Pobjoy Niagara
The Pobjoy Niagara is a British seven-cylinder, air-cooled, radial, aero-engine first produced in 1934, with an unusual offset-from-centre propshaft due to its engine reduction gearing.[1] The Niagara was a popular engine for light and experimental aircraft. The entire series of Pobjoy motors were seven-cylinder radials with compact dimensions and very high rpm. The entire Pobjoy range was well regarded due to its small diameter, smooth operation, low noise and innovative engineering.
Variants
- Niagara I[2]
- Bore/stroke 77x87 mm (3.03x3.43 in), swept volume 2,835 cc (173 cu in). Compression 6.25:1, gearing 0.47:1. Normal continuous power 84 hp (63 kW) at 3,200 rpm at sea level.
- Niagara II[2]
- Bore/stroke 77x87 mm (3.03x3.43 in), swept volume 2,835 cc (173 cu in). Compression 6.0:1, gearing 0.39:1. Normal continuous power 84 hp (63 kW) at 3,200 rpm at sea level.
- Niagara III[2]
- Bore/stroke 77x87 mm (3.03x3.43 in), swept volume 2,835 cc (173 cu in). Gearing 0.47:1. Normal continuous power 88 hp (66 kW) at 3,300 rpm at sea level.
- Niagara IV[2]
- Similar to Niagara III. Normal continuous power 98 hp (73 kW) at 3,500 rpm at sea level.
- Niagara V[2][3]
- Bore/stroke 81x87 mm (3.19x3.43 in), swept volume 3,138 cc (192.5 cu in). Compression 8.0:1, gearing 0.47:1. Normal continuous power 125 hp (93 kW) at 4,000 rpm at sea level.
- Cataract I-III[2][3][4]
- De-rated, uncowled versions of Niagara I-III with simple inter-cylinder baffles for cooling and trickle-down lubrication for lower exhaust rockers. Compression 5.7:1, gearing 0.47:1.
- Cascade[4]
- Direct drive version of Cataract I. Normal continuous power 66 hp (49 kW) at 2,100 rpm.
Applications
Niagara
Cataract
Cascade
Survivors
A Pobjoy Niagra powered Comper Swift that is owned and operated by the Shuttleworth Collection remains airworthy in 2010.[5]
Engines on display
A preserved Pobjoy Niagara engine is on public display at the Science Museum (London).
Specifications (Pobjoy Niagara IV)
Data from Lumsden[2]
General characteristics
- Type: 7-cylinder, air-cooled, radial engine
- Bore: 3.03 in (77 mm)
- Stroke: 3.43 in (87 mm)
- Displacement: 173 cu in (2.8 L)
- Diameter: 26.5 in (673 mm)
- Dry weight: 130 lb (59 kg)
Components
- Valvetrain: 1 inlet and 1 exhaust valve per cylinder
- Fuel system: 1 Claudel carburettor
- Fuel type: 70 octane
- Cooling system: Air-cooled
Performance
See also
- Related development
- Related lists
References
Notes
Bibliography
- Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. ISBN 0715 35734 4.
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
- Ord-Hume, Arthur W.J.G. (2000). British Light Aeroplanes. Peterborough: GMS Enterprises. ISBN 1 870384 76 8 5.
External links
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