[AR] Re: Best Practices for Measuring Engine Temps with a Thermocouple

  • From: Eric Boyer <jeb19@xxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Mon, 21 Oct 2013 16:27:45 -0400

At 01:22 PM 10/21/2013, you wrote:
On 10/21/2013 7:20 AM, Eric Boyer wrote:
At 07:36 PM 10/18/2013, Henry Vanderbilt wrote:
Yes, I was careful to weasel-word that and not say it was outright
impossible, because I *knew* someone would take that as a challenge
<grin>

But until Omega lists W/Re TC's as a stock item, I think I'm fairly
safe in calling it thoroughly impractical.


http://www.omega.com/pptst/www26_w5w26_w3w25.html
:-)

We actually use W/Re TCs (Type C or D) fairly frequently in combustion
research. We get them either pre-made or spark-weld them ourselves
(especially the really small ones for better time/spatial resolution).
Gotta make sure they don't get even a whiff of anything oxidizing when
at high temperature, though--ever see how fast the filament of a broken
incandescent light bulb disappears?  Yeah, it's like that.

Eric

I'm having to back down from "just about impossible", through "thoroughly impractical", to just "mostly impractical". Sounds like if you pick your propellants, and accept low performance, and take a lot of care to run reliably fuel-rich throughout, you could measure chamber gas temp with off-the-shelf Omega Catalog hardware.


I'll definitely agree with "mostly impractical". Most of our applications for the W/Re TC measurements involve potting them in sort of ceramic (hafnia for the highest temps), using them to measure a subsurface temperature of something like graphite, or accepting that they're a sacrificial measurement device for a transient event (e.g., temperature-distance profile of a solid propellant flame).

Eric



Dang, ain't modern industrial resources something else?

Henry V

On 10/18/2013 4:27 PM, George Herbert wrote:
Tungsten melts at 3,400 K; it looks like peroxide motors should stay
under that, LOX/Kero at Pc of say 150-250 PSI might be under it (but not
much), LOX/alcohol should stay under it.

Rhenium is around 3,150 K, you could find propellant combinations that
would stay under that as well, so perhaps a W/Re TC?

But yes, this is edging into the "You just can't do that" trade space,
when we're having to look at the lowest temp propellants people here
might use and the highest temp metals available on the face of the
earth...



On Fri, Oct 18, 2013 at 3:08 PM, Henry Vanderbilt
<hvanderbilt@xxxxxxxxxxxxxx <mailto:hvanderbilt@xxxxxxxxxxxxxx>> wrote:

    I think the most ambitious thing we were talking about so far is
    directly TC measuring chamber wall temperature, which is merely
    really really hard.  Direct measurement of chamber gas temperature
    with a TC is pretty much impossible, since the chamber gas in any
    halfway efficient rocket motor tends to be hotter than the melting
    temperature of just about any material you can name.

    Henry


    On 10/18/2013 1:54 PM, johndom@xxxxxxxxx <mailto:johndom@xxxxxxxxx>
    wrote:

        I wonder what commercial TC can measure the inside of a firing
        chamber where
        uncooled stainless sensor protection tubing simply melts. Yes
        soldering it
        to the regenatively cooled wall is an option, but that is not
        the chamber
        gas temperature at all.

        jd

        -----Oorspronkelijk bericht-----
        Van: arocket-bounce@xxxxxxxxxxxxx
        <mailto:arocket-bounce@xxxxxxxxxxxxx>
        [mailto:arocket-bounce@__freelists.org
        <mailto:arocket-bounce@xxxxxxxxxxxxx>]
        Namens Norman Yarvin
        Verzonden: vrijdag 18 oktober 2013 21:00
        Aan: arocket@xxxxxxxxxxxxx <mailto:arocket@xxxxxxxxxxxxx>
        Onderwerp: [AR] Re: Best Practices for Measuring Engine Temps
with a
        Thermocouple

        On Fri, Oct 18, 2013 at 08:11:18AM -0400, Ed Kelleher wrote:

            A Swagelok 1/8" tube fitting, with 1/8" diameter
            stainless steel shell thermocouple (TC) will seal
            up nicely, though part of the fitting remains
            permanently attached to the TC.  You can remove
            the TC and use it on other thrust chambers, but
            it will be locked into that initial position/extension.


        One thing to remember about such setups, though, is the limits
        of the
        theory behind why it's okay to weld a thermocouple to the
chamber in
        the first place (as opposed to keeping it electrically isolated
        like a
        normal sensor).  The theory is that as long as all the hot-end
        junctions between dissimilar metals are at the same
temperature, it
        doesn't matter how many junctions there are: their effect nets
        out to
        zero.  So if you have part of the current going from
        thermocouple lead
        A directly to thermocouple lead B, and another part of it going
        through the chamber wall C, it doesn't matter how much current
        goes by
        which path, because all the junctions between A, B, and C are
all at
        about the same temperature.  Or at least they are, to a
decent first
        approximation, when you're measuring the outside of the chamber.

        If you're trying to measure the temperature of the inside of the
        chamber wall, on the other hand, you need to electrically
        isolate the
        thermocouple from the outside of the chamber wall.  Otherwise
you'll
        get some mix of inside and outside temperatures, the details
being
        dependent on exactly what currents are flowing where.  (Well,
        the heat
        equation being what it is, you'll be getting a mix anyway,
not the
        temperature of the very innermost micron of the surface.  But
this
        will make it much worse.)






--
-george william herbert
george.herbert@xxxxxxxxx <mailto:george.herbert@xxxxxxxxx>

_____________________________________________________________
Eric Boyer                                              jeb19@xxxxxxx




------------------------
Eric Boyer Assistant Director, High Pressure Combustion Lab Research Associate Department of Mechanical and Nuclear Engineering
(814) 863-2264                  Penn State University
jeb19@xxxxxxx           University Park, PA  16802


Other related posts: