|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
94 inches
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:first_flight
|
gptkb:1984
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW4000 family
|
|
gptkbp:innovation
|
high bypass ratio
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:number_of_engines
|
over 1,000
|
|
gptkbp:propulsion
|
18,500 to 33,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1984
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:variant
|
gptkb:PW4000-100
gptkb:PW4000-112
gptkb:PW4000-94
gptkb:PW4000-114
gptkb:PW4000-115
gptkb:PW4000-116
gptkb:PW4000-117
gptkb:PW4000-118
gptkb:PW4000-119
gptkb:PW4000-120
gptkb:PW4000-121
gptkb:PW4000-122
gptkb:PW4000-123
gptkb:PW4000-124
gptkb:PW4000-125
gptkb:PW4000-126
PW4000-113
PW4000-127
PW4000-128
PW4000-129
PW4000-130
PW4000-131
PW4000-132
PW4000-133
PW4000-134
PW4000-135
PW4000-136
PW4000-137
PW4000-138
PW4000-139
PW4000-140
PW4000-141
PW4000-142
PW4000-143
PW4000-144
PW4000-145
PW4000-146
PW4000-147
PW4000-148
PW4000-149
PW4000-150
|
|
gptkbp:weight
|
approximately 8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:PW4000-113_E
gptkb:PW4000-100
gptkb:PW4000-100_I
gptkb:PW4000-100_J
gptkb:PW4000-100_R
gptkb:PW4000-113_I
gptkb:PW4000-113_J
gptkb:PW4000-100_E
|
|
gptkbp:bfsLayer
|
6
|