Hot Air Engines - Thermodynamic Cycles

Thermodynamic Cycles

A hot air engine thermodynamic cycle can (ideally) be made out of 3 or more processes (typical 4). The processes can be any of these:

  • isothermal process (at constant temperature, maintained with heat added or removed from a heat source or sink)
  • isobaric process (at constant pressure)
  • isometric / isochoric process (at constant volume)
  • adiabatic process (no heat is added or removed from the working fluid)
    • isentropic process, reversible adiabatic process (no heat is added or removed from the working fluid - and the entropy is constant)
  • isenthalpic process (the enthalpy is constant)

Some examples (not all hot air cycles, as defined above) are as follows:

Cycle Process 1-2
(Compression)
Process 2-3
(Heat Addition)
Process 3-4
(Expansion)
Process 4-1
(Heat Rejection)
Notes
Power cycles normally with external combustion - or heat pump cycles:
Bell Coleman adiabatic isobaric adiabatic isobaric A reversed Brayton cycle
Carnot isentropic isothermal isentropic isothermal
Ericsson isothermal isobaric isothermal isobaric the second Ericsson cycle from 1853
Rankine adiabatic isobaric adiabatic isobaric Steam engine
Scuderi adiabatic variable pressure
and volume
adiabatic isochoric
Stirling isothermal isochoric isothermal isochoric
Stoddard adiabatic isobaric adiabatic isobaric
Power cycles normally with internal combustion:
Brayton adiabatic isobaric adiabatic isobaric Jet engines
the external combustion version of this cycle is known as first Ericsson cycle from 1833
Diesel adiabatic isobaric adiabatic isochoric
Lenoir isobaric isochoric adiabatic Pulse jets
(Note: Process 1-2 accomplishes both the heat rejection and the compression)
Otto adiabatic isochoric adiabatic isochoric Gasoline / petrol engines

Yet another example is the Vuilleumier cycle.

Read more about this topic:  Hot Air Engines

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