Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:armament |
composite materials
|
| gptkbp:average_temperature |
high temperature capability
|
| gptkbp:cancellation_reason |
compliant with Stage 4 noise regulations
|
| gptkbp:certification |
FAA certified
|
| gptkbp:combustor_type |
dry low NOx
|
| gptkbp:competitors |
gptkb:Rolls-Royce_Trent_1000
|
| gptkbp:compressor_type |
gptkb:6
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:customer_base |
global airlines
|
| gptkbp:customer_support |
gptkb:All_Nippon_Airways
comprehensive service agreements |
| gptkbp:design |
GE Aviation engineers
|
| gptkbp:design_purpose |
fuel efficiency and reduced emissions
|
| gptkbp:designed_for |
gptkb:Boeing_787_Dreamliner
|
| gptkbp:development |
part of the GEnx family
|
| gptkbp:diameter |
78 inches
|
| gptkbp:emissions_standard |
lower than previous generation engines
|
| gptkbp:engine |
advanced aerodynamics
collaborations with aerospace companies ongoing improvements and upgrades incorporates latest technologies widely available for airlines |
| gptkbp:engine_configuration |
detailed technical specifications available.
twin spool |
| gptkbp:engine_power |
high reliability ratings
optimized for long-haul flights |
| gptkbp:engine_type |
GEnx-1 B and GEnx-2 B
|
| gptkbp:environmental_impact |
lower carbon footprint
|
| gptkbp:first_flight |
gptkb:2007
|
| gptkbp:fuel_burn |
reduced fuel burn compared to older engines
|
| gptkbp:fuel_capacity |
lightweight design
approximately 11.5 ft approximately 7.5 ft |
| gptkbp:fuel_economy |
improved over previous models
|
| gptkbp:fuel_type |
Jet A or Jet A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric GEnx-2 B
|
| gptkbp:investment |
high pressure ratio
|
| gptkbp:is_tested_for |
extensive ground testing
state-of-the-art testing facilities |
| gptkbp:maintenance |
longer intervals than predecessors
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_period |
high bypass ratio
|
| gptkbp:part_of |
GE Aviation product line
|
| gptkbp:produces |
manufactured in multiple locations
|
| gptkbp:propulsion |
cascade
53,000 to 76,000 lbf |
| gptkbp:related_aircraft |
gptkb:Boeing_787
|
| gptkbp:service_entry |
gptkb:2011
|
| gptkbp:successor |
gptkb:General_Electric_GEnx-1_B
|
| gptkbp:turbine_type |
2
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
approximately 8,000 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_GEnx-1_B
|
| gptkbp:bfsLayer |
6
|