Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
military and civilian aircraft
|
| gptkbp:certification |
certified by aviation authorities
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
V engine
|
| gptkbp:control_system |
mechanical throttle control
mechanical throttle |
| gptkbp:cooling_system |
gptkb:Cooler
liquid-cooled radiator system |
| gptkbp:displacement |
27.0 liters
|
| gptkbp:engine |
four-stroke
upgraded versions developed produced in limited numbers used in training aircraft legacy in aviation engineering |
| gptkbp:engine_configuration |
inline engine
innovative design features front-mounted rated for 170 HP at 2,400 RPM |
| gptkbp:engine_power |
high reliability
known for reliability good fuel efficiency approximately 1,500 hours |
| gptkbp:engine_startup |
manual startup procedure
|
| gptkbp:engine_type |
multiple variants available
|
| gptkbp:first_introduced |
1930s
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| gptkbp:historical_significance |
important in aviation history
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 170 HP
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:is_tested_for |
extensive testing conducted
|
| gptkbp:maintenance |
regular maintenance required
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:noise_level |
moderate noise level
|
| gptkbp:notable_users |
gptkb:Avro_504_K
|
| gptkbp:powers |
170 horsepower
|
| gptkbp:production_years |
1930s to 1940s
|
| gptkbp:propeller |
variable pitch
|
| gptkbp:propulsion |
favorable power-to-weight ratio
|
| gptkbp:successor |
gptkb:Rolls-Royce_200_HP
|
| gptkbp:torque |
high torque output
pressure lubrication system |
| gptkbp:type |
gptkb:V8_engine
|
| gptkbp:used_in |
various aircraft
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
approximately 600 lbs
|
| gptkbp:bfsParent |
gptkb:Sir_Henry_Royce
|
| gptkbp:bfsLayer |
5
|