## Heat Transfer through lenses

## Heat Transfer through lenses

(OP)

Hi to everybody.

I am in a bit of a problem for calculating the various convective coefficients for the heat transfer through two lenses made of sapphire.

I have to create a window that will let a thermal camera see into the medium pressure stage (and later i will do the same study for the high pressure stage) of a Steam Turbine. The window will be created in a sort of hollow point of the outer casing, so I can conclude, or approximate, that the steam that pass there is immobile. So near the first lens the velocity of the steam is zero.

Now, i attach an image for better undestanding.

Data is:

lenses made of Sapphire (Al2O3) of Diameter 64mm.

The lenses are clamped, so the usable diameter is 54mm

T1=271,9 °C p1=5,752 bara

x1=12mm

cavity filled with air at p=pamb, later filled with nitrogen at p=pamb

x2=8mm

T2=20°C, p2=pamb

Now, as first approximation(after the immobile steam near the first lens) I can resolve my problem as a 1 Dimension Steady State (in the end I will use the thermal camera always in steady state).

How do i calculate the three convective coefficients?

Thanks in advance

I am in a bit of a problem for calculating the various convective coefficients for the heat transfer through two lenses made of sapphire.

I have to create a window that will let a thermal camera see into the medium pressure stage (and later i will do the same study for the high pressure stage) of a Steam Turbine. The window will be created in a sort of hollow point of the outer casing, so I can conclude, or approximate, that the steam that pass there is immobile. So near the first lens the velocity of the steam is zero.

Now, i attach an image for better undestanding.

Data is:

lenses made of Sapphire (Al2O3) of Diameter 64mm.

The lenses are clamped, so the usable diameter is 54mm

T1=271,9 °C p1=5,752 bara

x1=12mm

cavity filled with air at p=pamb, later filled with nitrogen at p=pamb

x2=8mm

T2=20°C, p2=pamb

Now, as first approximation(after the immobile steam near the first lens) I can resolve my problem as a 1 Dimension Steady State (in the end I will use the thermal camera always in steady state).

How do i calculate the three convective coefficients?

Thanks in advance

## RE: Heat Transfer through lenses

If you are trying to calculate the heat loss, assuming your turbine body is metal, I would expect the lens and the temperature of the nitrogen in the gap to basically be the same temperature as the housing wall at that point. So outer lens temp is same as outer wall, inner lens temp same as inner wall, etc.. Since there is nothing circulating the nitrogen in the gap conduction will win out.

If you are trying to calculate an offset for you thermal camera you will need to look at the transmission % of the sapphire over the wavelengths that your camera is sensitive to. Any coatings could have a very big effect too. For example, if we assume you are using a MWIR camera and sapphire transmits roughly 80% between 3-5um wavelengths you would be looking at only 64% of those wavelengths getting through your two lenses. Of course, if you are trying to measure absolute temperatures of components using a thermal camera the emissivity of the materials will have an even larger effect on the temperature values you read.

## RE: Heat Transfer through lenses

x1 and x2 are thicknesses? What is the gap spacing?

What exactly are you trying to see? Infrared sensors are not particularly good at seeing through steam.

TTFN (ta ta for now)

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## RE: Heat Transfer through lenses

First of all,

@IRstuff:

I am sorry, but i didn't mean i thought there would have been only convection, it would be nonsense.

x1 and x2 are the thickness of the two lenses. The thermal conductivity of sapphire is 40 W/mK at 27°C and 4 W/mK at 1227°C(it is not linear, but I still have to find a table containing various Thermal conductivity coefficients at various temperatures).

I am triyng to see the metal surface temperature of the rotor that is visible from this window.

@hendersc:

I still don't have the cavity thickness between the 2 lenses because I will have to implement it. I can prematurely say that it is 10mm.

Speaking for the gap made of air, I was not sure that I could say that it was only conductive tranfer in the gap, So I went and searched the Italian normes(I'm from Italy) to find the cavity resistance. I found some normes for buildings(so for thicker gaps, at least 5mm) saying that I can consider it only conductive transfer IF the cavity gap is 10% or less than one of the two walls surrounding it, so the gap should be less than 0.8mm. Unfortunately, even if I wanted to use it like that, there was only a Resistance for a gap of 5mm.

I already did some preliminar calculation with H1=510 W/m2K (really high,it was from a study on a combustor, so it is useless), H2=10W/m2K, Hi=15 W/m2K (the internal one was totally random, but I had to start from somewhere) and it turns out that the second lens was at 126°C, and the first at 269°C.

I will use all of this to calculate the thermal and mechanical stresses of the 2 lenses, but to try and be as precise as possible I have to find a way to calculate the convective coefficients (and find a table for the thermal conductivity of sapphire, but that should not be a problem),

How do I calculate the convective coefficents of the various stages?

## RE: Heat Transfer through lenses

At the very least, the outer edges of your sapphire windows that are in contact(in some way) with the metal housing will be the same temperature as the metal housing. You could look at this from a worst case perspective instead of trying to get exact values. The worst case (I assume) would be for the sapphire to be at the higher housing temperature.

It sounds like you are trying to neglect any heat transfer through the housing to the lens or through the housing to the air gaps which I think will give you much lower temperature values. I would suggest throwing this into a CFD software so you don't need to neglect one form or another of heat transfer.

## RE: Heat Transfer through lenses

> Can the imager see through the window system? which is a different question than your heat transfer question

The answer to that question depends on the transmission of the image photons through the steam. Ignoring the steam for the moment, if the transmission of the two "lenses" which I assume are actually flat panes of sapphire, is tolerably high, even 25% transmission might be sufficient, then you can "see" through the window.

The steam is a bigger problem, since it not only obscures by absorbing photons, it's the hottest material in the system and emits a bunch of photons on its own that can mask the contrast of features in the rotors that you are trying to image.

TTFN (ta ta for now)

I can do absolutely anything. I'm an expert! https://www.youtube.com/watch?v=BKorP55Aqvg

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## RE: Heat Transfer through lenses

How do i calculate them?

I found out that the property of steam at the exit(so near that window)

flow=13,45 kg/sec

entalphy=3004,3 kJ/kg

## RE: Heat Transfer through lenses

And then you need to know their velocities relative to the surfaces. If your lenses are very small (which I assume they are) then the convection between them will be very minimal, because of extremely small velocities.

What you really need is the velocity of the steam against the innermost lens surface- your assumption that the velocity on the inside of the lens is zero is almost certainly incorrect.

## RE: Heat Transfer through lenses

What surface temperature is the housing at? To the first order, the outer window temperature will be that of the housing around it

TTFN (ta ta for now)

I can do absolutely anything. I'm an expert! https://www.youtube.com/watch?v=BKorP55Aqvg

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## RE: Heat Transfer through lenses

## RE: Heat Transfer through lenses

TTFN (ta ta for now)

I can do absolutely anything. I'm an expert! https://www.youtube.com/watch?v=BKorP55Aqvg