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Data Sheet:

NICKEL SUPERALLOY  PE11

Chemical Composition Limits

Weight % Ni Cr Mo Fe Al Ti C
PE11 37.0 / 41.0 17.0 / 19.0 4.75 / 5.75 Remainder 0.70 / 1.0 2.2 / 2.5 0.03 / 0.08 
Weight % Cu Si Mn Co B Zr S
PE11 0.5 max 0.5 max 0.2 max 1.0 max 0.001 max 0.02 / 0.05 0.015 max

 

Alloy PE11 (UNS N09901) main elements are nickel, iron and chromium, but the additions of Aluminium, Titanium and Molybdenum makes the PE11 both precipitation hardened and solid-solution strengthened. PE11 is commonly used in gas turbines because of its high tensile ductility strength and as it was developed for use at 550°C (1020°F).

 

AVAILABILITY

PE11 is available in Sheet, Plate, Round Bar, Flat Bar, Forging Stock, Wire and Welding Wire.  For all stock availability contact Sales.

 

SPECIFICATIONS

DTD 5037

AFNOR Z8 NC D38

MSRR 7182 and MSRR 7181

Trade Mark - NIMONIC PE11

 

TYPICAL MECHANICAL PROPERTIES (PRECIPITATION HARDENED)

PE11 Rupture Strength (1000 h)

Temperature

psi

MPa

650°C / 1200°F  49,000 340
705°C / 1300°F  36,000 250
760°C / 1400°F 21,000 140

  

Disclaimer

Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.

  

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