Rolls-Royce aircraft piston engines

Last updated

A preserved Rolls-Royce Griffon 58, one of the last Rolls-Royce piston engines to be produced. The red and white "dumb bell" object to the left of the engine is an air raid siren exhibit Griffon58.JPG
A preserved Rolls-Royce Griffon 58, one of the last Rolls-Royce piston engines to be produced. The red and white "dumb bell" object to the left of the engine is an air raid siren exhibit

Rolls-Royce produced a range of piston engine types for aircraft use in the first half of the 20th century. Production of own-design engines ceased in 1955 with the last versions of the Griffon; licensed production of Teledyne Continental Motors general aviation engines was carried out by the company in the 1960s and 1970s.

Contents

Examples of Rolls-Royce aircraft piston engine types remain airworthy today with many more on public display in museums.

WWI

In 1915, the Eagle, Falcon, and Hawk engines were developed in response to wartime needs. The Eagle was very successful, especially for bombers. It was scaled down by a factor of 5:4 to make the Falcon or by deleting one bank of its V12 cylinders to make the Hawk. The smaller engines were intended for fighter aircraft. Subsequently, it was enlarged to make the Condor which saw use in airships. [1]

Inter-war years

The Rolls-Royce Kestrel RRKestrel.JPG
The Rolls-Royce Kestrel

The Kestrel was a post-war redesign of the Eagle featuring wet cylinder liners in (two) common cylinder blocks. It was developed into the supercharged Peregrine and later the Goshawk. [2]

Developed concurrently with the Kestrel was the unusual Rolls-Royce Eagle XVI X engine that was cancelled in favour of the Kestrel despite performing well on the test stand.

The Buzzard was an enlargement of the Kestrel [3] of Condor size, developed in its most extreme form into the Rolls-Royce R racing engine used for the Schneider Trophy competition. [4]

The Vulture of 1939 was essentially two Peregrines on a common crankshaft in an X-24 configuration, both of these types being deemed unsuccessful. [5]

WWII and beyond

The Rolls-Royce Merlin, and later the development of the Buzzard, the Rolls-Royce Griffon were the two most successful designs for Rolls-Royce to serve in the Second World War, the Merlin powering RAF fighters the Hawker Hurricane, Supermarine Spitfire, fighter/bomber de Havilland Mosquito, Lancaster and Halifax heavy bombers and also allied aircraft such as the American P-51 Mustang and some marks of Kittyhawk.

Experimental engines were developed as alternatives for high performance aircraft such as the H-24 configuration Rolls-Royce Eagle 22, [6] the two-stroke Rolls-Royce Crecy [7] and the Rolls-Royce Pennine [8] and Rolls-Royce Exe, the Exe being the only one of these last three engines to fly. [9] However the successful development of the Merlin and Griffon, and the introduction of jet engines precluded significant production of these types.

Production of Rolls-Royce designed aircraft piston engines ceased in 1955 with the last variants of the Griffon. [10] Between 1961 and 1981 Rolls-Royce was licensed to build the Teledyne Continental range of light aircraft piston engines including the Continental O-520. [11]

Surviving engines

As of 2017 examples of the Falcon, Griffon, Kestrel and Merlin remain airworthy. [12]

Engines on display

Various types of Rolls-Royce aircraft piston engines are on public display at the following museums:

Chronological list

[13]

1915 Rolls-Royce Eagle V-12 Rolls-Royce Eagle VIII.jpg
1915 Rolls-Royce Eagle V-12
The Rolls-Royce Merlin RollsRoyce Merlin 23.jpg
The Rolls-Royce Merlin

See also

Related lists

Related Research Articles

<span class="mw-page-title-main">Rolls-Royce Merlin</span> Aircraft engine family by Rolls-Royce

The Rolls-Royce Merlin is a British liquid-cooled V-12 piston aero engine of 27-litre capacity. Rolls-Royce designed the engine and first ran it in 1933 as a private venture. Initially known as the PV-12, it was later called Merlin following the company convention of naming its four-stroke piston aero engines after birds of prey. The engine benefitted from the racing experiences of precursor engines in the 1930s.

<span class="mw-page-title-main">Rolls-Royce Vulture</span> 1930s British piston aircraft engine

The Rolls-Royce Vulture was a British aero engine developed shortly before World War II that was designed and built by Rolls-Royce Limited. The Vulture used the unusual "X-24" configuration, whereby four cylinder blocks derived from the Rolls-Royce Peregrine were joined by a common crankshaft supported by a single crankcase. The engine was originally designed to produce around 1,750 horsepower (1,300 kW) but problems with the Vulture design meant that the engines were derated to around 1,450 to 1,550 hp in service by limiting the maximum rpm.

<span class="mw-page-title-main">Rolls-Royce Griffon</span> 1930s British piston aircraft engine

The Rolls-Royce Griffon is a British 37-litre capacity, 60-degree V-12, liquid-cooled aero engine designed and built by Rolls-Royce Limited. In keeping with company convention, the Griffon was named after a bird of prey, in this case the griffon vulture.

<span class="mw-page-title-main">Rolls-Royce Peregrine</span> 1930s British aircraft piston engine

The Rolls-Royce Peregrine was a 21-litre (1,300 cu in), 885-horsepower (660 kW) liquid-cooled V-12 aero engine designed and built by the British manufacturer Rolls-Royce in the late 1930s. It was essentially the ultimate development of the company's Kestrel engine, which had seen widespread use in military aircraft of the pre-war period.

<span class="mw-page-title-main">Rolls-Royce Kestrel</span>

The Rolls-Royce Kestrel is a 21.25 litre V-12 aircraft engine from Rolls-Royce. It was their first cast-block engine, and used as the pattern for most of their future piston-engine designs. Used during the interwar period, it was fitted to a number of British fighters and bombers of the era, including the Hawker Fury and Hawker Hart family, and the Handley Page Heyford. The Kestrel engine was also sold to international air force customers; in this role it was used to power prototypes of the German Messerschmitt Bf 109 and the Junkers Ju 87 "Stuka" dive-bomber, as the Junkers Jumo 210 engines were not ready to be fitted. Several examples of the Kestrel engine remain airworthy today.

<span class="mw-page-title-main">Rolls-Royce Buzzard</span> 1920s British piston aircraft engine

The Rolls-Royce Buzzard is a British piston aero engine of 36.7 litres capacity that produced about 800 horsepower (600 kW). Designed and built by Rolls-Royce Limited it is a V12 engine of 6 in (150 mm) bore and 6.6 in (170 mm) stroke. Only 100 were made. A further development was the Rolls-Royce R engine. The Buzzard was developed by scaling-up the Rolls-Royce Kestrel Engine.

<span class="mw-page-title-main">Rolls-Royce R</span> 1929 British aero engine

The Rolls-Royce R is a British aero engine that was designed and built specifically for air racing purposes by Rolls-Royce Limited. Nineteen R engines were assembled in a limited production run between 1929 and 1931. Developed from the Rolls-Royce Buzzard, it was a 37-litre capacity, supercharged V-12 capable of producing just under 2,800 horsepower (2,090 kW), and weighed 1,640 pounds (770 kg). Intensive factory testing revealed mechanical failures which were remedied by redesigning the components, greatly improving reliability.

<span class="mw-page-title-main">Rolls-Royce Eagle</span> 12-cylinder vee liquid cooled aircraft engine

The Rolls-Royce Eagle was the first aircraft engine to be developed by Rolls-Royce Limited. Introduced in 1915 to meet British military requirements during World War I, it was used to power the Handley Page Type O bombers and a number of other military aircraft.

<span class="mw-page-title-main">Rolls-Royce Eagle (1944)</span>

The Rolls-Royce Eagle Mk XXII is a British 24-cylinder, sleeve valve, H-block aero engine of 46 litre displacement. It was designed and built in the early-1940s by Rolls-Royce Limited and first ran in 1944. It was liquid-cooled, of flat H configuration with two crankshafts and was capable of 3,200 horsepower at 18 psi boost.

<span class="mw-page-title-main">Rolls-Royce Crecy</span> 1940s British piston aircraft engine

The Rolls-Royce Crecy was a British experimental two-stroke, 90-degree, V12, liquid-cooled aero-engine of 1,593.4 cu.in capacity, featuring sleeve valves and direct petrol injection. Initially intended for a high-speed "sprint" interceptor fighter, the Crecy was later seen as an economical high-altitude long-range powerplant. Developed between 1941 and 1946, it was among the most advanced two-stroke aero-engines ever built. The engine never reached flight trials and the project was cancelled in December 1945, overtaken by the progress of jet engine development.

<span class="mw-page-title-main">Rolls-Royce Falcon</span>

The Rolls-Royce Falcon is an aero engine developed in 1915. It was a smaller version of the Rolls-Royce Eagle, a liquid-cooled V-12 of 867 cu in capacity. Fitted to many British World War I-era aircraft, production ceased in 1927. The Falcon was designed by R.W. Harvey-Bailey.

<span class="mw-page-title-main">Rolls-Royce Goshawk</span> 1930s British piston aircraft engine

The Rolls-Royce Goshawk was a development of the Rolls-Royce Kestrel that used evaporative or steam cooling. In line with Rolls-Royce convention of naming piston engines after birds of prey, it was named after the goshawk.

<span class="mw-page-title-main">X24 engine</span>

The X-24 is one of the few configurations of X-type engines known to have been produced. The design consists of four banks of six cylinders with a common crankshaft. This is lighter than other multi-bank designs, which require multiple crankshafts. Few of the X-24 engines developed saw service, and their production lifetimes were very limited. Postwar developments of the turbojet and turbofan engines obviated the need for large piston aircraft engines of this type.

<span class="mw-page-title-main">Rolls-Royce Pennine</span> 1940s British piston aircraft engine

The Rolls-Royce Pennine was a British 46-litre air-cooled sleeve valve engine with 24 cylinders arranged in an X formation. It was an enlarged version of the 22-litre Exe; a prototype engine was built and tested, but never flew. The project was terminated in 1945, being superseded by the jet engine.

<span class="mw-page-title-main">Rolls-Royce Exe</span> 1930s British piston aircraft engine

The Rolls-Royce Exe, or Boreas, was a 24-cylinder air-cooled X block sleeve valve aircraft engine intended primarily for the new Fairey Fleet Air Arm aircraft, particularly the Fairey Barracuda. The Exe was relatively powerful for its era, producing about 1,100 hp (820 kW). This is notable given the relatively small 1,300 cubic inches (22 L) displacement, the Merlin requiring 1,600 cubic inches (27 L) for approximately the same power level. The X-24 layout made this quite a compact engine.

<span class="mw-page-title-main">Arthur Rubbra</span> English aeronautical engineer and industrial designer

Arthur Alexander Cecil Rubbra CBE was an English engineer who designed many of Rolls-Royce's successful aero engines. He was "placed by many alongside Royce, Rowledge and Elliot as one of Rolls-Royce's greatest engineers...".

The Rolls-Royce Eagle XVI was a British experimental 16 cylinder aero engine designed and developed by Rolls-Royce Limited in 1925. The engine was test run but did not fly, the project, together with the planned larger variant, the Eagle XX, was cancelled in favour of the Rolls-Royce Kestrel, that was being developed concurrently.

Alfred Cyril Lovesey CBE, AFRAeS, was an English engineer who was a key figure in the development of the Rolls-Royce Merlin aero engine.

<span class="mw-page-title-main">Arthur Rowledge</span>

Arthur John Rowledge, was an English engineer who designed the Napier Lion aero engine and was a key figure in the development of the inter-war Rolls-Royce aero piston engines, including the Rolls-Royce Kestrel and the Rolls-Royce Merlin.

References

Notes

  1. Lumsden 2003, pp.183-190.
  2. Lumsden 2003, pp.190-198.
  3. Lumsden 2003, p.198.
  4. Lumsden 2003, p.199.
  5. Lumsden 2003, p.200.
  6. Lumsden 2003, p.221.
  7. Nahum, Foster-Pegg, Birch 2004.
  8. Rubbra 1990, p.148.
  9. Lumsden 2003, p.201.
  10. Lumsden 2003, p.218.
  11. Gunston 1989, p.42.
  12. See individual articles for details
  13. By first run date

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN   1-85260-163-9
  • Nahum, A., Foster-Pegg, R.W., Birch, D. The Rolls-Royce Crecy, Rolls-Royce Heritage Trust. Derby, England. 1994 ISBN   1-872922-05-8
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN   1-85310-294-6.
  • Rubbra, A.A. Rolls-Royce Piston Aero Engines - a designer remembers: Historical Series no 16 :Rolls-Royce Heritage Trust, 1990. ISBN   1-872922-00-7

Further reading