Chemical composition Element Weight percent Element Weight percent Ni 44.5 min Cr 20–24 Co 10–15 Mo 8–10 Al 0.8–1.5 C 0.05–0.15 Fe 3.0 max Mn 1.0 max Si 1.0 max S 0.015 max Ti 0.60 max Cu 0.50 max B 0.006 max — —

Mechanical properties Typical room-temperature properties of solution-annealed material, Special Metals Table 5. Flat-product results are transverse to rolling. Product form 0.2% yield MPa Tensile MPa Elongation % Hot-rolled plate 322 734 62 Hot-rolled bar 318 769 56 Cold-drawn tubing 383 758 56 Cold-rolled sheet / strip 351 755 58 The summary table does not state an exact solution-annealing cycle. Do not equate these typical values with standard minima or allowable design stresses.

Application areas Gas turbine ducting, combustion cans and transition liners High-temperature heat-exchange equipment Chemical-process and power-generation thermal equipment

Chemical composition Element Weight percent Element Weight percent Ni 44.5 min Cr 20–24 Co 10–15 Mo 8–10 Al 0.8–1.5 C 0.05–0.15 Fe 3.0 max Mn 1.0 max Si 1.0 max S 0.015 max Ti 0.60 max Cu 0.50 max B 0.006 max — —

Mechanical properties Typical room-temperature properties of solution-annealed material, Special Metals Table 5. Flat-product results are transverse to rolling. Product form 0.2% yield MPa Tensile MPa Elongation % Hot-rolled plate 322 734 62 Hot-rolled bar 318 769 56 Cold-drawn tubing 383 758 56 Cold-rolled sheet / strip 351 755 58 The summary table does not state an exact solution-annealing cycle. Do not equate these typical values with standard minima or allowable design stresses.

Application areas Gas turbine ducting, combustion cans and transition liners High-temperature heat-exchange equipment Chemical-process and power-generation thermal equipment

Alloy 617/UNS N06617

Grade: Inconel 617/UNS N06617/Alloy 617/Nickel Alloy 617/AIT 617/W.Nr. 2.4663/NCF617/NiCr23Co12Mo/NiCr22Co12Mo9

Sheet/Plate: 0.3mm-150mm

Strip/Foil: 0.02mm-16mm

Pipe: 6mm*0.5mm-1200mm*100mm

Bar: Ф6mm – Ф600mm

Wire: Ф0.01mm – Ф6mm

Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.

Standard: ASTM/ASME/AMS

INCONEL 617 is a nickel chromium cobalt molybdenum alloy intended for demanding thermal service. It combines solid-solution strength with resistance to oxidation and a range of corrosive environments. Conventional forming and welding methods can produce complex components from several mill forms. Applications emphasize sustained elevated-temperature loading, making creep behavior, fabrication history and the selected solution treatment central to material qualification.

Chemical composition

Element	Weight percent	Element	Weight percent
Ni	44.5 min	Cr	20–24
Co	10–15	Mo	8–10
Al	0.8–1.5	C	0.05–0.15
Fe	3.0 max	Mn	1.0 max
Si	1.0 max	S	0.015 max
Ti	0.60 max	Cu	0.50 max
B	0.006 max	—	—

Mechanical properties

Typical room-temperature properties of solution-annealed material, Special Metals Table 5. Flat-product results are transverse to rolling.

Product form	0.2% yield MPa	Tensile MPa	Elongation %
Hot-rolled plate	322	734	62
Hot-rolled bar	318	769	56
Cold-drawn tubing	383	758	56
Cold-rolled sheet / strip	351	755	58

The summary table does not state an exact solution-annealing cycle. Do not equate these typical values with standard minima or allowable design stresses.

Application areas

Gas turbine ducting, combustion cans and transition liners
High-temperature heat-exchange equipment
Chemical-process and power-generation thermal equipment

Introduction

Specification

Chemical composition

Element	Weight percent	Element	Weight percent
Ni	44.5 min	Cr	20–24
Co	10–15	Mo	8–10
Al	0.8–1.5	C	0.05–0.15
Fe	3.0 max	Mn	1.0 max
Si	1.0 max	S	0.015 max
Ti	0.60 max	Cu	0.50 max
B	0.006 max	—	—

Mechanical

Mechanical properties

Typical room-temperature properties of solution-annealed material, Special Metals Table 5. Flat-product results are transverse to rolling.

Product form	0.2% yield MPa	Tensile MPa	Elongation %
Hot-rolled plate	322	734	62
Hot-rolled bar	318	769	56
Cold-drawn tubing	383	758	56
Cold-rolled sheet / strip	351	755	58

The summary table does not state an exact solution-annealing cycle. Do not equate these typical values with standard minima or allowable design stresses.

Application