- Source: 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.
Applications
Aichi E10A
Aichi E11A
Hiro H4H
Kawanishi E7K
Mitsubishi Ka-9
Specifications (Type 91 500hp-1)
= 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
See also
Related lists
List of aircraft engines
References
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.
Kata Kunci Pencarian:
- Kawanishi E7K
- Exile (grup musik)
- Staind
- Hiro Type 91
- Type 91
- Hiro H4H
- Hiro Type 94
- Hiro Type 14
- Mitsubishi G3M
- Kawanishi E7K
- Kugisho B3Y
- Hiro Naval Arsenal
- Hiroo Onoda
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