|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Lockheed_L-1011_Tri_Star
gptkb:Vickers_VC10
|
|
gptkbp:combustor_type
|
annular combustion chamber
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
hydromechanical control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:design_date
|
1950s
|
|
gptkbp:development
|
1955 to 1959
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
modular design
bleed air start
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:Conway_600
Conway 1000
Conway 1100
Conway 1200
Conway 1300
Conway 1400
Conway 1500
Conway 1600
Conway 1700
Conway 1800
Conway 1900
Conway 2000
Conway 2100
Conway 2200
Conway 2300
Conway 2400
Conway 2500
Conway 2600
Conway 2700
Conway 2800
Conway 2900
Conway 3000
Conway 500
Conway 700
Conway 800
Conway 900
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1959
|
|
gptkbp:fuel_capacity
|
3 ft 6 in
12 ft 6 in
|
|
gptkbp:fuel_economy
|
good fuel efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Conway
|
|
gptkbp:is_tested_for
|
gptkb:Rolls-Royce_test_facility
|
|
gptkbp:maintenance
|
long maintenance intervals
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
high bypass ratio
|
|
gptkbp:number_of_engines
|
2 to 4
|
|
gptkbp:operational_use
|
gptkb:civil_aviation
|
|
gptkbp:power_output
|
16,000 to 22,000 lbf
|
|
gptkbp:propulsion
|
22,000 lbf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:retirement_year
|
gptkb:1980s
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB211
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
axial-flow turbojet
|
|
gptkbp:used_in
|
gptkb:Boeing_707
gptkb:Douglas_DC-8
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Handley_Page_Victor
|
|
gptkbp:bfsLayer
|
5
|