Bronco X
Aerosoft GmbH 2012
16 17
The Garrett Turboprop Engine
The turboprop model in FSX is poorly modeled, the same is true for
torque and EGT readouts from FSX. Air-starting the engines by wind
milling is not featured by FSX, but through coding around the FSX
“engine”, we managed to correct all these deficiencies.
The turboprop available in FSX is based on the Pratt and Whitney PT6
type of engines. The PT6 is a free turbine engine. This means that the
core engine - the gas producer is a self-sustained gas turbine. The
propeller is driven through a gearbox connected to a separate turbine
placed after the gas producer. This means that the gas producer is
allowed to start and spool up independently of the propeller and it´s
turbine. Since propeller blade pitch angle is controlled via a hydraulic
governor, which uses engine oil pressure, the propeller will move into
feathered position when engine oil pressure is lost or if the condition
lever is moved fully back into the SHUTDOWN and FEATHER position.
A feathered propeller needs a huge amount of torque to overcome the
drag when spinning. Since a free turbine turboprop allows the gas
producer to spool up without turning the prop, sufficient engine oil
pressure will build up to un-feather the propeller.
The turboprop engines used on the Rockwell OV-10A Bronco are the
Garret T-76 types of engines. They are known as single shaft geared
turboprop, in which there is no separate turbine for the propeller. This
means that the propeller is directly linked to the gas producer via the
gearbox. With a feathered propeller, the engine starter will have to
both turn the gas producer as well as the propeller up to speed during
start up. As explained, a feathered propeller needs a lot of torque to
overcome the drag induced when the propeller starts spinning. This is
not desirable. To prevent this, a mechanism called Start latches are
built into the propeller. The start latches locks the propeller blades in
their beta range so with flat pitch position (between full fine and
reverse). In that position the propeller blades produce very little drag,
but also no forward thrust - or at least very little.