Statements (86)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
3
|
| gptkbp:bfsParent |
gptkb:aircraft
|
| gptkbp:aircraft_operated |
gptkb:Airbus_A330-800
gptkb:Airbus_A330-900 |
| gptkbp:application |
commercial aviation
|
| gptkbp:bypass_ratio |
8:1
9:1 |
| gptkbp:certification |
EASA and FAA certified
|
| gptkbp:competitors |
General Electric G Enx
Pratt & Whitney P W1100 G |
| gptkbp:controls |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:cooling_system |
advanced cooling technology
|
| gptkbp:customer_support |
gptkb:aircraft
gptkb:Air_Asia_X gptkb:Cathay_Pacific gptkb:Etihad_Airways gptkb:British_Airways gptkb:Singapore_Airlines gptkb:Turkish_Airlines gptkb:Iberia gptkb:Qantas gptkb:Virgin_Atlantic global support network |
| gptkbp:developed_by |
gptkb:Rolls-Royce_Trent_1000
|
| gptkbp:developer |
significant investment
Rolls-Royce Trent 7000 program |
| gptkbp:diameter |
81 inches
|
| gptkbp:elevation |
up to 43,000 feet
|
| gptkbp:emissions_standard |
lower C O2 emissions
|
| gptkbp:engine |
gptkb:Rolls-Royce_Trent_XWB
gptkb:Rolls-Royce_Trent_1000 twin-spool air-start system |
| gptkbp:engine_type |
turbofan
|
| gptkbp:environmental_impact |
lower emissions than predecessors
|
| gptkbp:features |
advanced aerodynamics
enhanced performance lightweight materials modular design reduced maintenance costs high efficiency improved reliability |
| gptkbp:first_flight |
gptkb:2017
|
| gptkbp:fuel_capacity |
2.06 m
3.5 m improved over Trent 1000 |
| gptkbp:fuel_type |
gptkb:Jet_A-1
dry low emissions |
| gptkbp:game_components |
gptkb:fandom
high-pressure turbine low-pressure turbine high-pressure compressor fan blades |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Trent 7000
|
| gptkbp:is_designed_for |
gptkb:aircraft
|
| gptkbp:is_tested_for |
extensive ground testing
|
| gptkbp:maintenance |
20,000 hours
longer than previous models |
| gptkbp:manufacturer |
gptkb:film_production_company
gptkb:Rolls-Royce |
| gptkbp:market |
leading engine for A330neo
|
| gptkbp:market_segment |
wide-body aircraft
|
| gptkbp:noise_level |
compliant with Chapter 14 regulations
|
| gptkbp:operational_area |
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:services |
gptkb:2018
|
| gptkbp:supports |
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 |