gptkbp:instance_of
|
gptkb:engine
|
gptkbp:bfsLayer
|
4
|
gptkbp:bfsParent
|
gptkb:A340-500
gptkb:Airbus_A340-600
gptkb:A340-600
|
gptkbp:aircraft_operated
|
gptkb:Airbus_A340-500
gptkb:Airbus_A340_family
|
gptkbp:application
|
gptkb:Airbus_A340-500
|
gptkbp:armament
|
composite
|
gptkbp:cancellation_reason
|
compliant with Chapter 4 regulations
|
gptkbp:certification
|
EASA certified
ICAOCAEP/6
|
gptkbp:compression_ratio
|
3-stage
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
gptkbp:cooling_system
|
bypass air
|
gptkbp:developer
|
gptkb:Rolls-Royce_Trent_family
|
gptkbp:diameter
|
2.5 m
2.7 m
112 inches
|
gptkbp:emissions_standard
|
low C O2 emissions
|
gptkbp:engine
|
gptkb:Rolls-Royce_Trent_series
twin-spool
|
gptkbp:engine_type
|
gptkb:Trent_500-22
gptkb:Trent_500-29
gptkb:Trent_500-30
gptkb:Trent_500-32
gptkb:Trent_500-36
gptkb:Trent_500-38
gptkb:3
2
turbofan
axial compressor
Trent 500-34
Trent 500-40
Trent 500-42
Trent 500-44
three-stage high-pressure turbine
|
gptkbp:first_flight
|
gptkb:2001
|
gptkbp:fuel_capacity
|
2.7 m
4,000 kg
3.4 m
high efficiency for long-haul flights
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
can-annular combustor
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Trent 500
|
gptkbp:length
|
3.4 m
|
gptkbp:maintenance
|
6,000 hours
approximately 6,000 cycles
|
gptkbp:manufacturer
|
gptkb:film_production_company
gptkb:Rolls-Royce
|
gptkbp:market
|
significant in wide-body aircraft
|
gptkbp:noise_level
|
Chapter 4 compliant
|
gptkbp:operational_area
|
high bypass ratio
|
gptkbp:operational_range
|
up to 8,000 km
|
gptkbp:produced_by
|
over 1,000 engines
|
gptkbp:propulsion
|
53,000 lbf
13.25:1
50,000 to 60,000 lbf
|
gptkbp:services
|
gptkb:2002
|
gptkbp:setting
|
high-bypass turbofan
|
gptkbp:successor
|
gptkb:Rolls-Royce_Trent_7000
gptkb:Trent_XWB
|
gptkbp:technology
|
three-shaft design
|
gptkbp:valve_configuration
|
2-stage
1-stage
|
gptkbp:variant
|
gptkb:Trent_800
gptkb:Trent_700
|
gptkbp:weight
|
4,000 kg
approximately 4,000 lb
|