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George Bailey Brayton (1830–1892) was an American mechanical engineer and inventor. He was noted for introducing the constant pressure engine that is the basis for the gas turbine , and which is now referred to as the Brayton cycle .
The Brayton cycle, also known as the Joule cycle, is a thermodynamic cycle that describes the operation of certain heat engines that have air or some other gas as their working fluid. It is characterized by isentropic compression and expansion, and isobaric heat addition and rejection, though practical engines have adiabatic rather than ...
Differs from Otto cycle in that V 1 < V 4. Brayton: adiabatic: isobaric: adiabatic: isobaric Ramjets, turbojets, -props, and -shafts. Originally developed for use in reciprocating engines. The external combustion version of this cycle is known as the first Ericsson cycle from 1833. Diesel: adiabatic: isobaric: adiabatic: isochoric Diesel engine ...
English: T-S diagram for a Brayton Cycle. Solid line shows an ideal cycle, dotted line a real one. Solid line shows an ideal cycle, dotted line a real one. 1) compressor inlet 2) compressor outlet 3) turbine inlet 4) turbine outlet C) compressor B) combustion chamber
The most common refrigeration cycle is the vapor compression cycle, which models systems using refrigerants that change phase. The absorption refrigeration cycle is an alternative that absorbs the refrigerant in a liquid solution rather than evaporating it. Gas refrigeration cycles include the reversed Brayton cycle and the Hampson–Linde cycle.
The Vector templates below can be used to derive images with, for example, Inkscape. This is the method with the greatest potential. This is the method with the greatest potential. See Human body diagrams/Inkscape tutorial for a basic description in how to do this.
English: Brayton-Joule cycle diagram (continuous line for ideal cycle, dotted line for real cycle) of a jet aircraft engine with afterburner with engine stations. 1 Inlet 2 Air Intake/Compressor 3 Compressor/Combustion Chamber 4 Combustion Chamber/Turbine 5 Turbine/Afterburner 6 Afterburner/Nozzle