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FS2004 Override Throttle settings

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italy
I've had a little play and what I tried didn't seem to work so I'm wondering if it is possible.
If I set my throttle to 100% at ISA I get 102% n2 -- fine.
Obviously if the temperature rises then the throttle setting to obtain 102% n2 lowers.
I tried using ambient temperature to create a fake throttle setting as it were. But it always seems to be overriden by the real throttle.
So in other words I want to set the physical throttle to 100% and the actual n2% output to change according to the temperature. Can that be done?
 
Thanks Roy,
As far as I'm aware (awaiting confirmation) the throttle is not advanced to max on a hot day. Reason being that on say ISA+15 n2 would far exceed the engine limitations schedule. The RR Conway was/is not a FADEC controlled engine. It is instead controlled by Mk1 eyeball of the EO!
My guess so far if confirmed is
ISA 100% TLA
ISA+5 98% TLA
ISA+10 92% TLA
ISA+15 90% TLA

In fact at SL at ISA on a long take-off run N2 would be at 102% at rotation. The limitation is 5 minutes at 102%.
On hot days n2 can go up to 105% for which the limitation is only 20 seconds.

As you say the sim models this correctly.
 
Only if you had some code that reduced throttle and hence thrust when the EGT hit some value. Fuel flow is proportional to net thrust in the Sim. I forget if FS9 has a TSFC config entry, but in any case a fuel flow scalar of 1.0 corresponds to a TSFC of 0.5.
Roy
 
Only if you had some code that reduced throttle and hence thrust when the EGT hit some value. Fuel flow is proportional to net thrust in the Sim. I forget if FS9 has a TSFC config entry, but in any case a fuel flow scalar of 1.0 corresponds to a TSFC of 0.5.
Roy
Thanks Roy,
I'll see if I can change anything
 
The L-39 uses a fuel governor that prevents the engine from running at more than 700°C EGT.

I've implemented this by countering throttle movement if the EGT is above 695°C.

Code:
  (P:ABSOLUTE TIME, seconds) (G:Var2) - 1 >
  if{ (P:ABSOLUTE TIME, seconds) (>G:Var2)
  (A:GENERAL ENG EXHAUST GAS TEMPERATURE:1,celsius) (>G:Var3)
  }
  (A:GENERAL ENG EXHAUST GAS TEMPERATURE:1,celsius) (G:Var3) - (>L:Delta_EGT,number)
 
  (A:GENERAL ENG EXHAUST GAS TEMPERATURE:1,celsius) 695 >
  (L:Delta_EGT,number) 0 >
  and
  if{ (A:GENERAL ENG THROTTLE LEVER POSITION:1, percent) (L:Delta_EGT,number) 10 * - 163.83 * (>K:THROTTLE_SET) 1 (>G:var4) }
  els{ (A:GENERAL ENG THROTTLE LEVER POSITION:1, percent) 80 <   
  (G:var4) 1 ==
  and
  if{ 80 163.83 * (>K:THROTTLE_SET) 0 (>G:var4) } }
 
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