Haynes HR160
2026-04-10 07:25:00 Origin： Remark：0 Click：
Specifications Haynes HR160 data sheet, chemical, Haynes HR160 properties from Steelmaking, ESR & VAR technique, hot bloomed, forged, rolled, heat treated
TECHNICAL DATA SHEET - Haynes HR160
Official test report: issued by TUV - SGS - CNAS
Material category: Ni-Co-Cr--Si base superalloy
Typical chemical compositions (mass weight - %)
Carbon, C (％): 0.05 ~ 0.10
Carbon, C (％): 0.05 ~ 0.10
Silicon, Si (％): 2.40 ~ 3.00
Manganese, Mn (％): ≤ 1.00
Phosphorus, P (％): ≤ 0.030
Manganese, Mn (％): ≤ 1.00
Phosphorus, P (％): ≤ 0.030
Sulfur, S (％): ≤ 0.015
Chromium, Cr (％): 25.0 ~ 30.0
Chromium, Cr (％): 25.0 ~ 30.0
Nickel, Ni (％): 37.0 Min.
Molybdenum, Mo (％): ≤ 1.00
Cobalt, Co (%): 27.0 ~ 33.0
Cobalt, Co (%): 27.0 ~ 33.0
Tungsten, W (%): ≤ 1.00
Aluminum, Al (%): ≤ 0.40
Aluminum, Al (%): ≤ 0.40
Copper, Cu (%): -
Titanium, Ti (%): -
Ferrum, Fe (% ): ≤ 3.50
TYPICAL MECHANICAL PROPERTIES
Tensile strength, σb ≥ MPa: 620
Yield strength, σ0.2 / MPa: 240
Elongation, δ5 ≥ (％): 40.0
Reduction of area, ф ≥ (％): -
Hardness via heat treatment /HBW: -
Reduction of area, ф ≥ (％): -
Hardness via heat treatment /HBW: -
TYPICAL APPLICATIONS
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on. The alloy is usually produced by AOD / VOD /VIM followed by electroslag refining (ESR) / VAR if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied bright surface in the solution annealed condition.
Final heat treatment - solution + Aged or Double aged.
FORMS & DIMENSIONS
Round bar / disc (diameter): 6.0 ~ 850 mm
Square bar / flat bar: 10 ~ 550 mm
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on. The alloy is usually produced by AOD / VOD /VIM followed by electroslag refining (ESR) / VAR if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied bright surface in the solution annealed condition.
Final heat treatment - solution + Aged or Double aged.
FORMS & DIMENSIONS
Round bar / disc (diameter): 6.0 ~ 850 mm
Square bar / flat bar: 10 ~ 550 mm
Wire rod (Diameter): 0.50 ~ 16 mm
Steel strip via cold rolled: T0.5 ~ 3 X W15 ~ 650 X L (or in coil form)
Forging piece: Different shapes based on OEM.
Steel strip via cold rolled: T0.5 ~ 3 X W15 ~ 650 X L (or in coil form)
Forging piece: Different shapes based on OEM.
Other sizes can be supplied to meet specific requirements.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers - E-mail: sales@ccsteels.com.
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers - E-mail: sales@ccsteels.com.
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