Statements (90)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:aircraft_operated |
gptkb:Embraer_Praetor_600
gptkb:Gulfstream_G700 gptkb:Bombardier_Global_7500 designed for easy integration into aircraft |
| gptkbp:application |
gptkb:engine
|
| gptkbp:armament |
composite materials
|
| gptkbp:cancellation_reason |
gptkb:battle
|
| gptkbp:certification |
gptkb:Federal_Aviation_Administration_(FAA)
gptkb:European_Union_Aviation_Safety_Agency_(EASA) FAA certified CAEP/6 compliant |
| gptkbp:competitors |
gptkb:Rolls-Royce_Pearl_15
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system digital engine control system |
| gptkbp:cooling_system |
air-cooled
advanced cooling techniques |
| gptkbp:customer_base |
business jet manufacturers
|
| gptkbp:customer_support |
global customer support network
|
| gptkbp:diameter |
approximately 40 inches
approximately 40 in approximately 36 in approximately 105 cm |
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissions_standard |
CAEP/6
mixed flow |
| gptkbp:engine |
gptkb:GE_Passport
high performance high reliability improved efficiency advanced features twin-spool various aircraft models innovative technology ongoing development global support network state-of-the-art design growing market available upgrades detailed specifications P W800 family |
| gptkbp:engine_type |
gptkb:6
gptkb:engine 2 multiple variants high bypass ratio single crystal superalloy |
| gptkbp:environmental_impact |
designed to minimize environmental impact
|
| gptkbp:facilities |
Pratt & Whitney test facility
|
| gptkbp:fan_art |
wide chord fan
|
| gptkbp:features |
low emissions
increased efficiency modular design high bypass ratio reduced noise levels |
| gptkbp:first_flight |
gptkb:2015
|
| gptkbp:fuel_capacity |
high
0.5 lb/lbf/hr improved fuel efficiency over previous models |
| gptkbp:fuel_type |
gptkb:Jet_A
annular combustor advanced fuel system design |
| gptkbp:has_programs |
joint development with Bombardier
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW800-19 engine
|
| gptkbp:is_tested_for |
extensive testing
|
| gptkbp:launched |
air start
|
| gptkbp:legal_issue |
turbofan
|
| gptkbp:length |
approximately 60 inches
approximately 60 in |
| gptkbp:maintenance |
5,000 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:market_segment |
business aviation
|
| gptkbp:noise_level |
low noise
Stage 4 compliant |
| gptkbp:number_of_stages |
10 stages
|
| gptkbp:operational_area |
high altitude
hot and cold temperatures |
| gptkbp:operational_range |
high altitude
|
| gptkbp:project |
ongoing research for next generation engines
|
| gptkbp:propulsion |
up to 20,000 lbf
13.3:1 |
| gptkbp:rating |
high performance rating in its class
|
| gptkbp:service_ceiling |
45,000 ft
|
| gptkbp:services |
gptkb:2016
|
| gptkbp:supports |
high airflow
|
| gptkbp:technology |
geared turbofan
|
| gptkbp:warranty |
standard warranty
standard warranty offered |
| gptkbp:weight |
approximately 1,500 lb
|