GO-480 | |
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Lycoming GO-480-B1 on display at the Deutsches Museum Flugwerft Schleissheim | |
Type | Piston aero-engine |
National origin | United States |
Manufacturer | Lycoming Engines |
First run | 1953 |
Major applications | Dornier Do 27 Helio Courier Utva 66 |
Produced | 1954–1986 out of production |
Developed from | Lycoming O-320 |
The Lycoming GO-480 is a family of six-cylinder, horizontally opposed fixed-wing aircraft engines of 479.6 cubic inch (7.86 L) displacement, made by Lycoming Engines. The engine is a six-cylinder version of the four-cylinder Lycoming O-320.
Design and development
GO-480 series engines are installed on a number of different aircraft types. Their main competitive engines are the Continental IO-520 and IO-550 series.
Variants
All engines have an additional prefix preceding the 480 to indicate the specific configuration of the engine. Although the series is known as the "O-480", there are only geared engines in the series. There are also numerous engine suffixes, denoting different accessories such as different manufacturers' carburetors, or different magnetos.
- GO-480
- Normally aspirated Opposed engine, equipped with a carburetor and Gearbox at the front end of the crankshaft to drive the propeller at a lower RPM than the engine.
- GSO-480
- Supercharger driven by the engine, gearbox to drive propeller, and equipped with a carburetor. Designated the O-480-1 by the US military.
- IGSO-480
- Supercharger driven by the engine, gearbox to drive propeller, with fuel Injection. Designated the O-480-3 by the US military.
- IGO-480
- Gearbox to drive propeller, normally aspirated with fuel injection.
Applications
- Aero Commander 560, 560A, 560E and 680, 680E and the pressurized 720 Alti-Cruiser.
- Aermacchi AM3CM (Bosbok)
- Beechcraft Twin Bonanza
- Beechcraft Queen Air
- Dornier Do 27
- Helio Courier
- Pilatus PC-6 Porter
- Soko J-20 Kraguj
- Temco 58
- Utva 66
Specifications (GSO-480-A1A6)
Data from FAA Type Certificate.
General characteristics
- Type: Six-cylinder air-cooled geared supercharged horizontally opposed engine
- Bore: 5.125 in (130 mm)
- Stroke: 3.875 in (98 mm)
- Displacement: 479.6 in (7.86 L)
- Dry weight: 498 lb dry (226 kg)
Components
- Valvetrain: Two overhead valves per cylinder
- Supercharger: 11.27:1 ratio, providing 48" Hg (1.6 atm / 8.8 psi) manifold pressure at sea level at maximum power
- Fuel type: 100 octane rating gasoline
- Cooling system: Air-cooled
- Reduction gear: 77:120 (.642:1)
Performance
- Power output: 340 hp at 3,400 rpm at sea level
- Compression ratio: 7.3:1
See also
Comparable engines
Related lists
References
- ^ Page listing all variants of the Lycoming O-480 series. Retrieved on 10 January 2009.
- FAA GO-480 Series Type Certificate. Retrieved on 10 January 2009.
- ^ FAA Lycoming GSO-480 Series Type Certificate. Retrieved on 10 January 2009.
Lycoming aircraft engines | |
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Opposed piston engines | |
Radial engines and H engines | |
Aircraft diesel engines | |
Turbofans | |
Turboprops/Turboshafts | |
Aero-derivative marine gas turbines | |
Joint development | Avco (Lycoming)/Pratt & Whitney: T800-APW (Turboshaft) |
See also |