Search found 503 matches
- Thu Jul 03, 2014 9:45 am
- Forum: Unconventional, Multi-Mode and Hybrid Jets
- Topic: Turbo cylinder?
- Replies: 10
- Views: 53688
Re: Turbo cylinder?
Turbos don't have a problem with "intermittent" flow to an IC engine unless the engine has less than 4 cylinders , if on a 2 cylinder engine then a large volume plenum is recommended to dampen out pulses ,I think I used a plenum of ~1.5 times engine capacity , the turbo rpm do change slightly as ...
- Fri May 02, 2014 10:39 pm
- Forum: Gas turbine forum
- Topic: Luc's Industrial Gas Turbines
- Replies: 9
- Views: 31781
Re: Luc's Industrial Gas Turbines
Hi Luc
LOL..............a simply little job
I'll think on it .
Cheers
John
LOL..............a simply little job
I'll think on it .
Cheers
John
- Thu May 01, 2014 10:59 pm
- Forum: Gas turbine forum
- Topic: Luc's Industrial Gas Turbines
- Replies: 9
- Views: 31781
Re: Luc's Industrial Gas Turbines
Hi Luc
Let me get this straight ....................you want to feed the output from the GT2560 into another GT2560 , this is even less likely to work , any freepower turbine will need to have a flow capacity twice the gas producers due to the lower gas densities and velocities achievable from the ...
Let me get this straight ....................you want to feed the output from the GT2560 into another GT2560 , this is even less likely to work , any freepower turbine will need to have a flow capacity twice the gas producers due to the lower gas densities and velocities achievable from the ...
- Wed Apr 30, 2014 11:26 pm
- Forum: Gas turbine forum
- Topic: Luc's Industrial Gas Turbines
- Replies: 9
- Views: 31781
Re: Luc's Industrial Gas Turbines
Hi Luc
Your GT4708R units aren't "working hard" , they're running rather cold so the relatively small turbine stage isn't a problem , once you get a turbine "working" with T I Ts of 900 C and above, the lowered density of the gases soon cause problems with undersized flow areas , we soon go into ...
Your GT4708R units aren't "working hard" , they're running rather cold so the relatively small turbine stage isn't a problem , once you get a turbine "working" with T I Ts of 900 C and above, the lowered density of the gases soon cause problems with undersized flow areas , we soon go into ...
- Tue Apr 29, 2014 10:25 pm
- Forum: Gas turbine forum
- Topic: Luc's Industrial Gas Turbines
- Replies: 9
- Views: 31781
Re: Luc's Industrial Gas Turbines
Hi Luc
The GT2560R turbos won't work :-(
With a 46.5mm comp inducer -1698 sq mms , we'd normally require a turbine exducer area at ~25% bigger , or 2122 sq mms or 52mm diameter , the GT2560R has a very small turbine wheel of 53mm inducer but with a 62Trim it only has an exducer diameter of ~41 ...
The GT2560R turbos won't work :-(
With a 46.5mm comp inducer -1698 sq mms , we'd normally require a turbine exducer area at ~25% bigger , or 2122 sq mms or 52mm diameter , the GT2560R has a very small turbine wheel of 53mm inducer but with a 62Trim it only has an exducer diameter of ~41 ...
- Tue Apr 29, 2014 10:14 pm
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
Nice graphics
Been in hospital for a couple of weeks so haven't been able to keep up to date on what you're up to .
Cheers
John
Nice graphics
Been in hospital for a couple of weeks so haven't been able to keep up to date on what you're up to .
Cheers
John
- Wed Apr 09, 2014 3:59 am
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
The smaller first stage gap could be better due to the finer entrainment at that point not requiring a lot of air , downstream as the jet surface starts to get "rougher" the larger clearance will have the capacity to supply air into that rougher jet boundary layer .
Have you looked at ...
The smaller first stage gap could be better due to the finer entrainment at that point not requiring a lot of air , downstream as the jet surface starts to get "rougher" the larger clearance will have the capacity to supply air into that rougher jet boundary layer .
Have you looked at ...
- Tue Apr 08, 2014 11:14 pm
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
LOL.....you're such a flatterer :-) ................heh heh , you should know I don't have an ego , flattery is wasted on me .
Yep , making sense why you need those 2 ejectors now .
Laminar flow downstream of the nozzle will keep backpressures to a minimum , is there any way you can add ...
LOL.....you're such a flatterer :-) ................heh heh , you should know I don't have an ego , flattery is wasted on me .
Yep , making sense why you need those 2 ejectors now .
Laminar flow downstream of the nozzle will keep backpressures to a minimum , is there any way you can add ...
- Mon Apr 07, 2014 11:15 pm
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
Checkout the length of jet nozzle I used on my GT6041 http://jetandturbineowners.proboards.com/thread/78/garrett-gt6041-powered-kart?page=8 , I used a central " boss" tube and straightening vanes to produce a smooth laminar flow into the jet nozzle , the gases exiting a turbo exducer fed ...
Checkout the length of jet nozzle I used on my GT6041 http://jetandturbineowners.proboards.com/thread/78/garrett-gt6041-powered-kart?page=8 , I used a central " boss" tube and straightening vanes to produce a smooth laminar flow into the jet nozzle , the gases exiting a turbo exducer fed ...
- Sun Apr 06, 2014 12:32 am
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
From doing a few numbers your 2.9" nozzle should have been putting out ~40 lbs of thrust at 80,000 rpm even with those low temps , that very efficient comp wheel works a treat
Yeh , industrial units need a big safety component , you got it pretty well spot on .
Cheers
John
From doing a few numbers your 2.9" nozzle should have been putting out ~40 lbs of thrust at 80,000 rpm even with those low temps , that very efficient comp wheel works a treat
Yeh , industrial units need a big safety component , you got it pretty well spot on .
Cheers
John
- Sat Apr 05, 2014 3:10 am
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
What sort of P2 pressures were you running the GT4708 up to ??
Heh heh , ........800 C exhaust would have been "interesting" in that industrial use .
Cheers
John
What sort of P2 pressures were you running the GT4708 up to ??
Heh heh , ........800 C exhaust would have been "interesting" in that industrial use .
Cheers
John
- Fri Apr 04, 2014 10:54 pm
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
LOL.....Theres no need for Jetspecs anymore , lotsa Youtube videos showing how to make a jet engine from a turbocharger using "stolen" info from the DIY Site .....................heh heh , its a pity most of them won't work properly though because the guys making the videos don't understand ...
LOL.....Theres no need for Jetspecs anymore , lotsa Youtube videos showing how to make a jet engine from a turbocharger using "stolen" info from the DIY Site .....................heh heh , its a pity most of them won't work properly though because the guys making the videos don't understand ...
- Fri Apr 04, 2014 12:32 am
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
If only it was so easy to give simple answers to the Rules of Thumb question . ..........................there are just so many variable to consider,........... big turbo with narrow map high pressure capability vs small turbo with wide map but limited pressure , diesel vs petrol turbo ...
If only it was so easy to give simple answers to the Rules of Thumb question . ..........................there are just so many variable to consider,........... big turbo with narrow map high pressure capability vs small turbo with wide map but limited pressure , diesel vs petrol turbo ...
- Wed Apr 02, 2014 10:55 pm
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
LOL.........I helped design Jetspecs , Jesse took my Rule of Thumb numbers from the Yahoo DIY Gas Turbines Site and put them into a workable Program , we spent months getting it "sorta right" , its not perfect but it does produce a working engine , so I'd still recommend a large combustor ...
LOL.........I helped design Jetspecs , Jesse took my Rule of Thumb numbers from the Yahoo DIY Gas Turbines Site and put them into a workable Program , we spent months getting it "sorta right" , its not perfect but it does produce a working engine , so I'd still recommend a large combustor ...
- Fri Mar 28, 2014 10:50 pm
- Forum: Gas turbine forum
- Topic: Jet Snowmobile Project/Team
- Replies: 35
- Views: 79559
Re: Jet Snowmobile Project/Team
Hi Luc
The ABB turbos are very expensive :-(
Yeh , Springer should be sued for false advertising , it really is all crap , just another poorly attempted money grab from unsuspecting guys wanting to build a turbine engine , thats why the DIY Gas Turbines Site was able to help out .
Our thrust ...
The ABB turbos are very expensive :-(
Yeh , Springer should be sued for false advertising , it really is all crap , just another poorly attempted money grab from unsuspecting guys wanting to build a turbine engine , thats why the DIY Gas Turbines Site was able to help out .
Our thrust ...