ABC Scorpion

1920s British piston aircraft engine


title: "ABC Scorpion" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["abc-aircraft-engines", "1920s-aircraft-piston-engines"] description: "1920s British piston aircraft engine" topic_path: "general/abc-aircraft-engines" source: "https://en.wikipedia.org/wiki/ABC_Scorpion" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary 1920s British piston aircraft engine ::

::data[format=table title="infobox aero engine"]

FieldValue
nameScorpion
imageFile:ABC Scorpion I.jpg
captionABC Scorpion I on display at the Shuttleworth Collection
engine_typeFlat-twin aero engine
national_originUnited Kingdom
manufacturerABC Motors
designerGranville Bradshaw
first_run1921
::

|name = Scorpion |image = File:ABC Scorpion I.jpg |caption = ABC Scorpion I on display at the Shuttleworth Collection |engine_type = Flat-twin aero engine |national_origin = United Kingdom |manufacturer = ABC Motors |designer = Granville Bradshaw |first_run =1921 |major_applications = |produced = |number_built = |developed_from = |variants_with_their_own_articles =

The ABC Scorpion is a 30 hp (22 kW) two-cylinder aero engine designed by British engineer Granville Bradshaw for use in light aircraft. The engine was built by ABC Motors Limited and first ran in 1921.

Variants

;Scorpion I :1923, 30 hp (22 kW) ;Scorpion II :1924, 34 hp (25 kW), increased bore and stroke.

Applications

::figure[src="https://upload.wikimedia.org/wikipedia/commons/d/df/ABCScorpion.JPG" caption="ANEC II]] at the [[Shuttleworth Collection"] ::

Survivors

The only ANEC II (G-EBJO) flies regularly at the Shuttleworth Collection at Old Warden and is powered by a Scorpion II.

Specifications (Scorpion I)

|ref=Lumsden |type=2 cylinder air cooled flat-twin |bore=3.6 in (87.5 mm) |stroke=3.7 in (91.5 mm) |displacement=73.32 cu in (1.1 L) |length= |diameter= |width= |height= |weight=90 lb (41 kg) |valvetrain= Overhead valve, two valves per cylinder |supercharger= |turbocharger= |fuelsystem= Carburettor |fueltype=74 Octane petrol |oilsystem= |coolingsystem=Air |power=30 hp (22 kW) at 2,750 rpm |specpower= |compression=4:1 |fuelcon= |specfuelcon= |oilcon= |power/weight= 0.33 hp/lb (0.53 kW/kg)

References

Notes

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.
  • Guttery, T.E. The Shuttleworth Collection. London: Wm. Carling, 1969.
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. .

References

  1. Gunston 1989, p.9.
  2. Lumsden 2003, p.54.

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