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Hiro Type 91

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 derived from the Napier Lion. An enlarged more powerful engine, the Hiro Type 90 600 hp water-cooled W-12 had also been developed, producing 600 hp.

Type 91
Type W-12 water-cooled piston engine
National origin Japan
Manufacturer Hiro Naval Arsenal
Developed from 12Eb

Applications edit

Specifications (Type 91 500hp-1) edit

General characteristics

Components

  • Cooling system: Liquid-cooled

Performance

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

See also edit

Related lists

References edit

  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 74.
  • Goodwin, Mike & Starkings, Peter (2017). Japanese Aero-Engines 1910-1945. Sandomierz, Poland: MMPBooks. ISBN 978-83-65281-32-6.

hiro, type, this, article, about, engine, flying, boat, hiro, full, designation, water, cooled, cylinder, water, cooled, engine, developed, aircraft, imperial, japanese, navy, 1930s, power, range, design, derived, from, napier, lion, enlarged, more, powerful, . This article is about the engine For the Hiro Type 91 flying boat see Hiro H4H 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 derived from the Napier Lion An enlarged more powerful engine the Hiro Type 90 600 hp water cooled W 12 had also been developed producing 600 hp Type 91 Type W 12 water cooled piston engine National origin Japan Manufacturer Hiro Naval Arsenal Developed from 12Eb Contents 1 Applications 2 Specifications Type 91 500hp 1 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 ReferencesApplications editAichi E10A Aichi E11A Hiro H4H Kawanishi E7K Mitsubishi Ka 9Specifications Type 91 500hp 1 editGeneral 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 continuousSee also editRelated lists List of aircraft enginesReferences editGunston Bill 1986 World Encyclopedia of Aero Engines Wellingborough Patrick Stephens p 74 Goodwin Mike amp Starkings Peter 2017 Japanese Aero Engines 1910 1945 Sandomierz Poland MMPBooks ISBN 978 83 65281 32 6 Retrieved from https en wikipedia org w index php title Hiro Type 91 amp oldid 1057769824, wikipedia, wiki, book, books, library,

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