Wright Vertical 4
From Infogalactic: the planetary knowledge core
| Wright Vertical 4 | |
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| Wright Vertical 4 aircraft engine on display at the Steven F. Udvar-Hazy Center. This particular engine was used on the Wright B-1 seaplane that crashed in 1912. A patch was bolted to the side of the crankcase in an attempt to repair the engine. | |
| Type | Piston aero engine |
| National origin | United States |
| Manufacturer | Wright Company |
| Designed by | Orville Wright |
The Wright Vertical 4 engine was an early aircraft piston engine with four inline cylinders.
Among other aircraft the Vertical 4 powered the U.S. Navy's first Wright aircraft, the B-1 "hydroaeroplane".
Contents
Specifications
General characteristics
- Type: 4-cylinder, liquid-cooled inline piston aircraft engine
- Displacement: 240 cubic inches (3.9 L)
- Length: 25 inches (635 mm)
- Width: 14 inches (356 mm)
- Height: 35 inches (890 mm)
- Dry weight: 180 pounds (81.6 kg)
Components
- Cooling system: liquid-cooled
Performance
- Power output: 36 horsepower (27 kW) at 1600 rpm
Notes
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- This article contains material that originally came from the placard at the Steven F. Udvar-Hazy Center.
External links
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