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
- Fast Shipping / Ready Stock
- ISO 9001 Factory
- Custom Cutting
- 100% MTC & SGS Inspection
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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