Rolls-Royce 290 HP

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:Sir_Henry_Royce
gptkbp:application military and civilian aircraft
gptkbp:compression_ratio 6.5:1
gptkbp:controls mechanical controls
gptkbp:cooling_system liquid-cooled
water-cooled
efficient cooling system
gptkbp:displacement 36.7 liters
gptkbp:engine gptkb:Rolls-Royce_K_series
gptkb:12
aerodynamic efficiency
commercial aviation
varies with altitude
longitudinal
high reliability rating
limited production runs
introduced new technologies
important in aviation history
detailed in technical manuals
designed for ease of maintenance
characterized by smooth operation
optimized for altitude
part of Rolls-Royce heritage
pioneered several advancements
supercharged option available
gptkbp:engine_type reciprocating engine
multiple variants produced
high output at low RP Ms
gptkbp:first_introduced 1930s
gptkbp:fuel_capacity variable based on load
gptkbp:fuel_type aviation gasoline
gptkbp:historical_significance used in WWII aircraft
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce 290 HP
gptkbp:ignition_system dual ignition
gptkbp:is_tested_for extensively tested for performance
used advanced testing facilities
gptkbp:legacy influenced future engine designs
gptkbp:maintenance requires regular servicing
gptkbp:manufacturer gptkb:Rolls-Royce_Limited
gptkbp:notable_users gptkb:Avro_683_Lancaster
gptkbp:performance high power-to-weight ratio
gptkbp:powers 290 horsepower
gptkbp:production_years 1930s to 1940s
gptkbp:reliability known for durability
gptkbp:setting V-type
gptkbp:successor gptkb:Rolls-Royce_R_engine
gptkbp:torque high torque output
gptkbp:type gptkb:engine
gptkbp:used_in various aircraft
gptkbp:valve_configuration overhead valves
gptkbp:weight approximately 1,200 pounds