Using The Sky As A Heat Sink
Posted: Wed Nov 12, 2014 12:06 am
If the basic requirement for the function of a Stirling engine is a heat source and a heat sink, other than the occasional rain, bat droppings and roof rats, why couldn't one use ambient temperature as the heat source and the much colder sky, via radiative cooling, as the heat sink, to move a Stirling engine to almost perpetually produce power?
Current local weather, in Taylor, Arizona: 23:30 MST, 7°C, 62% humidity, 1°C dew point, clear skies
Effective sky temperature, with a 25° compound parabolic aperture, -106.18°C
Stagnation temperature of radiator (after losses): -64°C
Carnot efficiency, with a radiator at -26°C: 11.8%
Engine efficiency, as a percentage of Carnot: 45%
Total efficiency: 5.3%
Heat radiated, net after losses, with the radiator at -26°C: ~100W m^-2
Heat radiated, net after losses, with the radiator at 7°C: ~225W m^-2
Engine output: 5.6W m^2
For background, see U.S. Patent 4624113, University of Chicago representing Argonne National Laboratory, on behalf of USDOE (assignee), 1986.
For the math, see Smith-2009
For adjustments for humidity and cloudiness see Berdahl-Martin.
The net radiated output is dependent on the radiator temperature. At the stagnation temperature the net output is zero. Surely, a Stirling engine can be tuned for a specific ΔT. Will the radiator equalize at the optimum output temperature?
Are there any other issues?
Edit: Added the radiated power for a radiator at ambient, for comparison.
Edit: The calculated losses are conservative, per Smith, using air between the radiator and the cover. I haven't done the math for a partial vacuum between the radiator and cover, per Argonne patent, but the losses should be less. I haven't found a mathematical model for that calculation yet.
Current local weather, in Taylor, Arizona: 23:30 MST, 7°C, 62% humidity, 1°C dew point, clear skies
Effective sky temperature, with a 25° compound parabolic aperture, -106.18°C
Stagnation temperature of radiator (after losses): -64°C
Carnot efficiency, with a radiator at -26°C: 11.8%
Engine efficiency, as a percentage of Carnot: 45%
Total efficiency: 5.3%
Heat radiated, net after losses, with the radiator at -26°C: ~100W m^-2
Heat radiated, net after losses, with the radiator at 7°C: ~225W m^-2
Engine output: 5.6W m^2
For background, see U.S. Patent 4624113, University of Chicago representing Argonne National Laboratory, on behalf of USDOE (assignee), 1986.
For the math, see Smith-2009
For adjustments for humidity and cloudiness see Berdahl-Martin.
The net radiated output is dependent on the radiator temperature. At the stagnation temperature the net output is zero. Surely, a Stirling engine can be tuned for a specific ΔT. Will the radiator equalize at the optimum output temperature?
Are there any other issues?
Edit: Added the radiated power for a radiator at ambient, for comparison.
Edit: The calculated losses are conservative, per Smith, using air between the radiator and the cover. I haven't done the math for a partial vacuum between the radiator and cover, per Argonne patent, but the losses should be less. I haven't found a mathematical model for that calculation yet.