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.

Combustion Engine Theory: Intro [ March 29th, 2009 ] By:Mark Ozimek

I was thinking the other day (rare, I know) it’s about time that I started up another interesting series. How about something that is at the heart and soul of almost every motorsport: The engine!

This is just the introduction to engines, I’ll cover the common terminology and give everyone a good starting point for understanding the finer design choices that I will cover later on.

Most automotive racing is powered by internal combustion engines. There are some variations within there to make things interesting. There are usually either two stroke or four stroke engines. I’m gonna focus on the latter, because two stroke engines are basically non-existent in rally. In four stroke engines, there are… wait for it… four strokes!

  • Intake: The piston is moving downward, away from Top Dead Center (TDC) with the intake valve(s) open and the exhaust valve(s) closed. This draws in fresh air/fuel mixture to burn later.
  • Compression: Intake valve closes, usually just after Bottom Dead Center (BDC), and the piston moves up to compress the air/fuel mix. Just before TDC (usually 10º-40º of crankshaft rotation), the combustion begins, either by igniting the fuel with a spark (gasoline) or injecting the fuel into the compressed air (diesel)
  • Expansion: This is the stroke where the power comes from, the burning air/fuel mix generates a lot of heat and pressure that pushes the piston down, generating torque.
  • Exhaust: Just before BDC, the exhaust valve opens up, and the piston moves back up to push all of the burnt gasses out of the engine. Once it reaches TDC, things start over again with the intake stroke.

The next choice is the type of fuel. Diesel engines run by compressing air a lot to generate very high temperatures, then inject the fuel, which combusts to generate pressure and heat that drives the engine. Spark ignition engines run a bunch of different fuels, usually gasoline, but can also include mixes of gasoline, ethanol, methanol, propane, compressed natural gas, and a few others. The air fuel mixture is ignited with a spark instead of relying on the sheer amount of heat in the diesel cycle.

There are also variations of the typical reciprocating piston engine, the most common being a rotary, or Wankel engine. The piston is replaced by a rotor with three faces housed inside of an oval-like housing that is technically known as an epitrochoid. Rotary engines have a very high power/displacement ratio because there are three power strokes for every revolution of the rotor, compared to the one power stroke every two revolutions of the crankshaft of a normal four stroke piston engine. However, sealing and lubricating the piston is a significant issue that hampers the reliability of this design

So now that this is out of the way, it’s time to get into the common terms used when describing or talking about engines. Let’s start at the macro level, things that everyone should be familiar with and move our way in.

Displacement: The amount of volume that all of the pistons displace in one stoke. This is dependent upon the number of cylinders, the bore and stroke.

Bore: The diameter of the cylinder when viewed from the top. The piston diameter is a small amount less than this, with rings to provide a good seal

Stroke: The distance the piston moves from TDC to BDC. This is dependent upon the crankshaft dimensions.

Compression Ratio: The ratio between the displaced volume (Vd) and the volume in the top of the cylinder (Vc) when the piston is at TDC. To calculate, CR = (Vd + Vc) / Vc.

Air/Fuel Ratio: Also known as AFR, or it’s reciprocal, FAR. Gasoline likes to burn within a specific range of ratios between the mass of air present and the mass of fuel present, typically between 8:1 to 20:1. the combustion can be considered the most “complete” when the AFR is stoichiometric (the wiki article does a better job explaining the chemistry than I ever could), 14.7:1 for pure gasoline, or ~14.2:1 for the 10% ethanol blend that almost all pump gas is now. This means that for every 14.7 kilograms of air that flows through the engine, the engine will try to supply 1 kg of gasoline. Ratios that are lower than stoich are called “rich”, and higher is “lean”. Given a constant set of parameters and optimized ignition advance, AFRs around 12.5-13 for gasoline give the most torque, because the fuel burns the fastest then.

Ignition Advance: Measured in the number of crankshaft degrees before the piston reaches TDC. Typically spark will be tuned to create maximum cylinder pressure around 14º after TDC. More advance is needed when the engine spins faster, because the burn speed of gasoline does not increase with the engine speed. However, the burn speed does increase with air density, and with AFR, with a maximum burn speed for gasoline being around 12.5-13. As such, timing is typically less advanced with more open throttle or higher boost pressure, but more advanced at higher engine speeds. Many design factors play a role in optimal ignition timing.

Volumetric Efficiency: This is essentially a measure of the amount of air that goes into a cylinder compared to how much a piston displaces. Since air is compressible, meaning the density changes with pressure, it makes more sense to think of it in terms of mass. A volumetric efficiency of 100% would imply that the mass of air that is in a piston is the same as the mass of whatever the displacement would weigh in the surrounding air. So taking the 100% efficiency example further, if it was a 4 cylinder 2.0L engine running at 100% efficiency at STP, the mass of air inside one cylinder would be equal to the density of air (1.184 kg/m³) multiplied by the volume (0.5L), the result is 0.592 grams of air. Doesn’t sound like a lot, but air is pretty light, and when you’re turning the engine at 6000 rpm, the engine is moving about 7 kg/min of air.

Mean Piston Speed: The average speed of the piston as it moves through a cycle. This is dependent upon the RPM (referred to as N in calculations) that the engine is running at and the stroke. To calculate, Sp = 2 * N * Stroke. Due to material strength and fatigue limitations, it is uncommon to see the mean piston speed exceed 25m/s or so, except in extremely high performance racing engines, like F1.

Brake Mean Effective Pressure: Commonly BMEP (or MEP when not measured at peak torque or power), this a way to measure how effective an engine is at making power in relation to it’s displacement and rpm. As a general rule of thumb, the more power you make per amount of displacement and the less rotational speed at that power level, the higher the BMEP is. Alternately, for those of you who know how torque, power and rpm relate to each other, the peak BMEP of the engine is at the peak torque of the engine. To calculate MEP, you need to know either the power and RPM, or torque, displacement, and number of strokes (2 or 4)

Calculating with power and rpm:

MEP = (P * Nr * C) / (Vd * N)

P is power, in HP or kW
Nr is the number of revolutions per power stroke, 1 for 2-stroke, or 2 for 4-stroke
C is a constant, use 396,000 for imperial (hp & ft-lbs) or 10³ for SI (kW & N-m)
Vd is displacement, cubic inches for imperial or liters for SI (61.02 CI per L if you need to convert)
N is the engine speed in RPM

Or with torque:

MEP = (T * C) / (Vd)

T is torque, ft-lbs or N-M
C is a constant, 75.4 for imperial, 6.28 for SI

Well, that’s it for the intro. I’m sure some of you have specific things that you would like me to go into detail on in this series, feel free to ask, and I’ll try my best to cover it!

March 29th, 2009 | 2 Comments

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