Chemical composition Element Weight percent Element Weight percent Ni + Co 42–45 combined Fe Balance Cr 15.5–17.5 Mo 2.8–3.8 Ti 1.1–1.3 Al 1.1–1.3 C 0.04–0.08 Si 0.5 max Mn 0.2 max Co 2.0 max Cu 0.5 max B 0.005 max Zr 0.02–0.04 S 0.015 max Ag 0.0005 max Bi 0.0001 max Pb 0.0015 max — —

Mechanical properties Typical sheet tensile properties, bulletin Table 7. Heat treatment: 15 min at 1040°C / air cool + 1 h at 900°C / air cool + 8 h at 750°C / air cool. Elongation gauge length: 50 mm. Test temperature °C 0.2% proof MPa Tensile MPa Elongation % 20 539 950 26.9 500 476 809 24.3 600 483 806 24.5 700 489 672 36.8 800 306 380 46.1 Values describe one sheet treatment and must not be transferred to bar or to the alternative 800°C / 700°C aging treatment.

Application areas Gas turbine flame tubes Aircraft ducting and missile hot sections Nuclear reactor components Superheater tubing

Chemical composition Element Weight percent Element Weight percent Ni + Co 42–45 combined Fe Balance Cr 15.5–17.5 Mo 2.8–3.8 Ti 1.1–1.3 Al 1.1–1.3 C 0.04–0.08 Si 0.5 max Mn 0.2 max Co 2.0 max Cu 0.5 max B 0.005 max Zr 0.02–0.04 S 0.015 max Ag 0.0005 max Bi 0.0001 max Pb 0.0015 max — —

Mechanical properties Typical sheet tensile properties, bulletin Table 7. Heat treatment: 15 min at 1040°C / air cool + 1 h at 900°C / air cool + 8 h at 750°C / air cool. Elongation gauge length: 50 mm. Test temperature °C 0.2% proof MPa Tensile MPa Elongation % 20 539 950 26.9 500 476 809 24.3 600 483 806 24.5 700 489 672 36.8 800 306 380 46.1 Values describe one sheet treatment and must not be transferred to bar or to the alternative 800°C / 700°C aging treatment.

Application areas Gas turbine flame tubes Aircraft ducting and missile hot sections Nuclear reactor components Superheater tubing

Alloy PE16/Nimonic PE16

Grade: Nimonic PE16/UNS N09016/Alloy PE16

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

NIMONIC PE16 is a nickel iron chromium alloy combining molybdenum strengthening with titanium and aluminum precipitation hardening. It was developed for elevated-temperature structures requiring strength together with practical forming and welding behavior. Different aging treatments adjust the balance between proof strength and ductility. Its established uses include turbine flame tubes, aircraft ducting, reactor components and superheater tubing.

Chemical composition

Element	Weight percent	Element	Weight percent
Ni + Co	42–45 combined	Fe	Balance
Cr	15.5–17.5	Mo	2.8–3.8
Ti	1.1–1.3	Al	1.1–1.3
C	0.04–0.08	Si	0.5 max
Mn	0.2 max	Co	2.0 max
Cu	0.5 max	B	0.005 max
Zr	0.02–0.04	S	0.015 max
Ag	0.0005 max	Bi	0.0001 max
Pb	0.0015 max	—	—

Mechanical properties

Typical sheet tensile properties, bulletin Table 7. Heat treatment: 15 min at 1040°C / air cool + 1 h at 900°C / air cool + 8 h at 750°C / air cool. Elongation gauge length: 50 mm.

Test temperature °C	0.2% proof MPa	Tensile MPa	Elongation %
20	539	950	26.9
500	476	809	24.3
600	483	806	24.5
700	489	672	36.8
800	306	380	46.1

Values describe one sheet treatment and must not be transferred to bar or to the alternative 800°C / 700°C aging treatment.

Application areas

Gas turbine flame tubes
Aircraft ducting and missile hot sections
Nuclear reactor components
Superheater tubing

Introduction

Specification

Chemical composition

Element	Weight percent	Element	Weight percent
Ni + Co	42–45 combined	Fe	Balance
Cr	15.5–17.5	Mo	2.8–3.8
Ti	1.1–1.3	Al	1.1–1.3
C	0.04–0.08	Si	0.5 max
Mn	0.2 max	Co	2.0 max
Cu	0.5 max	B	0.005 max
Zr	0.02–0.04	S	0.015 max
Ag	0.0005 max	Bi	0.0001 max
Pb	0.0015 max	—	—

Mechanical

Mechanical properties

Typical sheet tensile properties, bulletin Table 7. Heat treatment: 15 min at 1040°C / air cool + 1 h at 900°C / air cool + 8 h at 750°C / air cool. Elongation gauge length: 50 mm.