Supriya Ghosh (Editor)

Hiro Type 91

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The Hiro Type 91, (full designation Hiro Type 91 520 hp water-cooled W-12), was a 12-cylinder, water-cooled, W engine developed for aircraft use by the Imperial Japanese Navy in the mid-1930s. Power was in the 450 kW (600 hp) range. Its design was inspired by the Lorraine-Dietrich 12Eb Courlis. An enlarged more powerful engine, the Hiro Type 90 had also been developed, producing 600 hp.

Contents

Applications

  • Aichi E10A
  • Aichi E11A
  • Hiro H4H
  • Kawanishi E7K
  • Mitsubishi Ka-9
  • General characteristics

  • Type: 12-cylinder water-cooled W-block (3 banks of 4 cylinders) aircraft piston engine
  • Bore: 135 mm
  • Stroke: 160 mm
  • Displacement: 27.5 L
  • Components

  • Cooling system: Liquid-cooled
  • Performance

  • Power output:
  • 620 PS for takeoff
  • 520 hp for max continuous
  • References

    Hiro Type 91 Wikipedia