Nickel Alloy Incoloy A-286 UNS S66286

Short Introduction:

HY A-286 / IncoloyA-286 / GB GH2132 / UNS S66286 / SEW VDIUVW. Nr.1.4980 / AFNOR ZbNCT25 is an alloy that is precipitation hardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The alloy’s high strength and excellent fabrication characteristics make it useful for various components of aircraft and industrial gas turbines. Applications include blades, vanes, shafts, tail cones, afterburners, springs, and fasteners. This alloy is also used for automotive applications.

Fob price: US $ 25 - 80 / Kilogram

Min.order quantity: 300kg

Port: Shanghai

Payment terms: L/C,T/T,30% down payment after order, balance against copy of B/L

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HY A-286 Chemical composition:

Alloy	%	Ni	Cr	Mo	B	Fe	Al	Ti	C	Mn	Si	V	S
HY A-286	Min.	24	13.5	1.0	0.001			1.9				0.1
HY A-286	Max.	27	16	1.5	0.01	Balance	0.35	2.35	0.08	2.0	1.0	0.5	0.03

HY A-286 Physical properties:

Density	7.93 g/cm3
Melting point	1364-1424℃

HY A-286 minimum mechanical properties in the room temperature:

Status	Tensile strength Rm N/mm2	Yield strength RP0.2N/mm2	Elongation A5 %
HY A-286	950	680	28

An alloy that is precipitation hardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The alloy’s high strength and excellent fabrication characteristics make it useful for various components of aircraft and industrial gas turbines. Applications include blades, vanes, shafts, tail cones, afterburners, springs, and fasteners. This alloy is also used for automotive applications.

Specifications：

Rod, Bar, Wire and Forging Stock	ASTM A 638;ASME SA 638;SAE AMS 5726;SAE AMS 5731;SAE AMS 5732;SAE AMS 5734;SAE AMS 5737;SAE AMS 5895;BS HR 51;BS HR 52;AECMA PrEn2171;AECMA PrEN2119;AECMA PrEN2172;AECMA PrEN2173;AECMA PrEN2174;AECMA PrEN2303;AECMA PrEN2304;AECMA PrEN2398;AECMA PrEN2399;AECMA PrEN3510
Plate, Sheet and Strip	SAE AMS 5525;SAE AMS 5858;AECMA PrEN2175;AECMA PrEN241
Pipe & Tube	SAE AMS 5731;SAE AMS 5732;SAE AMS 5734;SAE AMS 5737;SAE AMS 5895

Regular shape for all kinds of alloys
Form	Specification	Supply Form	Others
Sheet	Thickness：0.40-4.75mm，General Width：1000、1219、1500mm	Whole Coil or piece of it	Cold Annealed，Surface 2B、2E
Plate	Thickness：4.76-60mm，Width：1500、2000、2500mm，Length：3000、6000、8000、8500mm（Under 10mm plate can be coiled）	Whole Coil or piece of it	Single hot rolling，Solid solution annealed state，Surface 1D
Belt	Thickness：0.10-3.0mm，Width：50-500mm	Whole Coil or Specified size	Cold Annealed，Surface 2B、2E
Bar & Rod	Rolled barΦ5-45mm，Length≤1500mm	Polished Bar（circle、Square）	Solution annealing,descaling
Bar & Rod	Forged barΦ26-245mm，Length≤4000mm	Polished Bar（circle、Square）	Solution annealing,descaling
Weld tube	Outer diameterΦ4.76-135mm，Wall Thickness0.25-4.00mm，Length：≤35000 mm	Base on your requirement
Seamless Tube	Outer diameterΦ3-114mm，Wall Thickness0.2-4.5mm	Base on your requirement
Wire	Outer diameterΦ0.1-13mm	Base on your requirement	Ni & Ni alloy, Ti & Ti alloy
Forged piece	discs,rings,squares,blocks,slabs	Base on your requirement	Steel, Alloy
Flangs	All kinds of Flangs	Base on your requirement	Steel, Alloy
Welding Material	Coil wire Φ0.025mm-1.6mm	Base on your requirement	Certificate of Origin：America, Sweden, Britain, Germany, Austria, Italy, France.
	Straight WireΦ1.6mm-4.0mm
	Welding rodΦ1.2mm-4.0mm
Tube	Elbow, three links, four links, different diameter size	Base on your requirement	Ni & Ni alloy, Ti & Ti alloy
Explosive bonded laminate	Raw Sheet Thickness≥2mm	Base on your requirement	Ni & Ni alloy, Ti & Ti alloy