JSBSim Engines: Difference between revisions

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== FGTurboprop ==
== FGTurboprop ==
The turboprop engine
The turboprop engine
<h3>Configuration parameters:</h3>
=== Parameter definitions ===
<pre>
{| class="prettytable"
milthrust   [LBS]
|milthrust
idlen1     [%]
|[LBS]
maxn1       [%]
|-
betarangeend[%]
|idlen1
    if ThrottleCmd < betarangeend/100.0 then engine power=idle, propeller pitch
|[%]
    is controled by ThrottleCmd (between MINPITCH and  REVERSEPITCH).
|-
    if ThrottleCmd > betarangeend/100.0 then engine power increases up to max  
|maxn1
      reverse power reversemaxpower [%] max engine power in reverse mode
|[%]
maxpower   [HP]
|-
psfc power specific fuel consumption [pph/HP] for N1=100%
|betarangeend[%]
n1idle_max_delay [-] time constant for N1 change
| if ThrottleCmd < betarangeend/100.0 then engine power=idle, propeller pitch is controled by ThrottleCmd (between MINPITCH and  REVERSEPITCH).<br /> if ThrottleCmd &gt; betarangeend/100.0 then engine power increases up to max reverse power reversemaxpower [%] max engine power in reverse mode
maxstartenginetime [sec]
|-
    after this time the automatic starting cycle is interrupted when the engine
|maxpower
    doesn't start (0=automatic starting not present)
| [HP]
startern1   [%]
|-
    when starting starter spin up engine to this spin
|psfc
ielumaxtorque [lb.ft]
| power specific fuel consumption [pph/HP] for N1=100%
    if torque>ielumaxtorque limiters decrease the throttle
|-
    (ielu = Integrated Electronic Limiter Unit)
|n1idle_max_delay
itt_delay [-] time constant for ITT change
|[-] time constant for N1 change
    (ITT = Inter Turbine Temperature)
|-
</pre>
|maxstartenginetime [sec]
|    after this time the automatic starting cycle is interrupted when the engine doesn't start (0=automatic starting not present)
|-
|startern1
|[%]
|when starting starter spin up engine to this spin
|-
|ielumaxtorque [lb.ft]
|if torque>ielumaxtorque limiters decrease the throttle (ielu = Integrated Electronic Limiter Unit)
|-
|itt_delay
|[-]
|time constant for ITT change (ITT = Inter Turbine Temperature)
|-
|}


== FGRocket ==
== FGRocket ==
189

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