Properties (55)
Predicate | Object |
---|---|
gptkbp:instanceOf |
turbofan engine
|
gptkbp:application |
gptkb:Boeing_747
Lockheed L-1011 TriStar |
gptkbp:certifications |
gptkb:EASA
gptkb:FAA |
gptkbp:controls |
FADEC
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:diameter |
2.5 m
|
gptkbp:engine |
3D printing
advanced aerodynamics lightweight materials advanced materials computer-aided design noise reduction technologies modular aerodynamic optimization high temperature materials high-pressure compressor design low-pressure turbine design modular maintenance design advanced fuel systems digital engine control engine performance optimization advanced combustion systems high-efficiency fan blades low emissions combustion technology vibration control systems thermal barrier coatings high bypass ratio fan engine health monitoring systems high efficiency turbine design |
gptkbp:engineType |
24
axial high-bypass turbofan high bypass ratio |
gptkbp:firstFlight |
1989
|
gptkbp:fuel_capacity |
0.5 lb/hp/hr
|
gptkbp:fuelType |
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label |
RB211-524G
|
gptkbp:inspiration |
fuel efficiency
reduced emissions low noise |
gptkbp:length |
3.5 m
|
gptkbp:maintenance |
4,000 hours
|
gptkbp:manufacturer |
gptkb:Rolls-Royce
|
gptkbp:noise_level |
Stage 3 compliant
|
gptkbp:operationalRange |
long-haul
|
gptkbp:operationalStatus |
commercial aviation
|
gptkbp:propulsion |
53,000 lbf
|
gptkbp:related_engine |
gptkb:RB211-524B
gptkb:RB211-524H |
gptkbp:serviceType |
1990
|
gptkbp:setting |
dual-spool
|
gptkbp:successor |
gptkb:RB211-535
|
gptkbp:weight |
4,000 kg
|