Statements (61)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:Curtiss_JN-4_Jenny
gptkb:Wright_Model_B |
| gptkbp:application |
military and civilian aviation
|
| gptkbp:compression_ratio |
6:1
|
| gptkbp:configuration |
single-row
|
| gptkbp:cooling_system |
air-cooled
uses air cooling |
| gptkbp:design_features |
simple design
|
| gptkbp:displacement |
600 cubic inches
|
| gptkbp:engine |
incorporated several innovations
influenced future engine designs widely used in the 1920s and 1930s used in various military applications used in training aircraft features advanced technology for its time developed during the golden age of aviation part of Wright's legacy mass-produced during its time used in various civilian aircraft. |
| gptkbp:engine_configuration |
designed for ease of use
horizontally opposed detailed specifications available front-mounted inline layout specifications published in aviation manuals characterized by robustness noted for its durability subject to modifications over time |
| gptkbp:engine_power |
reliable performance
known for reliability operates at high RPMs suitable for light aircraft performance metrics documented in tests |
| gptkbp:engine_type |
piston engine
multiple variants produced several variants adapted for different uses |
| gptkbp:first_flight |
gptkb:1929
|
| gptkbp:fuel_economy |
approximately 30 gallons per hour
|
| gptkbp:fuel_type |
aviation gasoline
|
| gptkbp:historical_significance |
important in early aviation history
|
| https://www.w3.org/2000/01/rdf-schema#label |
Wright J-6
|
| gptkbp:ignition_system |
dual ignition
|
| gptkbp:is_tested_for |
extensively tested
tested in various facilities |
| gptkbp:maintenance |
requires regular maintenance
|
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:number_of_engines |
9 cylinders
|
| gptkbp:operational_history |
widely used in the 1930s
|
| gptkbp:power_output |
300 horsepower
|
| gptkbp:predecessor |
gptkb:Wright_J-5
|
| gptkbp:production_years |
1929 to 1935
|
| gptkbp:propeller |
fixed-pitch propeller
|
| gptkbp:propulsion |
produces significant thrust
|
| gptkbp:successor |
Wright J-6-7
|
| gptkbp:torque |
produces significant torque
|
| gptkbp:type |
gptkb:radial_engine
|
| gptkbp:used_in |
various aircraft
|
| gptkbp:weight |
approximately 400 pounds
|
| gptkbp:bfsParent |
gptkb:Boeing_Model_80
|
| gptkbp:bfsLayer |
7
|