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#131
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T-56's don't have TAT probes Jackass
On Fri, 16 Jan 2004 18:55:11 -0800, "Tarver Engineering" wrote: "JL Grasso" wrote in message ... On Fri, 16 Jan 2004 17:57:34 -0800, "Tarver Engineering" wrote: "Bertie the Bunyip" wrote in message .. . "Tarver Engineering" wrote in : "Phil Miller" wrote in message news ![]() Hey Splappy, Do you remember this series of pronouncements; From: "Tarver Engineering" Newsgroups: rec.aviation.military Subject: Do Hercules military aircraft use the same fuel as civilian aircraft? Date: Fri, 8 Nov 2002 19:19:37 -0800 snip wrote in message Not really. On the T56 engine TIT = (T)urbine (I)nlet (T)empreture. Yes really, on every jet engine TIT is Total Inlet Temperature. Yep. Nope. Yep, the individually wired theromcouples are sent to a Totalizer, when they are not wired in series. That is why the datum is a total. One has to wonder if the trolls of ram will ever catch a clue. The irony of it all. ![]() Total Air Temperature (TAT)is the maximum temperature attainable by air when brought to rest adiabatically. Total Air Temperature is the total of several probes at the inlet of the engine. (ie T1) The word "Total", when used to describe the type of temperature reading that a probe is reporting, has nothing to do with totalizers or wiring connections. The term "total" has to do with the use of multiple probes. Wiring thermocoulpes in seris gives a Total temperature. Where the probes are wired in parallel, a Totalizer is used downstream to add the thermocouple outputs together. Why do you post, Grasso, when it is clear that there is no subject WRT aircraft that you know? Perhaps you would do better sticking to your parts catalogs and forget about pretending you understand anything about aircraft. Otherwise, you are likely to become a hazard to aviation. |
#132
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That is the most ridiculous statement I've heard from you yet, Tarver,
what are you smoking??? You are in my book as being seriously demented now, whats wrong with you? Where do you come up with that kind of off the wall crap??? I seriously hope our Govt doesn't do business with you, or you are not on a Govt project, I'd drop a dime on you for being a Jackass. On Sat, 17 Jan 2004 08:23:33 -0800, "Tarver Engineering" wrote: "running with scissors" wrote in message om... "Tarver Engineering" wrote in message ... "Phil Miller" wrote in message ... snip I ask because I came across an interesting paragraph in the T56-A-15 service manual yesterday. Went like this... Same for any MM, the data does not need to be accurate. grief ! so if that were the case, then a generic manual would suffice. Nope, the manual has to be close enough to do the work. Errors in MMs are commomplace and not any real hazard. Just as B-52 operators don't really need to know how their wing works, mechanics don't really need to know how a system works. |
#133
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![]() "Scet" wrote in message ... "Jim Yanik" wrote in message .. . "John R Weiss" wrote in news:Sp%Nb.73504$nt4.98595@attbi_s51: "Phil Miller" wrote... Yes really, on every jet engine TIT is Total Inlet Temperature. Yep. I ask because I came across an interesting paragraph in the T56-A-15 service manual yesterday. Went like this... ...measures the turbine inlet temperature by means of thermocouples...Eighteen thermocouple assemblies are mounted in the turbine inlet casing of each engine...One thermocouple of each assembly is connected to the turbine inlet temperature indicating system, and...one...is connected to the electronic datum control system. The 18 indicating system thermocouples are connected in parallel [!!] by the indicator turbine thermocouple harness assembly, I'm surprised you ever doubted the truth on this one! So, let's revise. That's going a bit too far... Nobody can revise the Tarver Chronicles! :-) bimetallic thermocouples generate millivolt signals,and paralleling them would not work.Standard practice is to series-connect them,and compare to a reference junction.Do these assemblies include signal processing to convert the mV signal to a digital form,which could then be sent on a parallel bus? -- Jim Yanik jyanik-at-kua.net Sorry Jim, but it does work. Scet Don't hide behind Google John, we all know you are wrong and know nothing about the subject. If you want to reply using Google hoping that most guys won't read your **** that's fine but it only makes you look stupider than you are( If that's possible) post your answers here for everones benefit, at the very least it is worth a laugh. Scet |
#134
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![]() "fudog50" wrote in message ... Tarver, you were "totally" wrong in your original response dated Nov 8th, 2002 about T-56's and TIT. Nope, but thanks for playing. Did you figure out that sailors call those things you think are "ships", "boats" yet? I mean, Funny dude, if you can't figure out what is going on right where you are, how can we believe anything you write about what is farther away? "Turbine Inlet Temperature". Turbine inlet temperature is a linear function, my idiot. |
#135
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![]() "B2431" wrote in message ... From: "Tarver Engineering" Date: 1/21/2004 8:29 PM Central Standard Time Message-id: "Scet" wrote in message ... No it isn't John and you know it from the discussion we had on this subject last time....you were wrong then and you are wrong now. I am still correct, the only difference is that I proved it in this thread. You are making a fool of yourself, Scat. Tarver, at the risk of a barrage of filth from you, can you provide a web site other than yours that shows TIT or EGT thermocouples in series? You are too confused for me to even respond, Dan. |
#137
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"Scet" wrote in
: Dan, we went through this early last year I think it was and Tarver was shown to be wrong as per normal. On T56 engines the thermocouples are connected in parallel and pick up TIT, the signal is then averaged. They are averaged due to the non-uniform temperatures that occur at the turbine inlet due to the short time of spraying fuel from the nozzle, to fuel ignition, to introducing the hot gasses at high velocity to the turbine inlet. The hot gases are not completely mixed and so there are some stratifications of hotter and cooler areas at the turbine inlet. The temperature averaging function of the parallel thermocouple circuits compensates for these non-uniform temperatures. Scet I fail to see how the separate thermocouples outputs will be "averaged",because any individual TC cannot rise in output,as all the others parallelled will prevent any rise in voltage.Or current would flow from a higher V to a lower one,just as if you wired batteries of different voltages together,you end up with circulating currents until all cells are of equal voltage.. Seems to me that parallelling them is only for the possibility of an individual thermocouple to be burned out or open. -- Jim Yanik jyanik-at-kua.net |
#138
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![]() "fudog50" wrote in message ... That is the most ridiculous statement I've heard from you yet, Tarver, what are you smoking??? You are in my book as being seriously demented now, whats wrong with you? Where do you come up with that kind of off the wall crap??? I seriously hope our Govt doesn't do business with you, or you are not on a Govt project, I'd drop a dime on you for being a Jackass. The B-52 wing aerodynamics were discussed here at ram and then in about a dozen .sci threads. The USAF teaches that small amounts of spoiler acutally increase lift, but that is incorrect. Buffdrver, a real B-52 pilot has already written to USAF about their error. USAF, of course, doesn't need their pilots to understand how the wing actually works. Did you figure out where the "boats" are yet, dog? |
#139
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![]() "Jim Yanik" wrote in message .. . "Scet" wrote in : Dan, we went through this early last year I think it was and Tarver was shown to be wrong as per normal. On T56 engines the thermocouples are connected in parallel and pick up TIT, the signal is then averaged. They are averaged due to the non-uniform temperatures that occur at the turbine inlet due to the short time of spraying fuel from the nozzle, to fuel ignition, to introducing the hot gasses at high velocity to the turbine inlet. The hot gases are not completely mixed and so there are some stratifications of hotter and cooler areas at the turbine inlet. The temperature averaging function of the parallel thermocouple circuits compensates for these non-uniform temperatures. I fail to see how the separate thermocouples outputs will be "averaged",because any individual TC cannot rise in output,as all the others parallelled will prevent any rise in voltage.Or current would flow from a higher V to a lower one,just as if you wired batteries of different voltages together,you end up with circulating currents until all cells are of equal voltage.. Also, Jim, the "total" is what you want for such small signals. Averaging would only reduce: accuracy, reliability simplicity. Scet is just being ignorant. |
#140
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![]() "Jim Yanik" wrote in message .. . Well,then it violates basic physics.If you have two voltage sources of slightly different voltages,currents DO flow between them.That's a basic principle. And bimetal TCs are simply millivolt voltage sources. I always wanted to take one of the series connection wiring on out J-75's TIT ring, but I was afraid I would get an Article 15. |
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