I was a votech A&P instructor until I retired (different school), and I'm very pleased to see that the current cohort is interested enough in what they're learning to put this video together. It's very well done.
hi, I worked for 32 years on the S2RT34 and S2RT660 turbo-thrush in different types of mission, spreading, demostication and fire, your videos are very interesting, good luck 👍 
at the 4:02 mark, the video is showing the Fuel Nozzles which encircle the complete Engine in a series pattern. To me, it seems the Engine would have lower fuel pressure on the opposite vs. the inlet side of the fuel rail. It seems there should be several inlets to the fuel rail designed to keep the fuel pressure even around the compete fuel rail. The engine has 2 fuel glow plugs, one at the four o'clock position, and the other at the 9 o'clock position. This is done so the engine has ignited fuel evenly supplying the combustion chamber. Unless there is something I missed, or didn't see explaining how they keep the fuel pressure even in the entire fuel rail. With one inlet, and the fuel tubing being the same size, fuel pressures should be uneven. Do you have an answer, or an opinion? Thanks in advance for your time answering my questions.
The nozzles have a valve that cracks at a predetermined pressure so the fuel does not dribble out but sprays with the proper pattern instantly. This prevents damage to the hot section components from streaking fuel. Also the flow is high enough to maintain an even pressure around the full circumference of the fuel manifold.
IT look's very powerfull engine , two stage planetarny reduction box with total range from 20 000 to 2000 RPM ..... That's must generate a monster power on the propeller shaft , other question od the fuel consumption .... Heh fourteen injectors IT must make a vacum in fuel tank :D
Joshua Smith it can run on anything you throw at it even AV gas for 150 before overhaul. 55 gallons equals a hour of engine run so in a emergency you can use almost any grade of aviation fuel or jet fuel as long as the standby fuel pumps are operative and you fly below 18000 feet.
Strange video, hello, good bye and that was it. Why did they put this painted face over the girl? This vid has no structure, one can make it better, Sorry, thumb down.
I was a votech A&P instructor until I retired (different school), and I'm very pleased to see that the current cohort is interested enough in what they're learning to put this video together. It's very well done.
hi, I worked for 32 years on the S2RT34 and S2RT660 turbo-thrush in different types of mission, spreading, demostication and fire, your videos are very interesting, good luck 👍

Thank you for sharing this.. I been a caravan pilot and appreciate explanation videos
Smart young people! Thank you, it was a pleasure to watch this video.
Great video!
Nice presentations!
Great vid, thanks for posting. Is this the 135a variant?
Please, I think you should put the credits where you got part of the video in the description. PROF.FER
She is brilliant. Why hide her!?
00:01 name music please?
whats the song?
at the 4:02 mark, the video is showing the Fuel Nozzles which encircle the complete Engine in a series pattern. To me, it seems the Engine would have lower fuel pressure on the opposite vs. the inlet side of the fuel rail.
It seems there should be several inlets to the fuel rail designed to keep the fuel pressure even around the compete fuel rail.
The engine has 2 fuel glow plugs, one at the four o'clock position, and the other at the 9 o'clock position. This is done so the engine has ignited fuel evenly supplying the combustion chamber.
Unless there is something I missed, or didn't see explaining how they keep the fuel pressure even in the entire fuel rail. With one inlet, and the fuel tubing being the same size, fuel pressures should be uneven.
Do you have an answer, or an opinion?
Thanks in advance for your time answering my questions.
The nozzles have a valve that cracks at a predetermined pressure so the fuel does not dribble out but sprays with the proper pattern instantly. This prevents damage to the hot section components from streaking fuel. Also the flow is high enough to maintain an even pressure around the full circumference of the fuel manifold.
Fluid is incompressible so the pressure is the same everywhere.
That last presenter is a beauty. Her hands don't look like they've seen the inside of an engine though, ever.
Request a video of a fighter jet engine
Tankz ma"am,nix viboe ,and more ,,ixplaination,,wbout this ,,ingine torbine
West Los Angeles College..."Go West...Go Far..."
combustion increases enthalpy not internal energy
IT look's very powerfull engine , two stage planetarny reduction box with total range from 20 000 to 2000 RPM ..... That's must generate a monster power on the propeller shaft , other question od the fuel consumption .... Heh fourteen injectors IT must make a vacum in fuel tank :D
Si possible des vidéos en Français
What's mean PT6A ?
Pratt and withny
Glow plugs huh? Didn't know the Pt6 ran on diesel
Joshua Smith it can run on anything you throw at it even AV gas for 150 before overhaul. 55 gallons equals a hour of engine run so in a emergency you can use almost any grade of aviation fuel or jet fuel as long as the standby fuel pumps are operative and you fly below 18000 feet.
I think ignitors is the correct term
The PT6 has used both igniters and glow plugs.
at exactly 2:52, the woman presenters shirt appears on the front to state, "Rent Me"!
Give lubrication details.
Locations of bearings.
Cooling of bearings.
Cooling of power turbine.
Moc of power turbine and compressor.
Why?
Strange video, hello, good bye and that was it. Why did they put this painted face over the girl? This vid has no structure, one can make it better, Sorry, thumb down.
Totally agree....would do for grade 5 presentation perhaps!
Ur mom