Alvis Leonides

{{short description|1930s British piston aircraft engine}}

{{Use dmy dates|date=May 2019}}

{{EngvarB|date=May 2019}}

{{Infobox aircraft begin

|name= Leonides

|image= File:Alvis Leonides EMA.jpg

|caption= Alvis Leonides on display at the East Midlands Aeropark

}}{{Infobox aircraft engine

|type= Radial engine

|manufacturer= Alvis

|national origin= United Kingdom

|first run= 1936

|major applications= Percival Pembroke
Scottish Aviation Twin Pioneer

|number built =

|program cost =

|unit cost =

|developed from =

|variants with their own articles =

|developed into = Alvis Leonides Major

}}

The Alvis Leonides is a British air-cooled nine-cylinder radial aero engine first developed by Alvis Car and Engineering Company in 1936.Gunston 1989, p.13.

Design and development

Development of the nine-cylinder engine was led by Capt. George Thomas Smith-Clarke. The prototype engine, called 9ARS and which weighed 693 lb and developed 450 hp, was run in December 1936. In 1938 Airspeed (1934) Ltd lent their test pilot, George Errington, and their much rebuilt Bristol Bulldog (K3183), to carry out test flights. Development was continued at a reduced pace during the Second World War and following testing in an Airspeed Oxford and an Airspeed Consul (VX587). Alvis was ready to market the engine in 1947 as the Series 500 (502, 503 and sub-types) for aeroplanes and Series 520 for helicopters. (Most helicopter engines were direct drive — no reduction gearbox — with a centrifugal clutch and fan cooling). The first production use was the Percival Prince, which flew in July 1948 and the Westland Sikorsky S-51 and Westland WS-51 Dragonfly helicopters. From 1959 the stroke was increased to 4.8 inches for the Series 530 (mainly the Mk. 531 for Twin Pioneers) rated at 640 hp. It was Britain's last high-power production piston aero-engine when manufacture ceased in 1966.

Variants

Notes: LE designations from Air Ministry system (where known); 500 series designations from Alvis company designation system; Mark numbers for civil variants.

;Alvis 9ARS: pre-war precursor to the Leonides – {{convert|450|hp|abbr=on}}/ 0.5:1

;LE.1M:(Leonides 501/1) – {{convert|520|hp|abbr=on}}/3,000 rpm/+6.6 lb boost/ 0.5:1

;LE.2M:(Leonides 501/2) – 0.625:1 reduction gearing, remote accessories

;LE.3M:(Leonides 501/3) – 0.5:1 reduction gearing, remote accessories

;LE.4M:(Leonides 501/4) – 0.625:1 reduction gearing

;LE.12HMH:(Leonides 522/2) Horizontal direct-drive for helicopters

;LE.21HMV:(Leonides 522/1) Vertical direct-drive for helicopters

;LE.23HM:(Leonides 524/1) Vertical direct-drive for helicopters

;LE.24HMV:(Leonides 524/1) Vertical opposite rotation reduction-geared drive for helicopters

;LE.25HMV:(Leonides 523/1)

;Leonides 501:{{convert|500|hp|abbr=on}}/3,000 rpm/+6.6 lb boost/ 0.5:1

;Leonides 502:{{convert|520|/|540|hp|abbr=on}}

;Leonides 503:{{convert|520|-|560|hp|abbr=on}}

;Leonides 504:{{convert|520|/|540|hp|abbr=on}}

;Leonides 514:{{convert|550|-|560|hp|abbr=on}}

;Leonides 521:{{convert|480|-|540|hp|abbr=on}}

;Leonides 522:{{convert|520|-|570|hp|abbr=on}}

;Leonides 523:{{convert|520|/|540|hp|abbr=on}} Helicopter vertical drive

;Leonides 524:{{convert|500|/|520|hp|abbr=on}} Helicopter vertical drive

;Leonides 525:{{convert|500|/|520|hp|abbr=on}}

;Leonides 530:{{convert|540|hp|abbr=on}} Long stroke

;Leonides 531:{{convert|640|/|650|hp|abbr=on}} Long stroke (+ 10mm), supercharger ratio 6.5:1

;Leonides 532:{{convert|620|hp|abbr=on}} Long stroke (+ 10mm), supercharger ratio 7.91:1

;Leonides Mark 22:(Leonides 503/2)

;Leonides Mark 24:(Leonides 503/4)

;Leonides Mark 50:(Leonides 521/2)

;Leonides Mark 70:(Leonides 523/1)

;Leonides Mark 125:(Leonides 504/5)

;Leonides Mark 125 01/2:(Leonides 503/5)

;Leonides Mark 126:(Leonides 503/6A)

;Leonides Mark 127 01/2:(Leonides 503/7A)

;Leonides Mark 128:(Leonides 504/8B)

;Leonides Mark 130:(Leonides 503/7)

;Leonides Mark 138:(Leonides 531/8B) {{convert|640|/|650|hp|abbr=on}} Long stroke (+ 10mm)

;Leonides Mark 173:(Leonides 524/1 & 525/1)

File:Alvis Leonides Mk 173-02.jpg]]

Applications

Survivors

  • A Leonides 126-powered Hunting Percival Provost (G-KAPW) with CAA permission to fly as XF603, owned by the Shuttleworth Trust and based at Old Warden, Bedfordshire is airworthy as of 2017, and is displayed to the public at home airshows during the airshow season.[http://www.shuttleworth.org/collection/percivalprovost/ The Shuttleworth Collection - Provost] {{Webarchive|url=https://web.archive.org/web/20170616065333/http://www.shuttleworth.org/collection/percivalprovost/ |date=16 June 2017 }} Retrieved 28 February 2017.
  • The world's only surviving Gloster Gauntlet, formerly powered by a Bristol Mercury VI engine, is now powered by a Leonides 503.
  • A privately owned, Leonides-powered Percival Pembroke remains airworthy in March 2010.{{cite web |url=http://www.caa.co.uk/application.aspx?catid=60&pagetype=65&appid=1&mode=detail&aircrafttype=pembroke&dataindex=0 |title=GINFO Search Results {{!}} Aircraft Register {{!}} Safety Regulation |website=www.caa.co.uk |url-status=dead |archive-url=https://web.archive.org/web/20110606114419/http://www.caa.co.uk/application.aspx?catid=60&pagetype=65&appid=1&mode=detail&aircrafttype=pembroke&dataindex=0 |archive-date=2011-06-06}}
  • Two privately owned Scottish Aviation Twin Pioneers are flying in Australia

Engines on display

Preserved Alvis Leonides engines are on public display at the following museums:

Specifications (Leonides)

File:AlvisLeonides.JPG]]

{{pistonspecs

|

|type= 9-cylinder supercharged air-cooled radial piston engine.

|bore= 4.8 inch (122 mm)

|stroke= 4.41 inch (112 mm)

|displacement= 718.6 in3 (11.8 L)

|length=

|diameter= 41 inch (1.04 m)

|width=

|height=

|weight= 815 lb (370 kg)

|valvetrain= Two pushrod-actuated poppet valves per cylinder with sodium-cooled exhaust valve.

|supercharger= Single speed, single stage, boost pressure automatically linked to the throttle.

|turbocharger=

|fuelsystem= Hobson single-point fuel injection unit.

|fueltype= Petrol, 115 Octane

|oilsystem= Dry sump

|coolingsystem= Air-cooled.

|power= 550 hp (410 kW)

|specpower=

|compression=

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=

}}

See also

References

;Notes

{{Reflist}}

;Bibliography

{{refbegin}}

  • 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}}.

{{refend}}