About backpressure : intake pressure...
Originally Posted by JKav
As for the escalating exhaust backpressure with engine speed, it is indicative of one or more of the following issues:
1. compressor power requirement is escalating sharply
2. turbine is running out of flow capacity
3. turbine efficiency is plummeting
4. turbine backpressure (downstream of turbine) is escalating
JKav,
thank you very much for your contribution.
#1 above is due to one of both of the following:
a. compressor pressure ratio is going up (this can happen even if boost remains constant, or even drops)
b. compressor efficiency is plummeting (running deep in choke)
In a. above, there might be a big pressure drop in the intercooler and/or plumbing.
a. compressor pressure ratio is going up (this can happen even if boost remains constant, or even drops)
b. compressor efficiency is plummeting (running deep in choke)
In a. above, there might be a big pressure drop in the intercooler and/or plumbing.
I have a large fmic and 2,5" pipes from compressor to tb.
And/or a lot of inlet depression (upstream of the compressor inlet) due to a restrictive filter and/or undersized plumbing.
single A'pex Power Intake dry filter... could it be restrictive ?
In b., there could be a leak in the intercooler plumbing, compressor could be undersized, or just plain crappy.
2. as I told, is a T04S, with anti-surge porting
Back up to #2, this is obviously affected by any leaks upstream of the turbine (including a wastegate!).
Sorry, I can't understand this passage... or the relation with a waste gate issue...
Quantifying/assessing plumbing-related pressures/drops is aided with proper instrumentation. You can use separate gauges (one at the compressor discharge, and one right upstream of the throttle body) and subtract the readings but there's a lot of measurement uncertainty this way. A better way is to use a delta p gauge. Same goes for more accurately measuring engine delta p. For compressor inlet depression measurement you want an inches of water gauge. Using a boost/vac gauge here is like using a claw hammer to remove a splinter.
Once all the plumbing/housekeeping-type issues are identified and addressed you can more accurately determine whether backpressure issues are hardware (turbo)-related. If so, it helps a lot to have representative compressor/turbine maps, which is not as common as you might think.
Once all the plumbing/housekeeping-type issues are identified and addressed you can more accurately determine whether backpressure issues are hardware (turbo)-related. If so, it helps a lot to have representative compressor/turbine maps, which is not as common as you might think.
Originally Posted by JKav
As for the escalating exhaust backpressure with engine speed, it is indicative of one or more of the following issues. . .
According to gas law, significantly elevating temperature likewise increases the pressure of the system, which seems to explain (at least partly) the high exhaust pressure. This is why I suggested in an earlier post to re-run the pressure test after his car is retuned for the lower (23 psi) boost level that I recommended. I believe he has a retuning session scheduled, so it will be interested to denote the difference. My estimation is this will go a long way toward reducing (if not eliminating) both his high EGT problem as well as the excessive exhaust pressures.
ItalianEvo, 2.5" sounds good but it still wouldn't hurt to check because some ICs, while large, can still have high pressure drop. It's not a likely culprit, but possible. Not sure about the filter but 4" inlet is plenty.
Who made the T04S housing for your GT3071R? Or rather where did you buy the turbo.
Also are you running an aftermarket exh manifold? Check for exh leaks at the head, at the turbine inlet, and where the w/g attaches. Any leaks upstream of the turbine will make backpressure go up.
What does your exhaust look like?
Who made the T04S housing for your GT3071R? Or rather where did you buy the turbo.
Also are you running an aftermarket exh manifold? Check for exh leaks at the head, at the turbine inlet, and where the w/g attaches. Any leaks upstream of the turbine will make backpressure go up.
What does your exhaust look like?
Originally Posted by Ted B
According to gas law, significantly elevating temperature likewise increases the pressure of the system,
Originally Posted by JKav
Who made the T04S housing for your GT3071R? Or rather where did you buy the turbo.
www.pagparts.com ( USA )
Turbine is a T31 .63, turbine exhaust is 2.5" OD.
Also are you running an aftermarket exh manifold?
HKS tubular 4 in 1
Check for exh leaks at the head, at the turbine inlet, and where the w/g attaches. Any leaks upstream of the turbine will make backpressure go up.
it seems to me that I have not any leak... I'll check again...
btw I'm really not able to understand how a leak upstream of the turbine could increase the backpressure... i'm feeling an idiot...
What does your exhaust look like?
Wastegate is HKS, wg exhaust is 1.75" and it goes back into the DP 27" far from the turbine.
Thank you.
Originally Posted by ItalianEvo
btw I'm really not able to understand how a leak upstream of the turbine could increase the backpressure...
A small leak upstream of the turbine acts just like a wastegate. It bleeds off mass flow, and to maintain turbine power the turbine expansion ratio (or pressure ratio) increases. Provided it is a reasonably small leak, turbine power (and boost) will be maintained, but at a higher exh manifold pressure.
This is also why higher-flowing turbines (or a larger a/r) typically make more power at a given boost than an otherwise equivalent lower-flowing turbine. The higher-flowing turbine wastegates less flow, and is thus able to run at a lower expansion ratio, reducing exh man pressure (and improving VE and generating more power assuming the valve events are appropriate to take advantage of the improved engine delta p).
Larger leaks will bleed too much flow and render the turbine essentially useless, and the exh man pressure will fall off. And boost will too.
Accordingly, if you plot exh man pressure and boost pressure vs rpm you can see precisely where the wastegate opens (right at the inflection point in the slope of the exh man pressure curve!)... if you have enough data points of course
This is also why higher-flowing turbines (or a larger a/r) typically make more power at a given boost than an otherwise equivalent lower-flowing turbine. The higher-flowing turbine wastegates less flow, and is thus able to run at a lower expansion ratio, reducing exh man pressure (and improving VE and generating more power assuming the valve events are appropriate to take advantage of the improved engine delta p).
Larger leaks will bleed too much flow and render the turbine essentially useless, and the exh man pressure will fall off. And boost will too.
Accordingly, if you plot exh man pressure and boost pressure vs rpm you can see precisely where the wastegate opens (right at the inflection point in the slope of the exh man pressure curve!)... if you have enough data points of course
ItalianEvo, one thing to be aware of is that someone other than Garrett themselves machined the turbine and compressor housing for your turbo. The only true Garrett turbine housings for the 60mm GT30R are the Ni-Resist 711679 family. The T31 housing was recontoured by someone at some point and adapted to fit your GT3071R. That's not to say that they didn't do a good job, but there is no guarantee that appropriate wheel clearances were maintained. As a very general rule, there is less risk associated with genuine Garrett parts than non-genuine parts.
Also, the GT3071R is available with a T04B or T04E housing from Garrett. The T04S housing you have is, again, something created downstream of Garrett themselves and is subject to the same caveat as your turbine housing. Depending on who did it and how well they did their homework... kind of a crapshoot.
Also, the GT3071R is available with a T04B or T04E housing from Garrett. The T04S housing you have is, again, something created downstream of Garrett themselves and is subject to the same caveat as your turbine housing. Depending on who did it and how well they did their homework... kind of a crapshoot.
Originally Posted by JKav
A small leak upstream of the turbine acts just like a wastegate. It bleeds off mass flow, and to maintain turbine power the turbine expansion ratio (or pressure ratio) increases. Provided it is a reasonably small leak, turbine power (and boost) will be maintained, but at a higher exh manifold pressure.
Originally Posted by JKav
Larger leaks will bleed too much flow and render the turbine essentially useless, and the exh man pressure will fall off. And boost will too.
Originally Posted by JKav
Would ideal gas law apply to an open system such as this though?
Originally Posted by JKav
A small leak upstream of the turbine acts just like a wastegate. It bleeds off mass flow, and to maintain turbine power the turbine expansion ratio (or pressure ratio) increases. Provided it is a reasonably small leak, turbine power (and boost) will be maintained, but at a higher exh manifold pressure.
This is also why higher-flowing turbines (or a larger a/r) typically make more power at a given boost than an otherwise equivalent lower-flowing turbine. The higher-flowing turbine wastegates less flow, and is thus able to run at a lower expansion ratio, reducing exh man pressure (and improving VE and generating more power assuming the valve events are appropriate to take advantage of the improved engine delta p).
Larger leaks will bleed too much flow and render the turbine essentially useless, and the exh man pressure will fall off. And boost will too.
Accordingly, if you plot exh man pressure and boost pressure vs rpm you can see precisely where the wastegate opens (right at the inflection point in the slope of the exh man pressure curve!)... if you have enough data points of course
This is also why higher-flowing turbines (or a larger a/r) typically make more power at a given boost than an otherwise equivalent lower-flowing turbine. The higher-flowing turbine wastegates less flow, and is thus able to run at a lower expansion ratio, reducing exh man pressure (and improving VE and generating more power assuming the valve events are appropriate to take advantage of the improved engine delta p).
Larger leaks will bleed too much flow and render the turbine essentially useless, and the exh man pressure will fall off. And boost will too.
Accordingly, if you plot exh man pressure and boost pressure vs rpm you can see precisely where the wastegate opens (right at the inflection point in the slope of the exh man pressure curve!)... if you have enough data points of course
the larger turbine operates at a lower expansion ratio because it's larger. also you don't get anything for nothing. while it operates on less ratio it still operates on the same or more fluid mass, fluid momentum.
the improved engine delta is the reason for making more power as the increased ve of the entire system makes power.
somehow i feel i might be saying the same thing as you, since it wastes less flow then it's because it's larger and maybe uses more fluid momentum to get the same compressor power but that's really unrigorous and bothers me.
basically i don't see what wasting less flow does for anything.
Originally Posted by trinydex
basically i don't see what wasting less flow does for anything.

Another problem is choke flow. At some point the turbine cannot flow any additional volume of air, so the air must be compressed further to fit through the same volume. When that happens, backpressure and EGT skyrocket as the exhaust gas must be compressed more and more to breathe through the turbine nozzle and that compression causes heat. And, since the turbine is taking more and more energy to run as the massflow through the compressor rises, the exhaust cannot be bled off through the wastegate without losing power to the compressor wheel.
Unfortunately, sizing a hotside so that ALL of the exhaust gas passes through it generally means extremely slow spool up on a gasoline engine. You end up with a compromise: quick spool-up with low efficiency, or slow spool up with high efficiency?
The quintessential dillema of turbine sizing, only partly solved by VNT/VGT at the cost of your wallet.
-Adrian
for the first point... i don't understand why wasting comes into the picture because once you're wasting you've reached desired boost level in which case it no longer matters.... or so i was believing.
does it matter once you hit target boost?
does it matter once you hit target boost?







