Over on the RC forum Whiteblue made this statement:
I am wondering what will be allowed, and what the manufacturers will choose to do.
With lower power of the ICE compared to today it is quite likely that the cars will run full throttle for a larger percentage of the lap. Considering hat at some tracks the cars already hold full throttle for as much as 70% of the time, will there be any need for variable valve timing and lift, and particularly to use it for throttle-less engine control?
Is it likely that injection pressures will be limited?
What is a bore/stroke ratio which minimises heat loss? The maximum allowed bore is to be 88mm, which would give a stroke of about 65.8mm, and a bore:stroke ratio of 1.34. Surely the manufacturers will still look to maximise piston area and valve area?
To contain costs some of the materials used in the engines will be specified. Will that dictate how hot various parts of the engine will run?
From the articles I have read it is unlikley that turbocompounding will be allowed for 2013, but may appear in 2014. How would it be achieved, and will it be worthwhile downstream of the turbo?
Apart from some Diesel truck engines, is anybody developing a turbo-compound for road use?
Also, some technologies will be proprietry, and thus may not be allowed unless it is freely available to all manufacturers. Could this be a problem?
With efficiency being the goal, will some teams/engine manufacturers try for a transverse installation?
Lastly, with the engine freeze system, and the likelihood of the FIA imposing limitations on engines used per season, how much development will occur?
We now have a max speed of 12000rpm, 500 bar injection pressure. It has been hinted that there will be a 100kg/hr max fuel flow and Ø88 bore.
So what will the engine be like?
With restricted fuel flow it is all about engine efficiency to get max power. This leads to a couple of key things:
1/ Absolutely want to reduce the piston velocity and port flow velocity as much as possible to increase efficiency, and that means maximum piston diameter allowed (just like current engines), Ø88mm seems unnecessarily restrictive to me - should be more like Ø95-100mm
2/ Most turbo engines are heavily overfuelled at max power in order to prevent the turbo from melting/ destroying itself, while max power occurs at about 13:1 A/F, Most high power turbos run at more like 10:1 at max power using fuel to keep the turbines cool (and is a tremendously wasteful approach). This is just not feasible given limited fuel flow so one of the keys will be getting the turbine inlet temps up. TiAl and MarM247 Turbines can handle 1050°C turbine inlet temp and this helps, but it will probably also be necessary to do one of the following:
a/ run a pre-turbine exhaust cooler of some type (water cooled exhaust manifold etc).
b/ run a ceramic turbine (lighter, and can handle higher temps - but can be durability issues)
c/ bypass a little compressor air straight to the turbine (not always possible, but can be done over a reasonable range of engine rpm given no muffler and efficient compressor and turbine - also helps prevent surge at low rpm)
d/ run a Miller cycle engine
From these options the Miller cycle (with late closing inlet valve to reduce the air in the cylinder) is an almost certainty. Miller cycle gives a relatively longer expansion stroke to suck a little more heat (and temp) out of the gas before it goes to the turbine and means that you get a higher efficiency engine (220-230 g/kWh vs 240-250 g/kWh for non-miller cycle that in turn means 5-10% more engine power for a fuel flow limited engine). The engine runs a higher geometric compression ratio (a couple of points above normal turbo, so for this engine might be more like 12:1 or 13:1 compression vs the 10:1 that a DI turbo with 1 bar boost would have. (Incidentally with 100kg/hr fuel flow and 220-250g/kWh we know that the power output will be about 400-450kW = 530-600hp).
I haven't seen any talk of limiting the boost pressure - and shouldn't need to given fuel flow restriction. That would point towards high boost levels and running at much lower speeds to reduce the engine frictional losses and improve efficiency at max power. 3 bar boost is definitely a possibility with max power from 6000rpm dropping off slowly through to 12000rpm. Would probably spend most time at lower end of this speed range - and perhaps voluntary self limited max rpm of maybe 8-9000rpm. There would be far less need to change gear than currently as the engines can deliver basically max power over such a broad rpm range.
This desire to run at lower speeds will run counter to F1 marketing, so I expect that this may push the rules towards either a boost level limit (say 2 bar) or a low rpm fuel flow limit to force engine designers to set max power point at say 9000-10000rpm and above.
Other issues:
Be interesting to see how the compromises on intercooling work out - bigger intercooler with greater aero drag losses and lag but higher engine efficiency, or smaller with efficiency hit?
Compressor wheels should be carbon fiber for reduced inertia and smaller running clearances (giving higher efficiency), though advantage over aluminium isn't huge.
Sodium cooled valves for sure.
VVT would be preferred from a development and performance point of view, but lets see what the rules allow.
It would be disappointing if they did not run brushless electric motors on the turbos for anti-lag (this is a technology that has useful crossover to cars and trucks) - and once that is in place it is very simple to also use it for turbocompounding for extra efficiency.
McClaren's engine supplier for the MP4-12C Riccardo is in the box seat with their experience on that 3.8l turbo, (max power at 7000-8500rpm, though would need a much bigger turbo)
Ton of North American experience from IRL, CART etc.
Cosworth are next door to one of the premier supercar turbo gasoline engine developers - Mahle Powertrain.