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 ⓘ