Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:compression_ratio |
5.5:1
|
| gptkbp:configuration |
gptkb:V12
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
27.0 L
|
| gptkbp:engine |
four-stroke
over 1,000 units renowned for quality part of aviation history influenced future designs biplanes dual ignition historically significant engine introduced several innovations 120 k W developed during WWI unique design features noted |
| gptkbp:engine_configuration |
inline engine
V-type engine detailed specifications available notable characteristics documented |
| gptkbp:engine_contributions |
contributed to aviation advancements
|
| gptkbp:engine_power |
high reliability
good performance at altitude performance metrics analyzed 2,000 RPM |
| gptkbp:engine_type |
multiple variants available
|
| gptkbp:first_introduced |
gptkb:1917
|
| gptkbp:fuel_capacity |
800 mm
1,200 mm 600 mm |
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 160 HP
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:is_tested_for |
extensively tested
|
| gptkbp:maintenance |
moderate maintenance required
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_users |
gptkb:Royal_Air_Force
|
| gptkbp:powers |
160 horsepower
|
| gptkbp:production_years |
1917-1925
|
| gptkbp:propulsion |
0.4 hp/lb
|
| gptkbp:replaced_by |
gptkb:Rolls-Royce_Kestrel
|
| gptkbp:successor |
gptkb:Rolls-Royce_Eagle
|
| gptkbp:torque |
400 Nm
|
| gptkbp:type |
gptkb:V8_engine
|
| gptkbp:used_in |
various aircraft
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 400 lb
|
| gptkbp:bfsParent |
gptkb:Sir_Henry_Royce
|
| gptkbp:bfsLayer |
5
|