Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:gas_turbine_engine
gptkb:thermodynamic_cycle |
| gptkbp:alternativeName |
constant pressure cycle
|
| gptkbp:application |
electricity generation
mechanical drive aircraft propulsion |
| gptkbp:component |
gptkb:compressor
gptkb:turbine combustion chamber |
| gptkbp:cycle |
closed cycle
open cycle |
| gptkbp:developedBy |
1872
|
| gptkbp:efficiencyDependsOn |
pressure ratio
turbine inlet temperature |
| gptkbp:fuelType |
gptkb:liquid_fuel
gaseous fuel |
| gptkbp:inventedBy |
gptkb:George_Brayton
|
| gptkbp:modernUse |
gptkb:steam_locomotive
|
| gptkbp:namedAfter |
gptkb:George_Brayton
|
| gptkbp:relatedTo |
gptkb:Diesel_cycle
gptkb:Otto_cycle gptkb:Rankine_cycle |
| gptkbp:thermodynamicProcess |
adiabatic compression
adiabatic expansion isobaric heat addition isobaric heat rejection |
| gptkbp:usedIn |
power plants
jet engines marine propulsion |
| gptkbp:workingFluid |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Brayton engine
|