Pobjoy Niagara

From Infogalactic: the planetary knowledge core
(Redirected from Pobjoy Cataract)
Jump to: navigation, search
Niagara
300px
Pobjoy Niagara on display at the Science Museum, London
Type Piston radial aero engine
Manufacturer Pobjoy Airmotors
First run 1934

The Pobjoy Niagara is a British seven-cylinder, air-cooled, radial, aero-engine first produced in 1934. The design ran at higher speeds than conventional engines, and used reduction gearing to lower the speed of the propeller. This led to a noticeable off-centre mounting for the propeller. The Niagara was a popular engine for light and experimental aircraft,[1] well regarded due to its small diameter, smooth operation, low noise and innovative engineering.

Variants

Niagara I
Bore/stroke 77 x 87 mm (3.03 x 3.43 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.[2]
Niagara II
Bore/stroke 77 x 87 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.[2]
Niagara III
Bore/stroke 77 x 87 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.[2]
Niagara IV
Similar to Niagara III but with a higher operating rpm. Normal continuous power 98 hp (73 kW) at 3,500 rpm at sea level.[2]
Niagara V
Larger version of the basic Niagara. Bore/stroke 81 x 87 mm (3.19 x 3.43 in), swept volume 3,138 cc (191.5 cu in). Compression 8.0:1, gearing 0.47:1. Normal continuous power 125 hp (93 kW) at 4,000 rpm at sea level.[2][3]
Cataract I-III
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.[2][3][4]
Cascade
Direct drive version of Cataract I. Normal continuous power 66 hp (49 kW) at 2,100 rpm.[4]

Applications

File:Pobjoy Niagara.jpg
Airworthy Pobjoy Niagara installed in a Comper Swift at the Shuttleworth Collection

Niagara

Cataract

Cascade

Survivors

A Pobjoy Niagara 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-Hobson carburettor
  • Fuel type: 70 octane
  • Cooling system: Air-cooled

Performance

See also

Related development
Comparable engines
Related lists

References

Notes

  1. Gunston 1989, p.111.
  2. 2.0 2.1 2.2 2.3 2.4 2.5 2.6 Lumsden 2003, p.179.
  3. 3.0 3.1 Jane's All the World's Aircraft p.26d
  4. 4.0 4.1 Ord-Hume p.589
  5. Shuttleworth Collection - Comper Swift www.shuttleworth.org Retrieved: 27 April 2010

Bibliography

  • Lua error in package.lua at line 80: module 'strict' not found.
  • 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.
  • Lua error in package.lua at line 80: module 'strict' not found.

External links