Chemical composition Element Weight percent Element Weight percent Ni 37–41 Fe Balance Cr 17–19 Mo 4.75–5.75 Ti 2.2–2.5 Al 0.7–1.0 C 0.03–0.08 Si 0.5 max Cu 0.5 max Mn 0.2 max Co 1.0 max B 0.001 max Zr 0.02–0.05 S 0.015 max

Mechanical properties Typical 1,000-hour rupture strength, precipitation-hardened condition; Special Metals handbook, printed page 32. Product form and the exact heat-treatment cycle are not specified in this summary. Test temperature °C 1,000 h rupture strength MPa 650 340 705 250 760 140 The bulletin supplies tensile curves, not a numerical tensile table. The rupture data are typical characterization values; their test temperatures do not establish a recommended service-temperature limit.

Application areas Gas turbine components Welded high-strength sheet fabrications for turbine service

Chemical composition Element Weight percent Element Weight percent Ni 37–41 Fe Balance Cr 17–19 Mo 4.75–5.75 Ti 2.2–2.5 Al 0.7–1.0 C 0.03–0.08 Si 0.5 max Cu 0.5 max Mn 0.2 max Co 1.0 max B 0.001 max Zr 0.02–0.05 S 0.015 max

Mechanical properties Typical 1,000-hour rupture strength, precipitation-hardened condition; Special Metals handbook, printed page 32. Product form and the exact heat-treatment cycle are not specified in this summary. Test temperature °C 1,000 h rupture strength MPa 650 340 705 250 760 140 The bulletin supplies tensile curves, not a numerical tensile table. The rupture data are typical characterization values; their test temperatures do not establish a recommended service-temperature limit.

Application areas Gas turbine components Welded high-strength sheet fabrications for turbine service

Alloy PE11/Nimonic PE11

Grade: Nimonic PE11/Alloy PE11/UNS N09901/W.Nr.2.4662

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 PE11 is a precipitation-hardenable nickel iron chromium alloy developed for strong, readily fabricated sheet structures. Titanium and aluminum provide age hardening, supported by molybdenum in the matrix. Its relatively high iron content assists working and weld ductility. Gas turbine fabrications are a principal use, where both the material condition and welded-joint properties require careful control.

Chemical composition

Element	Weight percent	Element	Weight percent
Ni	37–41	Fe	Balance
Cr	17–19	Mo	4.75–5.75
Ti	2.2–2.5	Al	0.7–1.0
C	0.03–0.08	Si	0.5 max
Cu	0.5 max	Mn	0.2 max
Co	1.0 max	B	0.001 max
Zr	0.02–0.05	S	0.015 max

Mechanical properties

Typical 1,000-hour rupture strength, precipitation-hardened condition; Special Metals handbook, printed page 32. Product form and the exact heat-treatment cycle are not specified in this summary.

Test temperature °C	1,000 h rupture strength MPa
650	340
705	250
760	140

The bulletin supplies tensile curves, not a numerical tensile table. The rupture data are typical characterization values; their test temperatures do not establish a recommended service-temperature limit.

Application areas

Gas turbine components
Welded high-strength sheet fabrications for turbine service

Introduction

Specification

Chemical composition

Element	Weight percent	Element	Weight percent
Ni	37–41	Fe	Balance
Cr	17–19	Mo	4.75–5.75
Ti	2.2–2.5	Al	0.7–1.0
C	0.03–0.08	Si	0.5 max
Cu	0.5 max	Mn	0.2 max
Co	1.0 max	B	0.001 max
Zr	0.02–0.05	S	0.015 max

Mechanical

Mechanical properties

Typical 1,000-hour rupture strength, precipitation-hardened condition; Special Metals handbook, printed page 32. Product form and the exact heat-treatment cycle are not specified in this summary.