@oscarrookie various fuels are used in gas turbine images depending on the environment they are used, whether aircraft, marine, power generation etc. fuels include kerosene, lpg, diesel and biofuels. somebody else might be able to help with what the engine layout and what fuel was used in the cars.
I have a few cylinder shaped large gas turbine air filters by AFF. There are two different sizes. They are brand new in the box. Ill sell and ship them CHEAP! send me message or comment if interested!
But how does it start? When the engine is off, there is no pressure from the first compressor blades. Is the expansion of the burning fuel in the combustion chamber enough to accelerate the last blades?
@EivindTube In big engines you may need a small turbine, we call it turbocharger. In other small engines, You may need a charger to startup the compressor. You can balance in between these two options, depending on the size of your engine.
Excellent! a very accurate description of what happens. Every home-made turbine engine designer needs to watch this, because most that I talk to are unaware of the importance of the combustor liner.
This animation was based on a real-world engine: the Rolls Royce Avon. Everything is quite familiar, but the Avon has 8 liners.
Thanks for posting. I will refer questions about combustors to this vid!
i can watch this all day, they can explain to me in the clearest, most simplest ways, they show me all the physics, and formulas.... seeing a plane fly is still very magical to me.
@crosseyed55 That it flies is mostly because of the shape of the wing, not just the engine. Engines produce thrust, wings are for the lift so it stays in the air. Yet it remains magical, imagine designing a plane... Fuck no!
Exhaust heat isn't always wasted, if it's a marine installation it's passed over an economizer bringing the plant to around 45/50% thermal efficiency. And fithare, i think you'll find 'british' english. Is actually just english. I'm guessing what you speak is it's inbred cousin, american.
For beginner's, The gas turbine engine consist's of Compressor, combustion chamber, turbine and exhaust, from combustion it is conversion in shape and frm turbine/ exhaust it changes to diversion in shape which helps alot to learn the fundamentals,
The gases leaving the combustor must be at a lower pressure than the incoming air (or the air wouldn't come in). There must be a principle of leverage that allows lower pressure gases to produce higher pressure air. Is the combustion chamber exhaust area larger than the area through which the high pressure air come in? I guess the total force of the burning gases = large exhaust area X low pressure. This force =(high pressure air X small area) + force to propel the aircraft
the combustion chamber uses a kind of aerodynamic valve to make the exhaust only come out in one direction. the highest amount of pressure is just after combustion, and most of this pressure is used to drive the drive the turbine..
This is incorrect. The highest pressure is found immediately after the exit guide vanes. All points aft have a lower pressure or flow would not be possible.
Well soo many points are missing in this explanation for example Exhaust cone which allows smooth air pressure and is diversion in shape so velocity decreases and pressure increases, and the point you are trying to say is we cal it Nozzle-Guide-Vane which we can find immediately after turbine after which it shoots out and there is still some small heat loss which we usually ignore,
Incoming air pressure is not equal to the pressure shooting out from Exhaust because of some heat and pressure loss during process, so it is never the same,
Very useful - thanks
sajithfaz 2 weeks ago
is this what is employed in gas turbine engine cars such as the 1964 Chrysler Turbine Cars? What fuel is used?
oscarrookie 1 month ago
@oscarrookie various fuels are used in gas turbine images depending on the environment they are used, whether aircraft, marine, power generation etc. fuels include kerosene, lpg, diesel and biofuels. somebody else might be able to help with what the engine layout and what fuel was used in the cars.
davypassane 1 month ago
many thanks..great animation & easy to follow up !!
martinilemonade 2 months ago
thanks a lot
rasoulsharif 3 months ago
Thanks pro
It is really good work
I appreciate that
omanian100 3 months ago
Good Work.. Help me as a beginner and saved a lot of time.. Thank you..:)
sajithsoma 3 months ago
o0sum video
very informative and easy to understand
Thanks
tj18668 4 months ago
thnx bro........that really helped..:-)
kentonNoel 4 months ago
Comment removed
Sonyoooo3 5 months ago
I have a few cylinder shaped large gas turbine air filters by AFF. There are two different sizes. They are brand new in the box. Ill sell and ship them CHEAP! send me message or comment if interested!
418cable418 5 months ago
nice, makes thermos much more understandable... thanks
heinetzel 6 months ago
nice one ..can u pls upload the pneumatic system if u have thanks a lot
naveen333ful 6 months ago
is the same mechanism used for electricity generation ?
hassans111 6 months ago
THANK YOU.. fricking awesome video.
Jeralddoerr 7 months ago
excellent
crudeoilsystems 7 months ago
Now lets talk about the "joys" of working on frame 5's! Yeah!
meforgodforall 7 months ago
My left ear liked that :)
Dropin16 8 months ago
But how does it start? When the engine is off, there is no pressure from the first compressor blades. Is the expansion of the burning fuel in the combustion chamber enough to accelerate the last blades?
EivindTube 9 months ago
@EivindTube In big engines you may need a small turbine, we call it turbocharger. In other small engines, You may need a charger to startup the compressor. You can balance in between these two options, depending on the size of your engine.
TFMRC 7 months ago
how efficient is a typical turbofan/turbojet engine?
Desmonddd2002 9 months ago
so thats why i have to start our gas turbines with a diesel engine, thanks man.
phatrides222000 10 months ago
Why does the audio only come out of the left speaker?
rfry 10 months ago
its really simple yet so complicated
420leadville719 10 months ago
This has been flagged as spam show
Awesome video you made
Thanks
hooda1970 1 year ago
Awesome video you made
hooda1970 1 year ago
this video is like 10 other videos put in 1
skateboy159 1 year ago 2
Thank you so much :), it helped me a lot
imcrazio 1 year ago
thanks
engineering7777 1 year ago
thank u!
xxgpGTxx 1 year ago
such a beautiful design...
spencertron88 1 year ago
Thank you so much. Excelent work. It's well explained.
Necronomiconmm 1 year ago
kkh
diandt 1 year ago
This has been flagged as spam show
thanks for the lovely information.now i understood....!
carmitha04 1 year ago
thanks for the lovely information.now i understood....!
carmitha04 1 year ago
Thanks, this helps me understand the gas turbine portion of my AME program :)
LuluAinia 1 year ago
so the compress air is running the motor ?
IIIgGeeksIII 1 year ago
Excellent! a very accurate description of what happens. Every home-made turbine engine designer needs to watch this, because most that I talk to are unaware of the importance of the combustor liner.
This animation was based on a real-world engine: the Rolls Royce Avon. Everything is quite familiar, but the Avon has 8 liners.
Thanks for posting. I will refer questions about combustors to this vid!
AgentJayZ 1 year ago
Amazing . !! thanks
mrihaveagoal 1 year ago
60%, really? is that kinda innefficient or anything like that
makmegs 1 year ago
i can watch this all day, they can explain to me in the clearest, most simplest ways, they show me all the physics, and formulas.... seeing a plane fly is still very magical to me.
crosseyed55 1 year ago
@crosseyed55 That it flies is mostly because of the shape of the wing, not just the engine. Engines produce thrust, wings are for the lift so it stays in the air. Yet it remains magical, imagine designing a plane... Fuck no!
TStyle123 1 year ago
heat energy is not wasted in turbines used on vessels
mazmut 1 year ago
could this burn methane gas ?
kienanyeo 1 year ago
Yeah it does help, Once the air is hot and expanded it will create more thrust when exiting the engine
freezinteen 1 year ago
i thought the temp diffent in the intake then out the exhaust helped in thrust? no? any1 wanna put there 2 cents on that?
shwagg15 1 year ago
isn't this more like a jet engine?
e regular gas powerplant would mix the presure air with natural gas
jhj123 2 years ago
@jhj123 it is a jet engine
CDFfilms 1 year ago
Exhaust heat isn't always wasted, if it's a marine installation it's passed over an economizer bringing the plant to around 45/50% thermal efficiency. And fithare, i think you'll find 'british' english. Is actually just english. I'm guessing what you speak is it's inbred cousin, american.
Matt1988C 2 years ago
This comment has received too many negative votes show
I hate oral british english.
fithare 2 years ago
Great vid, Love learning about turbine engines!
Xx69roadrunnerxX 2 years ago
For beginner's, The gas turbine engine consist's of Compressor, combustion chamber, turbine and exhaust, from combustion it is conversion in shape and frm turbine/ exhaust it changes to diversion in shape which helps alot to learn the fundamentals,
Cheers
Paki9190 2 years ago
thanks for posting. i accidently rated 1/5 star,ment 5/5 sorry.
blazerblast 2 years ago
tHANKS, LIKE IT.
1meGigo 2 years ago
thank you so much from an italian..!!!
domyaska 3 years ago
very nice, thanks for this video. I like it alot
Kuwaiti1990 3 years ago
very nice
sugumar1234 3 years ago
The gases leaving the combustor must be at a lower pressure than the incoming air (or the air wouldn't come in). There must be a principle of leverage that allows lower pressure gases to produce higher pressure air. Is the combustion chamber exhaust area larger than the area through which the high pressure air come in? I guess the total force of the burning gases = large exhaust area X low pressure. This force =(high pressure air X small area) + force to propel the aircraft
marcdesm 3 years ago
the combustion chamber uses a kind of aerodynamic valve to make the exhaust only come out in one direction. the highest amount of pressure is just after combustion, and most of this pressure is used to drive the drive the turbine..
matieman77 3 years ago
This is incorrect. The highest pressure is found immediately after the exit guide vanes. All points aft have a lower pressure or flow would not be possible.
craigbuckley4444 2 years ago
Well soo many points are missing in this explanation for example Exhaust cone which allows smooth air pressure and is diversion in shape so velocity decreases and pressure increases, and the point you are trying to say is we cal it Nozzle-Guide-Vane which we can find immediately after turbine after which it shoots out and there is still some small heat loss which we usually ignore,
Cheers
Paki9190 2 years ago
Incoming air pressure is not equal to the pressure shooting out from Exhaust because of some heat and pressure loss during process, so it is never the same,
Cheers
Paki9190 2 years ago
thanks alot,
it helped me as a biggener.
MPControl 3 years ago 10
You are welcome
Dave P.
davypassane 3 years ago 4
thank god for this video!!!
42states 3 years ago