The Jacobs R-915 or Jacobs L-6 is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States, production started in 1936.[1]
| R-915 | |
|---|---|
| Type | Radial engine |
| Manufacturer | Jacobs Aircraft Engine Company |
| Developed from | Jacobs R-755 |
The R-915 was effectively an enlargement of the R-755 with strengthened stressed parts.[2] With a bore and stroke of 5.5 in × 5.5 in (140 mm × 140 mm), for a displacement of 915 cu in (15 L). Take-off power was around 330 hp (250 kW). The engine features steel cylinders with aluminum-alloy cylinder heads.
Data from Jane's[5]
Related development
Comparable engines
Related lists
United States military piston aircraft engine designation system | |
|---|---|
| H (four-bank H-configuration inline) | |
| IV (inverted-V inline) | |
| L (single-bank inline) | |
| O (opposed) | |
| R (radial) |
|
| V (upright-V inline) | |
| V (inverted-V inline) | |
| VG (inverted-V inline) | |
| W (three-bank W-configuration inline) |
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