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ADC Nimbus 
Summary
The ADC Nimbus was a British inline aero engine that first ran in 1926. The Nimbus was developed from the Siddeley Puma aero engine by Frank Halford of the Aircraft Disposal Company, the goal was to develop the Puma to produce its intended power output which Halford eventually achieved. The Nimbus was further developed into an air-cooled version known as the ADC Airsix which did not enter production and was not flown.[1]
| Nimbus | |
|---|---|
| Type | Liquid-cooled inline piston engine |
| National origin | United Kingdom |
| Manufacturer | Aircraft Disposal Company |
| First run | 1926 |
| Major applications | Airco DH.9 Vickers Vendace |
| Developed from | Siddeley Puma |
Applications edit
Specifications (Nimbus) edit
Data from Lumsden [2]
General characteristics
- Type: Six-cylinder, inline, liquid-cooled, upright piston engine
- Bore: 6.0 in (152 mm)
- Stroke: 7.5 in (190 mm)
- Displacement: 1,150.3 cu in (18.85 L)
- Length: 70 in (1,778 mm)
- Width: 17.5 in (444 mm)
- Height: 44 in (1,118 mm)
- Dry weight: 670 lb (304 kg)
- Designer: Frank Halford
Components
- Valvetrain: 1 inlet and 2 exhaust valve per cylinder
- Fuel system: Carburettor
- Fuel type: 74 octane
- Cooling system: Air-cooled
- Reduction gear: Direct drive, right hand tractor
Performance
- Power output: 305 hp (227 kW) at 1,450 rpm (takeoff power)
- Specific power: 0.26 hp/cu in (12 kW/L)
- Compression ratio: 5.4:1
- Power-to-weight ratio: 0.46 hp/lb (0.9 kW/kg)
See also edit
Related development
Comparable engines
Related lists
References edit
Notes edit
Bibliography edit
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links edit
- Nimbus Martinsyde, Flight, July 1928