Siddeley Puma engine

E487135

The Siddeley Puma engine was a British six-cylinder, water-cooled inline aircraft engine widely used in World War I-era military aircraft.

All labels observed (1)

Label Occurrences
Siddeley Puma engine canonical 1

How this entity was disambiguated

Statements (42)

Predicate Object
instanceOf aircraft engine
inline engine
piston engine
application bombers
military aircraft
reconnaissance aircraft
bore approximately 140 mm
category World War I aircraft piston engine
inline-six engine
water-cooled aircraft engine
configuration six-cylinder inline
coolant water
coolingSystem water-cooled
countryOfOrigin United Kingdom
cylinderCount 6
designOrigin based on B.H.P. engine design
displacement approximately 18.9 litres
engineCycle four-stroke
era World War I
firstFlightInServicePeriod circa 1917
fuelType aviation gasoline
historicalSignificance widely used British WWI inline engine
ignitionSystem magneto ignition
manufacturer Armstrong Siddeley
Siddeley-Deasy
linked to: D. Napier & Son
notableUser Airco D.H.10 (early versions)
linked to: Airco DH.10

Airco D.H.9
linked to: Airco DH.9

Bristol F.2B (some variants)
linked to: Bristol F.2 Fighter

Royal Aircraft Factory R.E.8 (some aircraft)
powerOutput approximately 230 hp
productionPeriod late 1910s
propellerDrive direct drive
stroke approximately 190 mm
successor Armstrong Siddeley Jaguar
usedBy British military aviation
Royal Air Force
Royal Flying Corps
usedFor frontline service in WWI
postwar surplus aircraft
usedInConflict First World War
linked to: World War I
valveConfiguration overhead camshaft
single overhead camshaft

How these facts were elicited

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Airco DH.9 powerplant Siddeley Puma engine