Chemical composition Element Weight percent Element Weight percent Ni Balance Co 20 Cr 20 Mo 6 Fe 0.70 max Mn 0.40 Si 0.20 Al 0.60 max Ti 2.40 max C 0.06 B 0.005 max Zr 0.04 max Al + Ti 2.60 — —

Mechanical properties Cold-rolled sheet, mill annealed then aged at 800°C for 8 h and air cooled. Manufacturer typical tensile data. Test temperature °C 0.2% yield MPa Tensile MPa Elongation % RT 615 1041 35.8 649 518 901 36.9 760 524 696 26.6 871 296 348 58.1 Source: Haynes International 263 alloy data. Typical values; not purchase acceptance limits.

Application areas Aircraft turbine fabricated components Industrial gas turbine components Low-temperature combustors Transition liners and selected ring components

Chemical composition Element Weight percent Element Weight percent Ni Balance Co 20 Cr 20 Mo 6 Fe 0.70 max Mn 0.40 Si 0.20 Al 0.60 max Ti 2.40 max C 0.06 B 0.005 max Zr 0.04 max Al + Ti 2.60 — —

Mechanical properties Cold-rolled sheet, mill annealed then aged at 800°C for 8 h and air cooled. Manufacturer typical tensile data. Test temperature °C 0.2% yield MPa Tensile MPa Elongation % RT 615 1041 35.8 649 518 901 36.9 760 524 696 26.6 871 296 348 58.1 Source: Haynes International 263 alloy data. Typical values; not purchase acceptance limits.

Application areas Aircraft turbine fabricated components Industrial gas turbine components Low-temperature combustors Transition liners and selected ring components

Alloy 263/UNS N07263

Grade: Haynes 263/UNS N07263/Nimonic 263

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

HAYNES 263, also known commercially as NIMONIC 263, is an age-hardenable nickel cobalt chromium molybdenum alloy. Gamma-prime precipitation provides elevated-temperature strength, while the annealed material offers good forming and welding behavior. Its fabrication characteristics make it useful for complex turbine components. It is commonly considered for service up to approximately 900°C, with material condition and component stresses determining the practical operating limit.

Chemical composition

Element	Weight percent	Element	Weight percent
Ni	Balance	Co	20
Cr	20	Mo	6
Fe	0.70 max	Mn	0.40
Si	0.20	Al	0.60 max
Ti	2.40 max	C	0.06
B	0.005 max	Zr	0.04 max
Al + Ti	2.60	—	—

Mechanical properties

Cold-rolled sheet, mill annealed then aged at 800°C for 8 h and air cooled. Manufacturer typical tensile data.

Test temperature °C	0.2% yield MPa	Tensile MPa	Elongation %
RT	615	1041	35.8
649	518	901	36.9
760	524	696	26.6
871	296	348	58.1

Source: Haynes International 263 alloy data. Typical values; not purchase acceptance limits.

Application areas

Aircraft turbine fabricated components
Industrial gas turbine components
Low-temperature combustors
Transition liners and selected ring components

Introduction

Specification

Chemical composition

Element	Weight percent	Element	Weight percent
Ni	Balance	Co	20
Cr	20	Mo	6
Fe	0.70 max	Mn	0.40
Si	0.20	Al	0.60 max
Ti	2.40 max	C	0.06
B	0.005 max	Zr	0.04 max
Al + Ti	2.60	—	—