The inversion temperature of gas and its role in hot air engines
Posted: Mon Sep 30, 2024 6:26 pm
The following excerpt is from https://en.wikipedia.org/wiki/Joule%E2% ... n%20effect.
Despite the lack in chamber performance, huge heat input and almost non-existent cooling, these things offer an impressive show. The hot end easily reaches the inversion temperature of at least nitrogen. This should be a significant advantage even if it's only being partly utilized in these models.
It seems that for real gasses, the increased heat (read kinetic) energy eventually manifests itself at high enough temperatures, likely when the inertia of the gas molecules from heat energy is enough to start overcoming intermolecular attractive forces. Then perhaps more molecules are available to impart their energy at any one given time. So perhaps no actual change to internal energy levels, just an increase in readily available energy. Like R.A.M but R.A.E (random access energy) lol.
What does this mean for hot air engines? At worst this all wrong, but at best a potential increase in classical efficiency if gamed well.
For the low tech engine, it's hard to maintain a hot end that is entirely above the inversion temperature. But if only a select area of the hot end can maintain well above the inversion temperature, it should have large benefits to the propagation of heat and pressure throughout, as well as potentially more complete utilization of heat for an adiabatic process exhausting to Earth's atmosphere.
This is from https://en.wikipedia.org/wiki/Inversion_temperatureHelium and hydrogen are two gases whose Joule–Thomson inversion temperatures at a pressure of one atmosphere are very low (e.g., about 40 K, −233 °C for helium). Thus, helium and hydrogen warm when expanded at constant enthalpy at typical room temperatures. On the other hand, nitrogen and oxygen, the two most abundant gases in air, have inversion temperatures of 621 K (348 °C) and 764 K (491 °C) respectively: these gases can be cooled from room temperature by the Joule–Thomson effect.[1][11]
Besides explaining why power gains from helium and hydrogen can be so significant, this also explains model HTD engines. This thread documented the low displacer chamber effectiveness of these models. viewtopic.php?t=5638&hilit=toysThe inversion temperature in thermodynamics and cryogenics is the critical temperature below which a non-ideal gas (all gases in reality) that is expanding at constant enthalpy will experience a temperature decrease, and above which will experience a temperature increase. This temperature change is known as the Joule–Thomson effect, and is exploited in the liquefaction of gases. Inversion temperature depends on the nature of the gas.
Despite the lack in chamber performance, huge heat input and almost non-existent cooling, these things offer an impressive show. The hot end easily reaches the inversion temperature of at least nitrogen. This should be a significant advantage even if it's only being partly utilized in these models.
It seems that for real gasses, the increased heat (read kinetic) energy eventually manifests itself at high enough temperatures, likely when the inertia of the gas molecules from heat energy is enough to start overcoming intermolecular attractive forces. Then perhaps more molecules are available to impart their energy at any one given time. So perhaps no actual change to internal energy levels, just an increase in readily available energy. Like R.A.M but R.A.E (random access energy) lol.
What does this mean for hot air engines? At worst this all wrong, but at best a potential increase in classical efficiency if gamed well.
For the low tech engine, it's hard to maintain a hot end that is entirely above the inversion temperature. But if only a select area of the hot end can maintain well above the inversion temperature, it should have large benefits to the propagation of heat and pressure throughout, as well as potentially more complete utilization of heat for an adiabatic process exhausting to Earth's atmosphere.