Armstrong Siddeley Panther

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Armstrong Siddeley Panther on a Blackburn Ripon Mark IIf.

The Armstrong Siddeley Panther is an aircraft engine that the British manufacturer Armstrong Siddeley built from 1929. The two-row 14-cylinder radial engine has a displacement of 27,317 cm³. The panther was also called the Jaguar Major in the beginning .

Aircraft with Armstrong Siddeley Panthers

Data (Panther VII)

General

  • Two-row 14-cylinder radial engine, air-cooled, with compressor
  • Bore: 133.4 mm
  • Stroke: 139.7 mm
  • Displacement: 27,317 cm³
  • Length: 1626 mm
  • Diameter: 1180 mm
  • Weight: 475 kg

Components

  • Valve train: Two overhead valves per cylinder
  • Compressor: for all cylinders, direct drive
  • Mixture preparation: carburettor
  • Cooling: air
  • Reduction gear: no

power

  • Power: 638 bhp (478 kW) at 2400 rpm. and 3.5 kPa boost pressure
  • Output per liter: 17.50 kW / l
  • Compression: 5.1: 1
  • Power-to-weight ratio : 1.136 kg / kW

literature

  • Alec Lumsdem: British Piston Engines and their Aircraft . Airlife Publishing, Marlborough 2003. ISBN 1-85310-294-6 .

Web links

Commons : Armstrong Siddeley Panther  - Collection of images, videos and audio files

Individual evidence

  1. ^ A b c Alec Lumsden: British Piston Engines and their Aircraft . Airlife Publishing, Marlborough, Wiltshire 2003. ISBN 1-85310-294-6 . Pp. 72-73.