Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:Douglas_DC-3
gptkb:Beechcraft_Staggerwing gptkb:Wright_Model_700 |
| gptkbp:application |
gptkb:civil_aviation
gptkb:military_aircraft |
| gptkbp:compression_ratio |
6:1
|
| gptkbp:configuration |
radial
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
760 cubic inches
|
| gptkbp:engine |
gptkb:Wright_R-series
high durability smooth operation easy installation improved fuel efficiency low noise levels easy maintenance low operational costs high torque output long service life good power-to-weight ratio versatile applications robust construction reduced vibration effective cooling system low maintenance requirements proven technology good acceleration wide availability of parts good altitude performance adaptable to various airframes used in vintage aircraft restoration high operational reliability good thermal efficiency high power output for size suitable for aerobatic aircraft |
| gptkbp:engine_configuration |
9-cylinder
horizontally opposed aircraft propulsion |
| gptkbp:engine_power |
high reliability
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Wright R-760
|
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:notable_users |
gptkb:Pan_American_Airways
gptkb:Trans_World_Airlines gptkb:United_States_Air_Force |
| gptkbp:number_of_engines |
gptkb:9
|
| gptkbp:original_run |
gptkb:1929
|
| gptkbp:power_output |
300 horsepower
|
| gptkbp:propeller |
variable pitch
|
| gptkbp:successor |
gptkb:Wright_R-975
|
| gptkbp:type |
gptkb:radial_engine
|
| gptkbp:weight |
approximately 400 pounds
|
| gptkbp:bfsParent |
gptkb:Boeing_Stearman_Model_75
|
| gptkbp:bfsLayer |
5
|