Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
H-block
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
1940s
|
| gptkbp:displacement |
46 liters
|
| gptkbp:engineType |
liquid-cooled
H-24 |
| gptkbp:firstFlight |
1944
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFeature |
complex H-block design
|
| gptkbp:numberOfEngines |
24
|
| gptkbp:powerOutput |
3,500 hp
|
| gptkbp:predecessor |
Rolls-Royce Eagle (WWI engine)
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:successor |
none
|
| gptkbp:usedIn |
gptkb:Westland_Wyvern
|
| gptkbp:valveConfiguration |
sleeve valve
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Griffon_piston_engines
gptkb:Rolls-Royce_Griffon_V12_piston_engine |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Eagle 22
|