Volvo Project - Part 2 [ February 7th, 2011 ] By: Mark Ozimek Posted in » Ramblings

I mentioned in part 1 that I have a hard time making up my mind. This is the story of how I came to decide what turbo should get bolted up to the engine to get me to where I want to go. Be forewarned: A lot of text lies ahead. I’ll do my best to be interesting as I tell the (not so) enthralling tale.

As a point of reference in all this, for those who are unfamiliar with the Volvo powertrain, the stock shortblock seems to be good for around 600hp without sleeving, assuming the engine tune is good and heat is managed properly. Beyond that, the cylinder liners have a tendency to crack where they touch the next cylinder. The 5 speed transmission, M56H, is reliable for around that much as well, and can handle more, although gear and bearing life is rapidly declining at that point.

Originally, I was aiming for around 350whp, maybe a bit more, with a 56 trim Garrett GT2871R tucked away behind the engine. Let’s take a look at how the engine matches up with the compressor map. I made some very basic and incorrect assumptions that will get me into a ballpark estimation, such as the pressure ratio across the turbine being equal to the pressure ratio across the compressor. That will give a rough feel for where the boost threshold lies.

This is at 21psi, with a 7000rpm rev limit. Because I am looking to make this last a reasonably long time, I am choosing to keep the shaft speed around 90% of the maximum listed on the compressor chart. For the GT2871R, this is a whopping 120,000rpm! This allows for some special circumstances, like driving up mountains, to avoid overspeeding the turbo to hit the higher PR needed to get target boost in thinner air.

Anyway, onto the actual graph. As you can see, this turbo looks pretty well matched to the engine I want to build, although it is just a bit on the small side for peak power. The spool-up is based on the 0.64 A/R turbine housing flow curve that Garrett provides. Volvo uses a T3 flanged manifold, so I would get this turbo with the T3 based 0.63 A/R turbine housing, but that shouldn’t noticeably change spool.

That is just about enough airflow for about 400bhp without pushing the turbo too hard, or around 340whp. Being a FWD car, that seemed pretty reasonable figure. More would only really be usable at very illegal speeds, or on a pretty high speed track. The real nice thing about the GT2871R was that it should be making as much boost as I wanted by around 3000rpm, which is perfect for the highway, where the engine sits at 3000rpm as the car cruises at 75mph in 5th gear. Stepping up to a GT3071R or GT3076R will bring the boost up to 3500-3750rpm, which may be a bit too late for my tastes, despite the possibility of a bit more power and a cooler running engine from less exhaust restriction on a small turbine wheel.

I thought I had my turbo picked out, and had everything picked out to support it; ATP ultimate internal wastegate, the actuator, an adapter flange, the hose kit needed to get all the fluids to and away from it, the whole nine yards.

Fast forward a few months, and Garrett announces the GTX3582R, 3076R and 3071R. With a redesigned compressor wheel, they give about a 20% boost in max airflow from each turbo over the GT turbos they replace. Curiously enough, they switched from 12 split blades to 11 equal height. That will certainly affect how the compressor wheel performs. Plus they added “extended tips”, which basically just makes the compressor wheel bigger than its advertised exducer size.

Older “GT” compressor wheels look like this:

Newer GTX:

The basic sizes of the wheels remained about the same, and overall efficiency didn’t change noticeably. The general operating window got pushed to higher PR and more flow, including shifting the surge line up. By by pushing the compressor map to the right with the same turbine wheel, the compressor will be operating in a slightly less efficient spot during spool-up. I suspect this will push the boost threshold up in the RPM range a bit, as there will be more energy required from the turbine to compress the same amount of air to the same PR.

Despite previously ruling it out because of the spool time, the GTX3071R seemed like more viable alternative. It suddenly offered a much higher power potential without a significant impact on spool from before. Despite being “slow” compared to the 2871R, I reasoned that having boost by 3500-3750rpm could be doable for a DD. That still left me with about half of my total RPM range in boost, which is far from being a spiky peak hp dyno monster.

Not long after that, I found out about BorgWarner’s EFR line. There were a couple things that I really liked about what BW did with them. First, they made a really light turbine wheel, and kept the size up. This improves the turbine efficiency, and increases the amount of torque the exhaust gas should be exerting on the turbo shaft. This, along with the reduced rotating mass compared to the typical Inconel turbine wheel, should greatly improve transient response, and reduce backpressure a lot while keeping a configuration that still allows a respectable boost threshold.

In playing around with Matchbot, it seems that the EFR7064 will spool around 2750-3000rpm, and the 7670 will spool around 3250-3500rpm. As far as turbo performance goes, the 7064 stacks up pretty well against the GT2871R; similar boost threshold, potentially faster transient response, and can supply a few extra lb/min of airflow at the top end. The Garrett is better than the BW at lower pressure ratios. The most pressure I want to run on the GT2871R is about 21psi, from what we saw on the chart before. The improved performance of the 7064 at higher PR and higher flow means that I could run about 25psi and get a reasonable improvement in power without compromising the spool.

In the end though, I ended up settling on the EFR 7670. Here are the operating points found through the matchbot program, targeting a peak boost of 30psi, the points are at 2750, 3000, 3250, 3500, 6000 and 8000rpm. As you can see if you can squint hard (or right click and open the image to see the original size), it can make 30psi by 3500rpm and hold it to 8000rpm without overspinning the turbo:

I decided that having full boost by 3500rpm, going through the peak efficiency islands of the compressor wheel, and a potential for 500+whp was a good compromise, despite being more power than I should really be trying to push out of the block, and even more than I should be trying to put down to the front wheels of a street car. Logic be damned, I’m gonna do what I want! Plus, the EFR series has the distinct advantage of having a built-in recirculating BOV, and a high-flow IWG with an actuator that comes with the turbo. Those two things save enough money to make the higher cost of the EFR worthwhile.

So, one step of the project out of the way! I know what turbo I’m going with now. It’s time to make the rest of the engine support my goals. I’ll save that for part 3, since this is already a tl;dr post.

Turbochargers! - Part 3 [ June 20th, 2008 ] By:Mark Ozimek

Welcome back to the Turbochargers! series, where I get to have fun rambling on about one of the most effective ways to create a lot more power from an internal combustion engine. If you haven’t done so already, I recommend reading part one and part two and grabbing a snack before continuing on with this one.

There are several things I left open ended in part two that I would like to cover this time around. First is compressor efficiency, and other things, like how having a turbocharger affects the engine itself, will follow.

Simply put, the efficiency of a turbocharger is how much work is put into compressing the air compared to how much work would have been done in an ideal world. What is different about the ideal world? Well, things like turbulence, heat transfer between the blades and the air, the effects of sound, air’s high and low pressure points within the compressor wheel, and so forth. Nothing can ever be 100% efficient, so we just try to get as close as possible. Newer turbos are generally more efficient than older ones, thanks to improvements in modeling technology, more experience in design, improved bearing tech, and stronger materials to name a few.

The efficiency of the turbo really affects two things:

  1. Exhaust pressure right before the turbine inlet
  2. Intake air temperature after the compressor wheel

Both of these are very important things to keep as low as possible. I’ll touch on exhaust pressure (commonly referred to as back pressure) more later, since it ties in with a few other important things regarding turbo selection and engine design. The intake air temperature is pretty obvious, the lower the temperature at a given pressure, the more dense the air is, which means more air can get into the cylinders per stroke, mass-wise. This ultimately means more power, if it is not immediately obvious why, I have gone over the effects of temperature on engine performance in more detail before.

I won’t get into detail on the theory behind the calculations involved with efficiency and intake air temperature, but if you really need to know this stuff for some bizarre reason, go do some research on adiabatic compression. For the calculation, you need to know 4 different things to find the compressor outlet temperature, which I will designate as To for temperature outlet:

  1. Ti: Compressor inlet absolute temperature (ie: Kelvin or Renkin, add 293.15 or 457.69 to Celcius and Farenheit, respectively)
  2. Pi: Compressor inlet absolute pressure (ie: psia)
  3. Po: Compressor outlet gauge pressure (absolute works too, but you will have to modify the equation)
  4. n: Compressor efficiency (ranges from 1 to 0, typically around 0.7 to 0.6)

This may seem a little messy, but it is straightforward. Plug the values into the upcoming equation and you have the outlet temperature.

We can find the pressure ratio to help us simplify the final equation, and help us relate to the compressor maps, since they are given in terms of airflow and pressure ratio between the inlet and outlet pressures:

Pressure ratio (Pr) = (Po + Pi) / Pi

The equation used for finding the compressor outlet temperature:

To = ((Ti*Pr)^0.283)-Ti)/n+Ti

So if we have a car that is running with an 80ºF inlet temperature, 14.2 psia inlet pressure, 10.0 psig outlet pressure and 70% efficiency…

Pr = (10 + 14.2) / 14.2 = 1.704

To = (((80ºF + 459.67) * 1.704^0.283) - (80ºF + 459.67)) / 0.7 + (80ºF + 459.67)

Do the math and you get To to be 665.2ºR. The units are significant here, since we did all the temperatures in absolute value due to the ratios involved, the result is an absolute value. To convert, just simply subtract the number needed to convert it back to relative, 459.67 for imperial units (Fahrenheit and Rankine) and 273.15 for metric (Celsius and Kelvin)

So the outlet temperature is 206ºF, I usually round to the nearest integer, since these calculations are hardly accurate due to the complexities involved. Either way, that is pretty warm, eh? It gets much hotter with more boost and less efficient compressors. This is what we use intercoolers for.

Many intercoolers are rated up to a certain horsepower, but I find this a rather silly notion. The calculations involved with the temperature drop across the intercooler are quite complex due to the nature of the geometry of the intercooler, and I will omit them simply because we usually don’t know things like the fin height, depth, thermal resistance between the plate and fin, and so forth. It is possible to calculate the outlet temperature based on an airflow speed through the intercooler, speed of the intercooler through the air, and a lot of geometry, but it’s still an estimation at best.

So when picking an intercooler, my advice is to use as big of an intercooler as will fit in the area you’re working with, since bigger intercoolers can remove more heat and usually have a smaller pressure drop across them, which means your turbo can do less work to get the same pressure at the intake manifold. Just remember that the more volume it has, the more air must be put into it when the boost pressure increases (read: throttle response time increases)

In a similar vein, be careful of how much tubing is used to install the intercooler. The bigger the diameter, the less restriction, which is always good, but there is more volume. To avoid excess restriction, try to use as few bends in the intake path as possible, and when you need them, use a bend with as large of a radius as will fit, since that will give the least restriction to the airflow. The whole idea with the intake is to allow it to flow as freely as possible without increasing the volume, thus lag, too much. This is something that you will have to figure out on your own, or talk to other people who have done similar modifications on the same car as yours to find their opinion on how to set things up.

The same thing applies to the exhaust side of the engine too. There are two evils with exhaust restrictions, reduced power and increased exhaust gas temperatures.

I see people say things like “This engine needs a little bit of back pressure to perform properly”, and then I end up laughing a lot. The camshaft profile was designed to create optimal torque with some specified amount of back pressure. Reducing the pressure may reduce torque, but only because that is how the cam profile is set up. Change the profile some and you will end up with more power with less pressure. I’m not going to get into cam profiles yet, since it is an area that is beyond my understanding for now. With turbocharged engines, this is not a concern at all, since the turbine creates an enormous amount of back pressure.

This pressure is created by the work needed to spin the compressor wheel, and the geometry of the turbine wheel and housing. The smaller the overall turbine assembly is, the more pressure it generates at a given airflow. This is why larger turbos tend to generate more power at the same boost level as a smaller turbo. However, as we went over in part two, a larger turbo almost always spools later in the RPM band. This means that while the peak power will be higher, the total amount of energy the engine is capable of putting down to the road is lower.

Getting back to what I was talking about before with back pressure, with a turbocharged car, it is best to keep the back pressure as low as possible, since the turbine generates a substantial amount of pressure for the engine to deal with. This pressure is not constant either. Increasing the boost increases the back pressure even more, since neither the turbine wheel or the compressor wheel are 100% efficient.

In addition to this, the turbine creates energy through the difference in pressure between the inlet and outlet of the turbine wheel. Once again, due to the nature and inefficiencies of the turbine, every small increase in pressure after the turbine wheel creates a larger increase in pressure before the turbine wheel.

Why is this so bad? Well, as I pointed out before, you can make more power with less backpressure. You may have to modify the cam profile to make full use of it, but the net result is more power, which is our goal. The other is equally important. Higher exhaust pressures increase the exhaust gas temperature (EGT) with everything else being held constant. When pushing an engine close to it’s limit, a close eye needs to be kepts on the EGTs to make sure that ridiculous things like melting a piston or warping the manifold don’t happen. Plus, lower EGT’s typically mean a longer engine lifespan, since there is less thermal stress on the parts.

So how to reduce exhaust pressure? Quite simple really, use the biggest diameter exhaust pipe you can fit into the car, straight-through mufflers are a huge plus, use as few bends as possible, and possibly most importantly, the part known as the downpipe must be capable of supporting the airflow.

The downpipe is often the most restrictive part in the exhaust after the turbo (known as the turbo-back, all the parts after the turbine housing) aside from the mufflers, because the exhaust is the hottest in that part. Hot air means low density, which means a high volume for the same mass. This low density creates a high airflow velocity, and drag increases exponentially with velocity. Just like the rest of the air stream, try to ensure that the downpipe has a large diameter, smooth bends, a smooth interior surface (roughness causes more turbulence, which almost always increases the resistance to flow), and the turbo will thank you.

Well, I think that’s enough for this time around. I didn’t cover quite as much as I wanted, but the topics I did cover were gone into a lot of detail, which is good. On the plus side, I already have a few ideas for part four. I always welcome comments, questions or suggestions, so feel free to ask and I’ll do my best to help you out.

So what is everyone’s personal motto for the next month? Less restriction is better!

June 20th, 2008 | 2 Comments

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