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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:Wright_Model_B
gptkb:De_Havilland_DH.4
gptkb:Boeing_40
gptkb:Curtiss_JN-4
gptkb:Martin_MB-1
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gptkbp:application
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gptkb:civil_aviation
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gptkbp:compression_ratio
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5.5:1
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gptkbp:configuration
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air-cooled
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gptkbp:cooling_system
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air-cooled
direct air cooling
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gptkbp:design
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aircraft propulsion
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gptkbp:displacement
|
1,200 cubic inches
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gptkbp:engine
|
robust construction
produced in large numbers
introduced several engineering innovations
various military and civilian aircraft
contributed to advancements in aviation technology
remains a significant part of aviation history
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gptkbp:engine_configuration
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varied by model
radial layout
single-row radial
characterized by its distinctive sound
conventional radial engine design
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gptkbp:engine_power
|
high power-to-weight ratio
improved over time
considered reliable for its time
popular among early aviators
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gptkbp:engine_type
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multiple variants developed
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gptkbp:first_flight
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gptkb:1917
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gptkbp:fuel_type
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aviation gasoline
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gptkbp:historical_significance
|
used in World War I aircraft
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|
https://www.w3.org/2000/01/rdf-schema#label
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Wright R series
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gptkbp:ignition_system
|
dual ignition
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gptkbp:influenced
|
subsequent aircraft engine designs
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gptkbp:is_tested_for
|
extensively tested during development
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gptkbp:legacy
|
paved the way for modern radial engines
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gptkbp:maintenance
|
moderate
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gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
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gptkbp:number_of_engines
|
gptkb:9
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gptkbp:operational_history
|
extensive use in early aviation
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gptkbp:power_output
|
up to 1,000 hp
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gptkbp:production_years
|
1917-1930s
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gptkbp:propeller
|
fixed-pitch propeller
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gptkbp:reliability
|
high
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gptkbp:successor
|
gptkb:Wright_R-1820
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gptkbp:type
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gptkb:radial_engine
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gptkbp:used_in
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gptkb:military_aircraft
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gptkbp:variant
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gptkb:Wright_R-1300
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gptkbp:weight
|
approximately 600 lbs
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gptkbp:bfsParent
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gptkb:Wright_R-1300
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gptkbp:bfsLayer
|
6
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