Hiro Type 94
(Redirected from Hiro Type 94 (Engine))
| Type 94 900hp liquid-cooled in-line | |
|---|---|
| Type | "W"-18 cylinder liquid-cooled aircraft engine |
| National origin | Japan |
| Manufacturer | Yokosuka Naval Air Arsenal |
| First run | 1933 |
| Developed from | Hiro Type 91 |
The Type 94 900 hp liquid-cooled in-line was a W-18 liquid-cooled aircraft engine. Two Type 94 engines were used to power the Imperial Japanese Navy Hiro G2H land-based bomber in 1933. The Type 94 engine was the eighteen-cylinder version of the Hiro Type 90 600 hp water-cooled W-12/Hiro Type 91 520 hp water-cooled W-12 engines.
Applications
[edit]- Hiro G2H land-based bomber
Specifications (variant)
[edit]Data from Mikesh
General characteristics
- Type: 40° W-18 liquid-cooled piston engine
- Bore: 135mm (5.315 in.)
- Stroke: 160mm (6.2992 in.)
- Displacement: 41.25l (2,515.6 ci)
Components
- Cooling system: Liquid
Performance
- Power output: 900–1,180 hp (670–880 kW)
References
[edit]Bibliography
[edit]- Mikesh, Robert C. and Abe, Shorzoe. Japanese Aircraft 1910-1941. London:Putnam, 1990. ISBN 0 85177 840 2
- Goodwin, Mike & Starkings, Peter (2017). Japanese Aero-Engines 1910-1945. Sandomierz, Poland: MMPBooks. ISBN 978-83-65281-32-6.
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