Napier Lion

The Napier Lion was a 12-cylinder 'broad arrow' W12 configuration aircraft engine built by D. Napier & Son from 1917 until the 1930s. A number of advanced features made it the most powerful engine of its day and kept it in production long after other contemporary designs had been superseded. It is particularly well known for its use in a number of racing designs, for aircraft, boats and cars.

Lion
Napier Lion II at Canada Aviation Museum
Type Piston aero-engine
Manufacturer D. Napier & Son
First run 1917
Major applications Handley Page Hyderabad
Vickers Vernon

Design and development

Early in the First World War, Napier were contracted to build aero engines to designs from other companies, initially a Royal Aircraft Factory model and then Sunbeams. Both engines proved to be unreliable and in 1916 Napier decided to design an engine with high power, light weight and low frontal area. Napier's engineers laid out the engine with its 12 cylinders in what they called a "broad arrow"—three banks of four cylinders sharing a common crankcase. This suggested the design's first name, the Triple-Four. The configuration is also known as a W engine.[1] The engine was also advanced in form, the heads using four valves per cylinder with twin overhead camshafts on each bank of cylinders and a single block being milled from aluminium instead of the common separate-cylinder steel construction used on almost all other designs.

Under Arthur Rowledge, the design of the engine, renamed Lion, was completed in 1917; hand-built prototypes ran later that year. It was fitted to an Airco DH.9 in early 1918, and many cooling problems were observed during testing. The milled block was difficult to build with the required accuracy and the design reverted to separate aluminium cylinders. Both problems were solved by the middle of the year and the engine entered production in June 1918. The first Lion I versions delivered 450 horsepower (340 kW) from their 24 litres. The power output made the Lion the most powerful Allied aircraft engine, which had previously been the Liberty L-12, producing 400 horsepower (300 kW).

As the most powerful engine available (particularly after a turbocharger became an option in 1922), the Lion went on to commercial success. Through the years between the wars the Lion was ubiquitous and Napier manufactured little else. They stopped making cars in 1925 and little thought was given to replacing their world-famous product. Between the wars the Lion engine powered over 160 different aircraft types.

In highly tuned racing versions, the engine could reach 1,300 hp (970 kW) and it was used to break many world height, air speed and distance records in aircraft and boats, delivering 1,375 hp (1,025 kW) in a highly tuned Lion for a water speed record of 100 mph (160 km/h) in 1933. In land speed records, Lion engines powered many of Sir Malcolm Campbell's record breakers including a record of over 250 mph (400 km/h) in 1932 and John Cobb's 394 mph (634 km/h) Railton Mobil Special in 1947—a record that came well after the Lion had passed its prime and stood until the 1960s. The record had been held by British drivers for 32 years. Lions powered successful entrants in the most prestigious event in air racing, the Schneider Trophy, in 1922 and 1927 but were dropped by Supermarine in favour of a new engine, the Rolls-Royce R, which had been designed for racing.

During the 1930s a new generation of much larger and more powerful engines appeared and the Lion became uncompetitive. By the time the Bristol Hercules and the Rolls-Royce Merlin arrived in the late 1930s, the Lion was obsolete. The Sea Lion, a marine version of the Lion, was used to power high speed RAF Rescue Launches. The Lion aero engine was also adapted to power propeller-driven motor sleighs, which were used for high-speed transport and SAR duties on sea ice by the Finnish Air Force and Navy.

Turning away from the broad arrow layout, Napier designed new engines using the more compact H engine layout. The 16-cylinder Napier Rapier produced 400 hp (300 kW) and the 24-cylinder Napier Dagger delivered just under 1,000 hp (750 kW). The engines were smaller than contemporary designs from other companies and Napier started afresh with a new sleeve valve design, which evolved into the Napier Sabre.

Variants

Lion models[2][3]
ModelDateWorks No.PowerNotesNotable uses
I1918450 bhp (340 kW) at 1,950 rpmgeared, also related IA and 1AY
II1919E64450 bhp (340 kW) at 2,000 rpm
IIII experimental geared Gloster Gorcock
V470 bhp (350 kW) at 2,000 rpm
500 bhp (370 kW) at 2,250 rpm
VA had increased CR to 5.8Mainstay engine of the RAF in the late 1920s, replaced by Lion XI
VSE79Turbocharged, intercooled
VIS1927TurbochargedGloster Guan
VII1925700 bhp (520 kW) (racing)Gloster III (Schneider Trophy entrant)
Supermarine S.4
VIIA1927E86900 bhp (670 kW) (racing)Golden Arrow
Blue Bird (1927)
Miss England I
Supermarine S.5
Gloster IV
VIIB1927875 bhp (652 kW) (racing)gearedSupermarine S.5
Gloster IV
VIID1929E911,350 bhp (1,010 kW) at 3,600 rpm (racing)Supercharged, about 6–8 builtBlue Bird (1931)
Fred H Stewarts Enterprise
Betty Carstairss Estelle V powerboat
Miss Britain III
Gloster VI (Schneider Trophy entrant)
Railton Special (John Cobb's land speed record car)
VIII1927direct driveGloster Gorcock
XIA1928580 bhp (430 kW) at 2,585 rpm, 6:1 CRRAF production modelNapier-Railton
LionessE71Inverted layout, for better visibility. At least some were built turbocharged, for racing.
Sea Lion1933500 and 600 bhp (370 and 450 kW)Marine version of Lion XIBritish Power Boat Company Type Two 63 ft HSL

Applications

Aircraft

Other applications

Engines on display

Preserved Napier Lion engines are on static display at

Specifications (Lion II)

Data from Lumsden[7]

General characteristics

  • Type: 12-cylinder water-cooled W-block (3 banks of 4 cylinders) aircraft piston engine
  • Bore: 5.5 in (139.7 mm)
  • Stroke: 5.125 in (130.17 mm)
  • Displacement: 1,461.6 in³ (23.944 L)
  • Length: 57.5 in (1460 mm)
  • Width: 42.0 in (1067 mm)
  • Height: 43.5 in (1105 mm)
  • Dry weight: 960 lb (435 kg)

Components

  • Valvetrain: Two intake and two exhaust valves per cylinder actuated via double overhead camshafts per cylinder block.
  • Cooling system: Water-cooled

Performance

See also

Comparable engines

Related lists

References

Notes

  1. Domonoske, Arthur Boquer; Finch, Volney Cecil (1936). Aircraft Engines: Theory, Analysis, Design and Operation (Engineering textbook). J. Wiley & Sons. p. 7. The W, or broad arrow engine, has three rows of cylinders of which the central row is vertical with the other two rows forming equal angles with the vertical.
  2. Vessey 1997
  3. "Napier Aero-Engines". Flight. 73 (2579): 893. 27 June 1958.
  4. Ransom and Fairclough, S and R (1987). "English Electric Aircraft and their Predecessors". Their Fighting Machines. Putnam. Retrieved 7 January 2017.
  5. 2nd MTB Flotilla.pdf
  6. "Miss Britain III – National Maritime Museum". Collections.rmg.co.uk. Retrieved 6 March 2013.
  7. Lumsden 2003, p.166.

Bibliography

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
  • Vessey, Alan. Napier Powered. Stroud: Tempus (Images of England series), 1997. ISBN 0-7524-0766-X.
  • "The Napier Lion Aeromotor". Flight. XI (13): 397–402. 27 March 1919. No. 535. Retrieved 12 January 2011. Contemporary technical description of the Lion with photographs and drawings.
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