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Inside Pratt & Whitney PT6A-67B engine, two turbine systems spin in opposite directions at tens of thousands of rpm, yet they aren't mechanically connected at all. The gas generator spool reaches roughly 37,500 rpm. Its hot gas drives an independent power turbine at nearly 30,000 rpm, producing up to... show more
25,903 次观看 • 1 个月前 •via X (Twitter)
12 条评论

Indistinguishable from art.

This is an interesting bit

More quiet than turboshafts. It is also more resistant to icing / ice ingestion. Much easier to spin up at start (less mass) without a coupled prop shaft. the KA B100 was produced with TPE 331's (labor strike) and it was never as successful as the PT6 despite being more powerful and fuel efficient. The PT6 was more maintainable and tolerant of less than perfect engine management.

King Air 350's rock.

And yet every brain cell of mine screams: this thing can’t work/is badly engineered: *compressor aft, turbines fore: so compressor doesn’t benefit from forward motion plane to thrust air in *power turbines are driven by exhaust gas that has already given away energy to compressor

It's like two torque converters from automatic transmissions put together...

Wouw

fascinating engineering challenge

That air flow ducting kills me every time.

amazing technology

@grok En qué se usa esa turbina y cuánta es la vida útil de los motores de los aviones f22 y f16 y qué pieza se remplaza más en ellos, cómo son los rodamientos que soporten esas temperaturas sin lubricación?

The hot section is in front of the engine so easy to remove or be worked on because it needs to be serviced more often than the air intake/compressor section, I believe.
