Alloy 91/UNS N07091

Grade: Nimonic 91/UNS N07091

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 91 is described by HB Special Alloy as a wrought nickel chromium cobalt alloy related to NIMONIC 90, with higher chromium for improved resistance to salt and sulfur contamination. Aluminium and titanium provide strengthening. It is intended for stressed turbine components in aggressive hot-corrosion environments. Public manufacturer documentation is limited, so chemical limits, heat treatment, mechanical acceptance values and designation should be confirmed for each purchase.

Chemical composition

Element Weight percent Element Weight percent
Ni Balance Cr 27.0–30.0
Co 19.0–21.0 Nb 0.4–1.1
Al 0.9–1.5 Ti 1.9–2.7
C 0.10 max Si 1.00 max
Mn 1.00 max P 0.020 max
S 0.015 max Cu 0.50 max
Fe 1.00 max — —

Mechanical properties

HB Special Alloy lists these as typical room-temperature, annealed properties. Product form, annealing cycle, proof-stress offset and elongation gauge length are not stated; values remain unverified screening data.

Test condition Yield strength MPa Tensile MPa Elongation %
RT, supplier reports annealed 680 1190 30

No independently verified elevated-temperature tensile or creep table was found in the cited sources. The supplied values must not be interpreted as certified minima.

Application areas

  • Gas turbine blades exposed to impure fuels
  • Stressed turbine parts operating in marine environments
  • High-temperature parts requiring resistance to salt and sulfur related hot corrosion

NIMONIC 91 is described by HB Special Alloy as a wrought nickel chromium cobalt alloy related to NIMONIC 90, with higher chromium for improved resistance to salt and sulfur contamination. Aluminium and titanium provide strengthening. It is intended for stressed turbine components in aggressive hot-corrosion environments. Public manufacturer documentation is limited, so chemical limits, heat treatment, mechanical acceptance values and designation should be confirmed for each purchase.

Chemical composition

Element Weight percent Element Weight percent
Ni Balance Cr 27.0–30.0
Co 19.0–21.0 Nb 0.4–1.1
Al 0.9–1.5 Ti 1.9–2.7
C 0.10 max Si 1.00 max
Mn 1.00 max P 0.020 max
S 0.015 max Cu 0.50 max
Fe 1.00 max — —

Mechanical properties

HB Special Alloy lists these as typical room-temperature, annealed properties. Product form, annealing cycle, proof-stress offset and elongation gauge length are not stated; values remain unverified screening data.

Test condition Yield strength MPa Tensile MPa Elongation %
RT, supplier reports annealed 680 1190 30

No independently verified elevated-temperature tensile or creep table was found in the cited sources. The supplied values must not be interpreted as certified minima.

Application areas

  • Gas turbine blades exposed to impure fuels
  • Stressed turbine parts operating in marine environments
  • High-temperature parts requiring resistance to salt and sulfur related hot corrosion
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