Combustion Sustained: Starter Motor Torque/Inertia Selection

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SUMMARY

The discussion centers on the selection of starter motors for gas turbines, specifically addressing the torque and inertia required to overcome both the compressor and turbine. It is established that the starter motor primarily needs to overcome the inertia of the compressor, as it is essential for initiating airflow into the combustor. Once the combustion process begins, the turbine takes over, driving the compressor and sustaining operation. The gearbox's role in facilitating the initial spin of the shaft is also highlighted as critical for starting the engine.

PREREQUISITES
  • Understanding of gas turbine mechanics
  • Knowledge of starter motor specifications
  • Familiarity with gearbox functions in engine systems
  • Basic principles of combustion and airflow dynamics
NEXT STEPS
  • Research the specifications and torque requirements for gas turbine starter motors
  • Explore the role of gearboxes in gas turbine engine starting systems
  • Study the dynamics of airflow in gas turbines and their impact on performance
  • Learn about the transition from compressor-driven to turbine-driven operation in gas turbines
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Aerospace engineers, mechanical engineers, and anyone involved in the design and operation of gas turbine engines will benefit from this discussion.

Bonavaero
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In selecting starter motor for a gas turbine, which minimum torque or inertia is it supposed to overcome, it that of the compressor or the turbine, or both.
 
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I would assume it would be the turbine. The gearbox would play an important role in getting the engine started.
 
If you're spinning the shaft to start it, then you'll obviously need something to spin the shaft...the whole thing. In addition to that, the blades will be moving air, so that will increase the torque required.
 
I would assume once the shaft is spinning at a moderate speed and the gas is let out to the combustor, the process becomes self sustaining?
 
Oh yea. Jet engines are super easy to design. You'll be adding a high-pressure spool in a month.

edit: I should add this post may contain extreme levels of sarcasm.
 
I assume starter motor are predominantly for compressors (even though turbine is attached from a coomon shaft) ; because after combustion start turbine start to move & carryout combustion one must move compressor such that air is sucked & compressed to combustor. However once process is self-sustained its the opposite; turbine movement causes compressor to move!
 

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