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.
Observed surface forms (1)
| Surface form | Occurrences |
|---|---|
| Siddeley Puma | 0 |
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 NERFINISHED ⓘ |
| firstFlightInServicePeriod | circa 1917 ⓘ |
| fuelType | aviation gasoline ⓘ |
| historicalSignificance | widely used British WWI inline engine ⓘ |
| ignitionSystem | magneto ignition ⓘ |
| manufacturer |
Armstrong Siddeley
NERFINISHED
ⓘ
Siddeley-Deasy NERFINISHED ⓘ |
| notableUser |
Airco D.H.10 (early versions)
NERFINISHED
ⓘ
Airco D.H.9 NERFINISHED ⓘ Bristol F.2B (some variants) NERFINISHED ⓘ Royal Aircraft Factory R.E.8 (some aircraft) NERFINISHED ⓘ |
| powerOutput | approximately 230 hp ⓘ |
| productionPeriod | late 1910s ⓘ |
| propellerDrive | direct drive ⓘ |
| stroke | approximately 190 mm ⓘ |
| successor | Armstrong Siddeley Jaguar NERFINISHED ⓘ |
| usedBy |
British military aviation
ⓘ
Royal Air Force ⓘ Royal Flying Corps NERFINISHED ⓘ |
| usedFor |
frontline service in WWI
ⓘ
postwar surplus aircraft ⓘ |
| usedInConflict | First World War NERFINISHED ⓘ |
| valveConfiguration |
overhead camshaft
ⓘ
single overhead camshaft ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.