EMISIVITY/ABSORBANCE – effects and possible applications..
Posted: Wed Jul 11, 2012 9:39 pm
EMISIVITY/ABSORBANCE – effects and possible applications in stirling engine design...
OK, I’m about to step way out or my comfort zone with this topic.
Is a materials emissivity a function that’s relative to 0deg kelvin (absolute zero)..(the higher the temp above zero, the greater the emission of radiation)?
Is material thermal conductivity/exchange a function of delta t (and also the relative different material conductivity and is the lower rated conductor the limiting factor)?
Is the gas the limiting factor for heat transfer due to its lower thermal conductivity compared to the other mediums (is the lower rated conductor the limiting factor) ie. In stirling engines, From the metal (say, aluminium 250 W/(m.K) Aluminium Oxide 30 W/(m.K)) to the gas (air, atmospheric 0.024 W/(m.K) (relative to air pressure and effective exposed area) (also I assume its inportant to consider that the gas/fluid has velocity and turbulance which changes its thermal conductivity/transfer rate/function (volume-time-turbulance, etc))?
What I am proposing is that it may be possible to increase thermal transfer to/from the working gas, in addition to regular conduction, by utilising radiation (emissivity /absorbance) not only directly into the gas (this might be quite low due to relative gas dencity) but also past/through the gas to other less utilised surface areas. ie. Transferring heat via radiation from the outer cylinder wall to the hot cap which then can conduct that heat to the working gas, or inversely having the cold cap absorb heat from the working gas and emit it to the outer wall where it can be dissipated away.. Thermal Energy is transferred back and forth to surface areas via radiation in their quest for relative equilibrium (with some interference by the gas relative to its density and gap)
I have also contemplated increasing hot and cold heat exchange by circulating fluids through the pistons/caps, so as to utilise their surface area, but although possible it is very problematic for multiple reasons.
With regards to aluminium, The surface areas could be black anodised (black/grey body) increasing emissivity/absorbance, while not interfering with thermal conductivity too much (as long as its not too thick, in the end all aluminium exposed to regular air becomes oxidised/anodised on the surface.) Im assuming that the thermal conductance of regular anodised aluminium is similar to that of colour anodising. Anodised aluminium Does seem to have a significantly higher Emissivity Coefficient than regular aluminium.
Aluminium Anodised 0.77
Aluminium Heavily Oxidised 0.2 - 0.31
Aluminium Commercial sheet 0.09
Aluminium Foil 0.04
Aluminium Highly Polished 0.039 - 0.057
It may also be worth considering making the surface less polished before anodising to reduce its reflective properties (and so increasing emissivity/absorbance).
I've read somewhere that anodised aluminium surface areas can tolerate up to and above about 180 deg Celsius before the different rates of expansions can cause crazing/cracking, but the anodising still is bonded to the surface. This might limit the workable temperature range, at least on the hot side.
These are just ramblings of some thoughts and questions I have, and none, some or all can be entertained, ignored or disputed as the reader so desires.
Has anyone got any thoughts, experiences or questions on this topic?
vamoose
OK, I’m about to step way out or my comfort zone with this topic.
Is a materials emissivity a function that’s relative to 0deg kelvin (absolute zero)..(the higher the temp above zero, the greater the emission of radiation)?
Is material thermal conductivity/exchange a function of delta t (and also the relative different material conductivity and is the lower rated conductor the limiting factor)?
Is the gas the limiting factor for heat transfer due to its lower thermal conductivity compared to the other mediums (is the lower rated conductor the limiting factor) ie. In stirling engines, From the metal (say, aluminium 250 W/(m.K) Aluminium Oxide 30 W/(m.K)) to the gas (air, atmospheric 0.024 W/(m.K) (relative to air pressure and effective exposed area) (also I assume its inportant to consider that the gas/fluid has velocity and turbulance which changes its thermal conductivity/transfer rate/function (volume-time-turbulance, etc))?
What I am proposing is that it may be possible to increase thermal transfer to/from the working gas, in addition to regular conduction, by utilising radiation (emissivity /absorbance) not only directly into the gas (this might be quite low due to relative gas dencity) but also past/through the gas to other less utilised surface areas. ie. Transferring heat via radiation from the outer cylinder wall to the hot cap which then can conduct that heat to the working gas, or inversely having the cold cap absorb heat from the working gas and emit it to the outer wall where it can be dissipated away.. Thermal Energy is transferred back and forth to surface areas via radiation in their quest for relative equilibrium (with some interference by the gas relative to its density and gap)
I have also contemplated increasing hot and cold heat exchange by circulating fluids through the pistons/caps, so as to utilise their surface area, but although possible it is very problematic for multiple reasons.
With regards to aluminium, The surface areas could be black anodised (black/grey body) increasing emissivity/absorbance, while not interfering with thermal conductivity too much (as long as its not too thick, in the end all aluminium exposed to regular air becomes oxidised/anodised on the surface.) Im assuming that the thermal conductance of regular anodised aluminium is similar to that of colour anodising. Anodised aluminium Does seem to have a significantly higher Emissivity Coefficient than regular aluminium.
Aluminium Anodised 0.77
Aluminium Heavily Oxidised 0.2 - 0.31
Aluminium Commercial sheet 0.09
Aluminium Foil 0.04
Aluminium Highly Polished 0.039 - 0.057
It may also be worth considering making the surface less polished before anodising to reduce its reflective properties (and so increasing emissivity/absorbance).
I've read somewhere that anodised aluminium surface areas can tolerate up to and above about 180 deg Celsius before the different rates of expansions can cause crazing/cracking, but the anodising still is bonded to the surface. This might limit the workable temperature range, at least on the hot side.
These are just ramblings of some thoughts and questions I have, and none, some or all can be entertained, ignored or disputed as the reader so desires.
Has anyone got any thoughts, experiences or questions on this topic?
vamoose