PT6 Prop Governor Operational Principles

  Рет қаралды 26,822

qp Aviation

qp Aviation

Күн бұрын

Пікірлер: 43
@peterbeyl5817
@peterbeyl5817 8 ай бұрын
I'm an "OLD" A/P mechanic and wished I had this animation and clear explanation back in tech school, it would have saved me a lot of OJT time. Thanks and keep up the good work.
@qpAviation-qp14
@qpAviation-qp14 8 ай бұрын
Thank you, I feel the same way. That is why I started doing this.
@sarafinanthoki5143
@sarafinanthoki5143 10 ай бұрын
This is the best Prop system explanation I have seen! 🎉 Exceptional!!
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
Thank you. I am glad it was helpful!
@luispendragon6551
@luispendragon6551 18 күн бұрын
Thank you so much for this excellent video. Starting here my first job with a PT6 as aircraft mechanic.
@qpAviation-qp14
@qpAviation-qp14 10 күн бұрын
You are welcome, congratulations on the new job!
@larsbkurin1740
@larsbkurin1740 11 ай бұрын
Very educational and nice graphics. This channel was quickly shortlisted as important.
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
Thank you!
@fabianesparza1534
@fabianesparza1534 11 ай бұрын
That’s what I was looking for so much time. I was wondering why some pilots told me that the FTG on PT6 works only when the primary and secondary TG failed and that’s didn’t make sense for me due to so many info finding in websites, however none explanation (text) really help to understand like this video. I will keep waiting for more videos like this, thanks.
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
You are very welcome. I am glad that it was helpful.
@DanielSaunders-m6d
@DanielSaunders-m6d Ай бұрын
This video is excellent. I always find in lessons on propellors that the more context that can be given showing the mounting, plane of rotation and direction of travel, help to understand the concept being explained. At 4:30 in this video, if the image is rotated clockwise 90 degrees, the concept becomes much easier to understand.
@qpAviation-qp14
@qpAviation-qp14 Ай бұрын
Thank you for the idea. I will keep that in mind for future presentations.
@Rubibi-saltwaterjim
@Rubibi-saltwaterjim 10 ай бұрын
Best video on this I've seen.
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
Thank you
@Rubibi-saltwaterjim
@Rubibi-saltwaterjim 9 ай бұрын
Adding the complexity layer by layer makes so much more sense than throwing a full system diagram up at once.
@johnbalieboardman5324
@johnbalieboardman5324 5 ай бұрын
Very good! Making this informative video must have taken a lot of work and time. Thank you!
@qpAviation-qp14
@qpAviation-qp14 5 ай бұрын
You are welcome, I hope you have found it helpful.
@nickwad
@nickwad Ай бұрын
This is the kind of material i crave. Thank you for making this, an instant subscribe, save & like from me. 👍
@demoitgroup9532
@demoitgroup9532 11 ай бұрын
Brilliant video and channel
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
Thank you very much!
@uTube486
@uTube486 9 ай бұрын
My God! Such a cool video. Thanks!
@qpAviation-qp14
@qpAviation-qp14 9 ай бұрын
Glad you liked it!
@SocInfoTv
@SocInfoTv Ай бұрын
Excellent explanation
@qpAviation-qp14
@qpAviation-qp14 Ай бұрын
thank you
@mrkc10
@mrkc10 10 ай бұрын
Exceptional video.
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
Glad you enjoyed it!
@rikokabakofficialpapua1750
@rikokabakofficialpapua1750 2 ай бұрын
I have a few questions bro. Related to Pt6 engine props 1. What happend to the props if eng oil pres drop to 15 PSI ? 2. What action should be taken if props moves to reverse in flight ? 3. What is the max prop RPM before starting a prop overspeed governor check ?
@Hahaa99
@Hahaa99 9 ай бұрын
Brilliant Video
@qpAviation-qp14
@qpAviation-qp14 9 ай бұрын
thank you
@ruphia
@ruphia 5 ай бұрын
the P T stands for Papyrus Typeface
@qpAviation-qp14
@qpAviation-qp14 5 ай бұрын
nice
@erkanorman5936
@erkanorman5936 6 ай бұрын
perfect explanation, thanx
@qpAviation-qp14
@qpAviation-qp14 6 ай бұрын
thank you
@bmzinga
@bmzinga 8 күн бұрын
What could be damaged (linkages) if reverse is selected when the propeller lever is not in the full fine (full forward position) while the engine is running? Great video by the way!
@qpAviation-qp14
@qpAviation-qp14 Күн бұрын
The linkages will not be damaged if the engine is running. Selecting reverse while the engine is NOT running can damage the linkages to the beta system because the slip block can not function properly while the slip ring is stationary. However, if you select reverse with the engine running and the props not full forward, while linkage damage will not occur, the propeller governor may not be able to maintain sufficient oil pressure to keep the propeller in the beta range. This means that one of the propellers may transition to forward thrust production while the other remains in reverse. The resulting control issues may lead to a runway departure and I suppose that if you hit something hard enough that could damage the linkages, along with everything else on the plane. For more information on how this happens look at the video around minute 19.
@Rubibi-saltwaterjim
@Rubibi-saltwaterjim 10 ай бұрын
FCU video next please!
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
FCU is on the list, hopefully I should have it out in the next couple of months.
@joshuadrake7960
@joshuadrake7960 4 ай бұрын
May want to check the theory behind aerodynamic twisting and centrifugal twisting. Happy to be educated but normally aerodynamic twisting goes to coarse and centrifugal twisting pitches to fine
@qpAviation-qp14
@qpAviation-qp14 4 ай бұрын
Thank you for your thoughtful comment. It is true that these forces could move in either direction depending on how the manufacture places the pivot attachment and CG of the propeller. The easiest way to determine the direction of these forces is to examine how the counterweight is mounted. If the counterweight is mounted toward or built into the leading edge of the airfoil, its purpose is to move the CG forward. A forward CG will act to pull the propeller to course pitch. This is why many POH and maintenance manuals talk about the counterweights moving the propeller toward feather or course pitch. Alternatively, you could evaluate the mounting point of the propeller blade to the propeller hub. Typically, propeller blades are attached forward of the center point because the increasing camber allows more room to create a sufficiently secure attachment point. If this is the case, there will be more surface area aft of the pivot point and aerodynamic twisting will move the blade toward fine pitch. Ultimately, it is the responsibility of the PIC to know the details of their unique aircraft systems. The purpose of this presentation is to present general principles that can be applied to most systems but there will always be outliers.
@АндрейЗи-т1я
@АндрейЗи-т1я 9 ай бұрын
This is the best explanation.Could you create a movie how work FCU (Fuel Control Unit) PT6? Please.
@qpAviation-qp14
@qpAviation-qp14 9 ай бұрын
Thank you, I am currently working on an FCU explanation. Watch for it in the coming months.
@filmmybro5071
@filmmybro5071 10 ай бұрын
Hellor sir, this is very big help for me becase im not good at english and having difficulties reading on MM. I hope you make another helpful vieos like this. Maybe you can make video for fuel system for pt6 engine also and oil system. Thank you so much
@qpAviation-qp14
@qpAviation-qp14 10 ай бұрын
Thank you for your comments. I plan to produce a series of videos that cover all of the systems of various aircraft including the fuel and oil systems.
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