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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Voisin_III
|
|
gptkbp:aircraft_operated
|
gptkb:Nieuport_11
gptkb:Morane-Saulnier_Type_L
gptkb:Sopwith_Camel
|
|
gptkbp:compression_ratio
|
5.5:1
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|
gptkbp:cooling_system
|
air-cooled
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|
gptkbp:displacement
|
14.9 L
14900 cc
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|
gptkbp:engine
|
gptkb:aircraft
gptkb:1914
gptkb:9
gptkb:Gnome_et_Rhône
gptkb:engine
160 hp
high reliability
historically significant
high power-to-weight ratio
simple construction
four-stroke cycle
influenced future designs
rotary design
excellent performance
pioneered rotary engine technology
lightweight and powerful
detailed specifications available.
vibration issues
1300 RPM
rotary engine layout
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1914
|
|
gptkbp:fuel_capacity
|
0.9 m
68 kg
1.1 m
0.8 m
0.4 kg/hp/hr
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Gnome 9-cylinder rotary engine
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:manufacturer
|
gptkb:Gnome_et_Rhône
|
|
gptkbp:operational_history
|
used extensively in WWI
|
|
gptkbp:power_output
|
160 hp
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:setting
|
rotary
|
|
gptkbp:successor
|
gptkb:Gnome_9_N
|
|
gptkbp:torque
|
200 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
World War I aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
150 lb
|