 | This is not a Wikipedia article: It is an individual user's work-in-progress page, and may be incomplete and/or unreliable. For guidance on developing this draft, see Wikipedia:So you made a userspace draft. Find sources: Google (books · news · scholar · free images · WP refs) · FENS · JSTOR · TWL |
The Hiro Type 90 was a twelve cylinder W-type engine with a bore of 135 mm. and a stroke of 160 mm. for a capacity of 27.5 litres. It appeared first in 1931 under the designation of Type 91, and had a rated power of 600 h.p. and a maximum power output of 750 h.p. The engine was installed in flying boats, sea reconnaissance aircraft with a crew of three, and in shipborne bombers.
Since in the course of further development sufficiently powered radial engines were produced, the production of liquid cooled in-line types gradually subsided in favor of the twin-row air-cooled radial.
| Hiro Type 90 | |
|---|---|
| Type | W-type liquid cooled aircraft engine |
| National origin | Japan |
| Manufacturer | Hiro Naval Arsenal |
| First run | 1931 |
Specifications (Hiro Type 90)
editData from Flight
General characteristics
- Bore: 135mm
- Stroke: 160mm
- Displacement: 27.5l
Components
- Cooling system: Liquid
Performance
- Power output: 600 to 750hp
References
editFLIGHT July 16, 1942 page 72
[[:Category:]]