Hiro Type 94 (Engine)
| Type 94 900hp liquid-cooled in-line |
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| 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
- Hiro G2H land-based bomber
Specifications (variant)
Data from Mikesh
General characteristics
- Type: 40° W-18 liquid-cooled piston engine
- Bore: 135mm
- Stroke: 160mm
- Displacement: 41.25l
Components
Performance
- Power output: 900–1,180 hp (670–880 kW)
References
- Mikesh, Robert C. and Abe, Shorzoe. Japanese Aircraft 1910-1941. London:Putnam, 1990. ISBN 0 85177 840 2
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| | Aircraft designed and produced by Hiro | |
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| | Prototypes and experimental aircraft | |
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| | Aircraft designed by others produced at Hiro | |
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| | Engines designed and produced by Hiro | |
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| | Aichi | |
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| | Hiro Naval Arsenal | |
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| | Mitsubishi | |
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| | Nakajima | |
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| | Tokyo Gasu Denki | |
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