W.Nr. 2.4663a)


Mechanical Properties of Inconel617 alloy

Product FormPlate BarTubingSheet or Strip
Production MethodHot RollingHot RollingCold DrawingCold Rolling
Yield Strength
(0.2% Offset)
ksi46.746.155.650.9
Mpa322318383351
Tensile Strengthksi106.5111.5110109.5
Mpa734769758755
Elongation%62565658
Reduction of Area%5650--
Hardness BHN172181193173






Wednesday, 16 November 2016

The Mechanical Properties of Inconel alloy 625

The Temperature Mechanical Properties of Inconel alloy 625



Temperature Mechanical Properties of Inconel 625
Form And ConditionTensile StrengthYield Strength
(0.2% Offset)
ElongationReduction of AreaHardness Brinell
ksiMpaksiMpa%%
ROD, BAR, PLATE
As-Rolled120-160827-110360-110414-75860-3060-40175-240
Annealed120-150827-103460-95414-65560-3060-40145-220
Solution-Treated105-130724-89642-60290-41465-4090-60116-194
SHEET and STRIP
Annealed120-150827-103460-90414-62155-30-145-240
Tube and Pipe,
COLD-DRAWN
Annealed120-140827-96560-75414-51755-30--
Solution-Treated100-120689-82740-60276-41460-40--