Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-08 Thread Tuomas Kuosmanen
Ok, I made a pretty gross hack for now, and used EGT but made the
gauge show 100°F higher :-P

On the other hand, since I am making a custom panel for the senecaII
anyway, I could just make the gauges EGT for now, as they serve more
or less the same purpose in engine management anyway.

Torsten, you seem to be the maintainer for the SenecaII, would you be
interested in including the gauges in the seneca at some point? Could
make another nice fullscreen minipanel, since the small engine gauge
cluster fits nicely in a monitor with the basic sixpack..
https://gitorious.org/fgfs-ftd-mik/mik-ftd/blobs/master/OH-TWN/Panels/screenshot.jpg

If yes, how would we proceed? And if yes, should they go in
Aircraft/Instruments/ or into the SenecaII folder?

I could also do some textures for the Seneca instrument panel, if that
is a welcome idea? I have some panel photos I took a while ago that
could be useful there..

//Tuomas

On 6 December 2011 22:37, Ron Jensen w...@jentronics.com wrote:
 On Tuesday 06 December 2011 07:39:48 Torsten Dreyer wrote:
 t.

 Ron Jensen is the master of the JSBSim piston engine code. IIRC he has
 the supercharger model on his backlog, maybe TIT will be part of his
 solution..

 The current supercharger code is old, and strictly RPM based, and I don't have
 a good solution.

 The EGT calculations changed slightly in the last (2.5) release, and will
 change again (already in git) in the next release, so they may be more
 accurate to use as a base for TIT.

 As I understand it, TIT is exhaust gas temperature measured before the turbo
 and EGT is exhaust gas temperature measured after the turbo, so TIT will be
 higher than EGT. The temperature difference should be somewhat proportional
 to the boost ratio. The more boost being produced, the higher the
 back-pressure in the turbine impeller, and higher pressure implies higher
 temperature.

 Ron

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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Gary Neely
On Mon, Dec 5, 2011 at 6:08 PM, Tuomas Kuosmanen
tuomas.kuosma...@gmail.com wrote:
 Hello.

 I am working on some XML 2D gauges for our aviation club flight
 training device. We have a twin engine trainer I built over the years
 which runs on top of MS Flight Simulator, and I am making a flightgear
 setup for it to have a platform that stays alive :-)

 The SenecaII looks like the best choice for FDM, and I started to
 model some gauges in the SenecaV style (as our trainer has the two
 columns of small engine gauges on the right -panel cutout in place).
 However, SenecaV new style engine cluster has a turbine inlet
 temperature gauge (TIT).

 Does FG model this value? The property tree seems to have a tit
 property but it seems to be empty no matter if engines run or not.

 Does anyone have a clue on how to do this? Or should this be done
 somehow via nasal / other assumptions based on manifold pressure and
 environment etc..? Or should the TIT value show something?

 Best wishes,

 //Tuomas


Tuomas,

I can say for certain that YASim does not model TIT, and I believe
JSBsim doesn't either, though there seems to be a stub for TIT
modeling which may be where that property comes from. Someone please
correct me if I'm wrong about JSBsim and TIT. A developer may have
written custom code to model turbine inlet temp for a specific model,
but I'm not aware of any examples.

I'm currently working on a project that aims to handle multi-cylinder
temperature reporting and yield results good enough to at least teach
the concepts of best power/best economy and LOP operations.
Unfortunately my effort doesn't yet model turbocharged engines.

Since you're using the JSBsim-based Seneca II, you might want to
consider working with JSBsim to add the necessary modeling for TIT, if
it doesn't already exist. You might try posting on the JSBsim forum on
this topic, as someone may already be developing this.

-Gary aka Buckaroo

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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Erik Hofman
On Tue, 2011-12-06 at 00:08 +0200, Tuomas Kuosmanen wrote:
 Hello.
 
 I am working on some XML 2D gauges for our aviation club flight
 training device. We have a twin engine trainer I built over the years
 which runs on top of MS Flight Simulator, and I am making a flightgear
 setup for it to have a platform that stays alive :-)
 
 The SenecaII looks like the best choice for FDM, and I started to
 model some gauges in the SenecaV style (as our trainer has the two
 columns of small engine gauges on the right -panel cutout in place).
 However, SenecaV new style engine cluster has a turbine inlet
 temperature gauge (TIT).
 
 Does FG model this value? The property tree seems to have a tit
 property but it seems to be empty no matter if engines run or not.

For the F-16 I did tie this instrument to engines/engine[0]/egt-degf
which might not be exactly true but maybe good enough?

Erik


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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Tuomas Kuosmanen
On 6 December 2011 11:07, Gary Neely grne...@gmail.com wrote:
 I can say for certain that YASim does not model TIT, and I believe
 JSBsim doesn't either, though there seems to be a stub for TIT
 modeling which may be where that property comes from. Someone please
 correct me if I'm wrong about JSBsim and TIT. A developer may have
 written custom code to model turbine inlet temp for a specific model,
 but I'm not aware of any examples.

Yeah, maybe one could do this with nasal, some educated guesswork
etc.. As long as everything is working normally, it should follow
other engine parameters and ambient air properties, I guess.

 I'm currently working on a project that aims to handle multi-cylinder
 temperature reporting and yield results good enough to at least teach
 the concepts of best power/best economy and LOP operations.
 Unfortunately my effort doesn't yet model turbocharged engines.

That is important stuff too, would be useful for me also. Actually it
would be nice to have something like the EDM-800 gauge
(http://www.jpinstruments.com/edm_800.html) to show the values.
Unfortunately my skills with fg / nasal / programming are not very
high, as I am more of a designer, but let me know if I can help with
graphics. I am better with that stuff. :)

 Since you're using the JSBsim-based Seneca II, you might want to
 consider working with JSBsim to add the necessary modeling for TIT, if
 it doesn't already exist. You might try posting on the JSBsim forum on
 this topic, as someone may already be developing this.

Good point.

//Tuomas

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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Gary Neely
On Tue, Dec 6, 2011 at 6:13 AM, Tuomas Kuosmanen
tuomas.kuosma...@gmail.com wrote:
 On 6 December 2011 11:07, Gary Neely grne...@gmail.com wrote:
 I can say for certain that YASim does not model TIT, and I believe
 JSBsim doesn't either, though there seems to be a stub for TIT
 modeling which may be where that property comes from. Someone please
 correct me if I'm wrong about JSBsim and TIT. A developer may have
 written custom code to model turbine inlet temp for a specific model,
 but I'm not aware of any examples.

 Yeah, maybe one could do this with nasal, some educated guesswork
 etc.. As long as everything is working normally, it should follow
 other engine parameters and ambient air properties, I guess.

 I'm currently working on a project that aims to handle multi-cylinder
 temperature reporting and yield results good enough to at least teach
 the concepts of best power/best economy and LOP operations.
 Unfortunately my effort doesn't yet model turbocharged engines.

 That is important stuff too, would be useful for me also. Actually it
 would be nice to have something like the EDM-800 gauge
 (http://www.jpinstruments.com/edm_800.html) to show the values.
 Unfortunately my skills with fg / nasal / programming are not very
 high, as I am more of a designer, but let me know if I can help with
 graphics. I am better with that stuff. :)


Well, I don't seem to have any 800's handy, but...

http://www.jubjubjamboree.com/grn/flightgear/images/fgfs-screen-002.png

maybe something loosely like an 830 would do for ya?

-Gary, aka Buck

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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Jon S. Berndt
 Tuomas,
 
 I can say for certain that YASim does not model TIT, and I believe
 JSBsim doesn't either, though there seems to be a stub for TIT
 modeling which may be where that property comes from. Someone please
 correct me if I'm wrong about JSBsim and TIT. A developer may have
 written custom code to model turbine inlet temp for a specific model,
 but I'm not aware of any examples.
 
 I'm currently working on a project that aims to handle multi-cylinder
 temperature reporting and yield results good enough to at least teach
 the concepts of best power/best economy and LOP operations.
 Unfortunately my effort doesn't yet model turbocharged engines.
 
 Since you're using the JSBsim-based Seneca II, you might want to
 consider working with JSBsim to add the necessary modeling for TIT, if
 it doesn't already exist. You might try posting on the JSBsim forum on
 this topic, as someone may already be developing this.
 
 -Gary aka Buckaroo

You can implement pretty much anything you want to as a function in an
engine specification or a system in JSBSim, as long as the variables that a
function depends on are publicly available. Ask on the JSBSim list. I don't
have time to answer now, but maybe someone else can. Or, I can provide an
example and discussion later tonight - maybe.

Jon



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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Torsten Dreyer
 Yeah, maybe one could do this with nasal, some educated guesswork
 etc.. As long as everything is working normally, it should follow
 other engine parameters and ambient air properties, I guess.
Hi Tuomas,

neither yasim nor jsbsim model TIT, unfortunately. Some nasal or 
property-rules might simulate a sane behaviour.

 I'm currently working on a project that aims to handle multi-cylinder
 temperature reporting and yield results good enough to at least teach
 the concepts of best power/best economy and LOP operations.
 Unfortunately my effort doesn't yet model turbocharged engines.
 That is important stuff too, would be useful for me also. Actually it
 would be nice to have something like the EDM-800 gauge
 (http://www.jpinstruments.com/edm_800.html) to show the values.
 Unfortunately my skills with fg / nasal / programming are not very
 high, as I am more of a designer, but let me know if I can help with
 graphics. I am better with that stuff. :)
I once made a EDM700 for the ZivkoEdge540, if that helps. You can find 
the Nasal code in
FGDATA/Aircraft/ZivkoEdge/Nasal/EDM700.nas and the model in
FGDATA/Aircraft/ZivkoEdge/Models/EDM700*

 Since you're using the JSBsim-based Seneca II, you might want to
 consider working with JSBsim to add the necessary modeling for TIT, if
 it doesn't already exist. You might try posting on the JSBsim forum on
 this topic, as someone may already be developing this.
 Good point.


Ron Jensen is the master of the JSBSim piston engine code. IIRC he has 
the supercharger model on his backlog, maybe TIT will be part of his 
solution..

Torsten

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Re: [Flightgear-devel] turbine inlet temperature in the seneca (TIT)

2011-12-06 Thread Ron Jensen
On Tuesday 06 December 2011 07:39:48 Torsten Dreyer wrote:
t.

 Ron Jensen is the master of the JSBSim piston engine code. IIRC he has
 the supercharger model on his backlog, maybe TIT will be part of his
 solution..

The current supercharger code is old, and strictly RPM based, and I don't have 
a good solution.

The EGT calculations changed slightly in the last (2.5) release, and will 
change again (already in git) in the next release, so they may be more 
accurate to use as a base for TIT.

As I understand it, TIT is exhaust gas temperature measured before the turbo 
and EGT is exhaust gas temperature measured after the turbo, so TIT will be 
higher than EGT. The temperature difference should be somewhat proportional 
to the boost ratio. The more boost being produced, the higher the 
back-pressure in the turbine impeller, and higher pressure implies higher 
temperature.

Ron

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of a cloud services business. Read Now!
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