User:Gorkypickeral/sandbox 5
| Titan X-340 | |
|---|---|
| |
| Titan X-340 engine on stand | |
| Type | Horizontally opposed piston engine |
| National origin | USA |
| Manufacturer | Continental Motors Corporation |
| Major applications | Van's Aircraft |
The Titan X-340 is an experimental four-cylinder, direct drive, horizontally opposed, air-cooled, piston aircraft engine.
Design and development[edit]
Variants[edit]
X-340 series[edit]
Applications[edit]
Specifications (X-340)[edit]
Data from [1]
General characteristics
- Type: Four-cylinder air-cooled horizontally opposed engine
- Bore: 5.125 in (130.18 mm)
- Stroke: 4.125 in (104.78 mm)
- Displacement: 340 cu in (5.57 L)
- Length: 29.07 in
- Width: 32.27 in
- Height: 20.36 - 23 in
- Dry weight: 259–296 lb (117–134 kg)
Components
- Valvetrain: Two overhead valves per cylinder
- Fuel system: Updraft carburetor
- Fuel type: minimum grade of 100LL avgas
- Oil system: Wet sump
- Cooling system: Air-cooled
Performance
- Power output: 174–180 hp (130–134 kW)
- Compression ratio: 8:1 - 9:1
- Power-to-weight ratio: 0.69
See also[edit]
References[edit]
Notes[edit]
Bibliography[edit]
External links[edit]
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