Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Mc_Donnell_Douglas_MD-95-30
|
| gptkbp:application |
gptkb:Airbus_A220
gptkb:Embraer_E-Jet_E2 Bombardier C Series |
| gptkbp:cancellation_reason |
up to 75% quieter than previous engines
|
| gptkbp:certification |
FAA certification
|
| gptkbp:competitors |
gptkb:CFM_International_LEAP
gptkb:Rolls-Royce_Trent_1000 |
| gptkbp:diameter |
81 inches
|
| gptkbp:emissions_standard |
meets CAEP/6 standards
|
| gptkbp:engine_type |
gptkb:6
2 |
| gptkbp:first_flight |
gptkb:2013
|
| gptkbp:fuel_capacity |
up to 16% better than previous engines
|
| gptkbp:fuel_type |
annular combustor
|
| gptkbp:has_programs |
GTF program
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney PW 1000 G
|
| gptkbp:key |
advanced aerodynamics
enhanced performance high durability modular design advanced materials reduced maintenance costs improved thermal efficiency lightweight design high efficiency advanced cooling technology advanced diagnostics reduced carbon footprint improved reliability high thrust-to-weight ratio enhanced safety features real-time monitoring capabilities digital engine control low emissions technology low noise technology increased operational flexibility sustainable aviation fuel compatibility improved fuel burn modular maintenance approach geared architecture high bypass ratio design integrated propulsion system advanced engine monitoring systems |
| gptkbp:maintenance |
up to 10,000 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:market_segment |
regional and narrow-body aircraft
|
| gptkbp:operational_area |
high bypass ratio
|
| gptkbp:propulsion |
15,000 to 33,000 lbf
|
| gptkbp:services |
gptkb:2016
|
| gptkbp:technology |
gptkb:Geared_Turbofan
|
| gptkbp:weight |
approximately 3,000 lbs
|