|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:bypass_ratio
|
8:1
9:1
|
|
gptkbp:certification
|
EASA and FAA certified
|
|
gptkbp:combustor_type
|
dry low emissions
|
|
gptkbp:competitors
|
gptkb:General_Electric_GEnx
gptkb:Pratt_&_Whitney_PW1100_G
|
|
gptkbp:components
|
gptkb:fans
high-pressure turbine
low-pressure turbine
high-pressure compressor
fan blades
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
advanced cooling technology
|
|
gptkbp:customer_support
|
gptkb:Air_Asia_X
gptkb:Cathay_Pacific
gptkb:Etihad_Airways
gptkb:British_Airways
gptkb:Singapore_Airlines
gptkb:Turkish_Airlines
gptkb:Airbus
gptkb:Iberia
gptkb:Qantas
gptkb:Virgin_Atlantic
global support network
|
|
gptkbp:design_features
|
advanced aerodynamics
enhanced performance
lightweight materials
modular design
reduced maintenance costs
high efficiency
improved reliability
|
|
gptkbp:designed_for
|
gptkb:Airbus
|
|
gptkbp:developed_by
|
gptkb:Rolls-Royce_Trent_1000
|
|
gptkbp:development
|
Rolls-Royce Trent 7000 program
|
|
gptkbp:development_cost
|
significant investment
|
|
gptkbp:diameter
|
81 inches
|
|
gptkbp:elevation
|
up to 43,000 feet
|
|
gptkbp:emissions_standard
|
lower CO2 emissions
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Trent_XWB
gptkb:Rolls-Royce_Trent_1000
air-start system
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:environmental_impact
|
lower emissions than predecessors
|
|
gptkbp:first_flight
|
gptkb:2017
|
|
gptkbp:fuel_capacity
|
2.06 m
3.5 m
|
|
gptkbp:fuel_economy
|
improved over Trent 1000
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Trent 7000
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:maintenance
|
20,000 hours
longer than previous models
|
|
gptkbp:manufacturer
|
gptkb:Ford_Motor_Company
gptkb:Rolls-Royce
|
|
gptkbp:market_position
|
leading engine for A330neo
|
|
gptkbp:market_segment
|
wide-body aircraft
|
|
gptkbp:noise_level
|
compliant with Chapter 14 regulations
|
|
gptkbp:operational_period
|
long-range missions
|
|
gptkbp:performance
|
high reliability
low maintenance costs
high thrust-to-weight ratio
compatible with various aircraft systems
excellent climb performance
suitable for long-haul flights
optimized for fuel economy
|
|
gptkbp:project
|
potential upgrades planned
next-generation engine concepts
|
|
gptkbp:propulsion
|
68,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Airbus_A330-800
gptkb:Airbus_A330-900
|
|
gptkbp:service_entry
|
gptkb:2018
|
|
gptkbp:support
|
gptkb:Rolls-Royce_Total_Care_service
|
|
gptkbp:technology
|
advanced materials
digital engine control
noise-reducing features
high bypass ratio design
3 D-printed components
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
lightweight design
approximately 3,000 lbs
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Airbus
|
|
gptkbp:bfsLayer
|
4
|