|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Boeing_B-17_Flying_Fortress
gptkb:P-47_Thunderbolt
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:development
|
Wright R-1 series
|
|
gptkbp:displacement
|
1,800 cubic inches
|
|
gptkbp:engine
|
gptkb:Wright_R_series
|
|
gptkbp:engine_configuration
|
radial
horizontally opposed
|
|
gptkbp:engine_type
|
supercharged
R-1 A
R-1 B
R-1 C
R-1 D
R-1 E
R-1 F
R-1 G
R-1 H
R-1 I
R-1 J
R-1 K
R-1 L
R-1 M
R-1 N
R-1 O
R-1 P
R-1 Q
R-1 R
R-1 S
R-1 T
R-1 U
R-1 V
R-1 W
R-1 X
R-1 Y
R-1 Z
|
|
gptkbp:first_flight
|
1930s
|
|
gptkbp:fuel_capacity
|
60 inches
50 inches
40 inches
|
|
gptkbp:fuel_economy
|
0.5 pounds per horsepower per hour
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright R-1 A
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:number_of_engines
|
14-cylinder
|
|
gptkbp:operational_history
|
gptkb:World_War_II
|
|
gptkbp:power_output
|
1,000 horsepower
|
|
gptkbp:production_years
|
1930 to 1945
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:replaced_by
|
gptkb:Wright_R-2600
|
|
gptkbp:successor
|
gptkb:Wright_R-3350
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:military_aircraft
|
|
gptkbp:weight
|
1,200 pounds
|
|
gptkbp:bfsParent
|
gptkb:Wright_R-1
|
|
gptkbp:bfsLayer
|
8
|