|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Fokker_100
|
|
gptkbp:application
|
gptkb:engine
|
|
gptkbp:average_temperature
|
1500 K
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Tay
gptkb:Rolls-Royce_Tay_611
gptkb:Rolls-Royce_Tay_650
in production
high reliability
twin-engine
Brayton cycle
high efficiency
twin-spool
high bypass ratio
bleed air start
|
|
gptkbp:engine_type
|
gptkb:Tay_620-15
gptkb:Tay_620-17
gptkb:Tay_620-18
turbojet
axial
high-pressure turbine
low-pressure turbine
Tay 620-16
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
0.5 lb/h/lbf
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Tay 620
|
|
gptkbp:is_tested_for
|
flight testing
ground testing
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
5000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:max_speed
|
Mach 0.85
|
|
gptkbp:noise_level
|
gptkb:Stage_4
low noise
|
|
gptkbp:notable_users
|
gptkb:Gulfstream_G550
gptkb:Dassault_Falcon_7_X
gptkb:Bombardier_Global_Express
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:propulsion
|
6200 lbf
4.13 lbf/kg
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:weight
|
1500 kg
|