Neil,
According to the data I have the efficiency of Lysholm type compressors doesn't reach more than 75% while centrifugal ones attain about 84% efficiency (overall).
Another point is that you can't drive directly - on the same shaft - a Lysholm compressor with an exhaust turbine since they don't spin at the same revs. Even with a reduction gear between it wouldn't work well because their characteristics maps do not follow the same pattern.
With the Nomad's design, all the turbomachinery lies on the same shaft and the power of the turbine directly drives the compressor, just like in a turbocharger. So, the CVT between the crankshaft and turbocharger never transmit a huge amount of power to or from the crankshaft.
There would be no point in driving a (two stages) volumetric compressor from the crankshaft and then recover the full power of the exhaust turbine by means of a reduction gear and a hydraulic coupling to absorb the torsion vibrations. In addition to the lower compressor efficiency, greater mechanical losses would occur. If the Wright R-3350 Turbocvlone used that scheme (but with a centrifugal compressor) it was probably just to exploit the existing Cyclone basic layout.
Let me get a little bit out of my way now!
For wheels traction purposes an even better concept can be envisaged. Let's call it "Turbocompound High Pressure Differential Supercharging" and let's drive the two-stage centrifugal compressor by means of a planetary differential and a step-up gear train. The crankshaft(s) of the (preferably opposed pistons 2-stroke) Diesel would drive the planet carrier, the ring the compressor while the sun would be on the output shaft. The exhaust turbine is then geared to the output shaft. We get a kind of half gas-generator, an engine working as an integrated torque converter. A problem is the excess of compressed air at vehicle launch. At 6 bars (abs) of intake pressure, about 57% of the crankshaft power goes to drive the compressor and the Diesel can only rev at 57 % of its nominal rpm with the output shaft stalled. But the compressor is spinning at full speed and delivers more air than needed for scavenging and combustion.
There are several solutions. Just 3 :
- The excess air can be by-passed directly to the turbine or to a separate turbine.
- Variable pitch stator blades on the compressor inlet would help.
- A variable compression ratio engine could be used( specific design wanted…)
Of course there would be a heat exchanger and an intercooler between the two compressor stages to lessen the power needed to drive it and decrease the thermal load. With a variable geometry turbine inlet, the efficiency would be quite good from low vehicle speed. A clutch or one way clutch to lock the differential would prevent the crankshaft to rev slower than the output shaft and so avoid stall or even reversion of the compressor rotation. A 4-speed powershift transmission would be all right for up to about 40 tons rigs.
Two locomotives using the concept of Dr Leonhard Geislinger (see CIMAC 1955, "A locomotive with thermo-pneumatic transmission" or something like that) were built and successfully put in regular duty in Sweden in 1955 . The worked about the same way, but with two Hedemora-Pielstick 4-stroke engines and an auxiliary combustion chamber to utilize the excess air. Frank Wallace at Bath University also published several papers about his DCE or "Differential Compound Engine", but he apparently ignored the previous work and practical results of Geislinger.
Cheers
Aorangi