bbodie52 wrote:So the turbo used by Olds in the 215 ci engine was significantly SMALLER than the Corvair turbo used on the 145 ci, and later 164 ci engines?
Much smaller; they aren't the same turbo by a long shot, but I'll explain what I know as of right now. Keep in mind: this is all my own opinion, and you have to see this from the perspective of someone who knows turbo tech looking back on what GM did.
In the 150hp Spyder engine, there was a drastically undersized compressor wheel but the turbine was about the correct size to give appropriate boost response. This means that while it was fun to drive, its performance was severely limited by its inefficient compressor. In the 180hp engine, the turbine was slightly too large and the compressor was again on the small side. This meant that its performance was somewhat lacking, because of the lag in boost onset caused by the large turbine.
It's possible that the reason for limited boost in the 150 and late boost in the 180 was because GM was all too aware of the limitations inherent in the cooling system of the aircooled powerplant, so they made sure that destruction of the engine was to be avoided at all costs- it was designed into the engine from the very beginning. Because neither engine was capable of more than about 10 psi even on a very hard run, I suspect that a large compressor would not have been seen as needed by the engineers. It could also be that they wanted to avoid undue transmission failures that might have been caused by loads of low RPM turbo torque, but that's purely speculation. Remember, these were folks that were pushing the envelope of what was possible, but they still had a company to look out for and so warranty claims were still a consideration.
Now let's look at the Jetfire.
Here's a 3.5L all aluminum V8 engine, cooled by water not air. It had more than enough cooling capacity to handle the turbocharger, so you would think they would go balls out on it. Not the case. On the contrary, they opted instead to use a very small turbo and also keep a very high static compression ratio. I can't say what motivated this decision, but it could be that they were directed to work with a base engine already in production. Since the turbo couldn't reliably add much power to an engine already at 10.25:1, 5 psi boost was the target, with any detonation being moderated by alcohol injection. Since only 5 psi was on tap, a large compressor wheel was not needed just like with the Corvair. The choice of such a small turbine could be explained by engineering wanting a flat torque curve, and instant reponse. Again, speculation. The main difference between the Corvair and F85 stuff is the F85 had a wastegate, and so a restrictive carb throat wasn't required to control boost pressure as it was with the Corvair. This may also have played into the turbine wheel size decision, since even a very small turbine could be controlled reliably via the wastegate. (without a wastegate, I suspect GM went with a slightly large turbine to help control the system).
If Oldsmobile engineers had utilized a proportionally larger single turbo for their 215 ci engine, would the larger turbine and impeller have caused significant spin-up delays because of the added mass and weight?
Possible. Though with 8 cylinders, spooling even a large turbo is easier than with only 4 or 6. It goes back to what they were trying to achieve, and we can't possibly know what they were thinking. Knowing what I know about OEM turbo engines today, they don't want a 'peaky' engine by any means. What they are after is as flat and broad a torque curve as possible, so it operates just like an N/A engine. That means you need nearly off-idle boost response, which could have been a contributing factor to turbine selection back then just as it is now.
I suppose that doubling the turbos, as you suggested, with two of the smaller T3-sized turbos would have avoided turbo lag, but would also have doubled the cost and would have added complexity.
Very true. Can you imagine a twin turbo 215 though? Would have been an absolute blast to drive. I believe that technology was holding them back, same as it was with the Corvair. That is the ultimate reason why the idea was abandoned, it didn't resurface again till the advent of multipoint injection in the early 80's when they had better control of the engine.
In a world where the aluminum engine costs and production problems were already killing the aluminum engine, the use of two small turbos would probably have been unacceptable.
Indeed, one turbo was eventually seen as unacceptable. lol
Turbochargers in production vehicles are still rare. I have a single turbo in my 1991 Toyota Supra, and Toyota later introduced twin turbos in the following generation Supra (although production was short lived). Where are the turbochargers now?
Actually, I believe turbos are again making a comeback because of rising fuel prices. Subaru, Mitsubishi, Ford, VW, Nissan, Dodge and Audi all have production turbocharged engines out there, though at a cost premium vs older technology. I personally have been waiting for this to happen for a long time, because large engines that suck down gas simply don't interest me. I'm not one of those greenie eco-nuts or anything like that, it's simply that we have had the technology to make better engines for a very long time but have chosen not to pursue that avenue. Why? The cost of fuel was low, so there was no incentive. So to a certain extent, I do believe that fuel should remain at around $3.50~$4.00 a gallon. There's simply no excuse for being so wasteful, especially when no one knows how much gasoline there is in the world for us all to use.
Back on topic though, technology was what kept them from making a truely viable turbocharged engine back in the 60's.
As for the turbos themselves, the Jetfire unit shares much in common with the TRW/Rajay unit from the Corvair. Both have radial compressors, neither of which involve backwards curved blades because it hadn't been invented yet. Both Corvair units employed full bladed compressors, while the earlier Jetfire unit had a split blade design (one set of fins lower than the other to improve flow). I found that strange since it was introduced first, only the E-flow Rajay wheel is like that. Both units have a positive-style carbon faced seal, but the Jetfire unit is encapsulated vs the rebuildable 4-piece design chosen by TRW. For bearings, the Jetfire unit has full floating bearings while the TRW has a pinned non-floating one. This architecture has been used by Garrett ever since the beginning then, because they still have a nearly identical support structure for the shaft to this day.
More later, my fingers are tired.