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Posted

I'm not a Black Shark expert, but it makes sense if the APU is like a turbine. When starting up a turbine you have a peak of temperature when you increase the fuel and the RPM is still low and then decrease when the air and fuel start to mix in the proper scale with the increase of RPM, so when the turbine is stable or at it's optimum RPM there should be a lower temperature than at the start. If there were a maximum at the end of the start, then something was wrong.

 

Regards.

  • Like 1

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Posted
I'm not a Black Shark expert, but it makes sense if the APU is like a turbine. When starting up a turbine you have a peak of temperature when you increase the fuel and the RPM is still low and then decrease when the air and fuel start to mix in the proper scale with the increase of RPM, so when the turbine is stable or at it's optimum RPM there should be a lower temperature than at the start. If there were a maximum at the end of the start, then something was wrong.

 

Regards.

 

It makes sense now :music_whistling:

Thanks to this a moment of enlightenment! Forgot about air/fuel mixtures and stable rpm! Thanks!

Posted

I've noticed that the EGTs drop quickly on shutdown.

 

Is this how it is on the real aircraft, or a bug?

 

Best regards,

Tango.

Posted (edited)
I've noticed that the EGTs drop quickly on shutdown.

 

Is this how it is on the real aircraft, or a bug?

 

Best regards,

Tango.

I do not work on helicopters, but every turbine engine I have work on, when you shut down you have a rapid decent in EGT temperature. It should, in most cases hover around 200 to 100 degrees Celsius after shutdown, then it will cool slowly. Is all about airflow. Keep in mind I a speaking generally, like I said, I have never work on helicopters.

 

Alpha16 or Yo-Yo will hopefully enlighten us.

Edited by mvsgas

To whom it may concern,

I am an idiot, unfortunately for the world, I have a internet connection and a fondness for beer....apologies for that.

Thank you for you patience.

 

 

Many people don't want the truth, they want constant reassurance that whatever misconception/fallacies they believe in are true..

Posted
I do not work on helicopters, but every turbine engine I have work on, when you shut down you have a rapid decent in EGT temperature. It should, in most cases hover around 200 to 100 degrees Celsius after shutdown, then it will cool slowly. Is all about airflow. Keep in mind I a speaking generally, like I said, I have never work on helicopters.

Alpha16 or Yo-Yo will hopefully enlighten us.

 

Yes, if you cut the fuel, there is no ignition.

The metal of the turbine is still very warm, so that will need to cool too

  • ED Team
Posted (edited)

The EGT gauge inertia in 1.0 was too large by mistake. Now it gets normal so you can see instant overtemperature on start up and temperature drop when duct valves close at 86% of GG_rpm.

 

In BS for indication we use only gas temperature regardless of metal case temperature. In A-10 we added a BODY (metal case) heat exchange to have temperature reading closer to real and to make engine motoring useful.

Edited by Yo-Yo

Ніщо так сильно не ранить мозок, як уламки скла від розбитих рожевих окулярів

There is nothing so hurtful for the brain as splinters of broken rose-coloured spectacles.

Ничто так сильно не ранит мозг, как осколки стекла от разбитых розовых очков (С) Me

Posted

Right, the idea is that after you shut down a turbine, the gas temperature, meaning the air going through that motor, decreases tremendously fast. Think about the temperature of the air entering the engine. When the engine is working, it goes up at first due to the compression of the compressor stages, then it jumps up when the fuel/air mixture ignites.

 

Once the engine is off, the temperature of the air going through the engine does not change much (keep in mind it still goes up, as it is still compressed some).

 

In the real world, though, the temperature of the air going through an engine that was just turned off goes up more than what I indicated above, because all of the metal parts composing the engine, but especially the combustion chamber and exhaust metals are still very hot, and heat up the air through radiation.

 

Sounds like in BS the metal temperatures are not modeled, so the EGT temperature drops dramatically. In the A-10 they are, so the EGT temperature takes longer to decrease. Makes sense?

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