ppj13 wrote:Tommy Cookers wrote:@ ppj (mostly)
AFAIK ....... a turbo is normally operating in blowdown turbine condition
blowdown 'pulses' drive the turbine, the mean exhaust pressure is not raised relative to the induction pressure (it can fall)
backpressure means the mean exhaust pressure is higher than the induction pressure, this is called pressure turbine condition (the exhaust valve motions of course isolate the combustion chamber from the backpressure)
1. Pressure inside exhaust manifold will be close to pressure at intake manifold (let's say I:3.0, E:2.5bar) when turbine is powering the compressor. If turbine is turbocompounding (powering the MGUH), probably higher.
2. Pressure inside exhaust manifold will be close to zero if you open a big wastegate. Pumping alone, doing very quick math, will take 20hp less than regular ICE, 40hp less than turbocompounding ICE. That extra power will "go" to the flywheel.
3. Air mass flow can be kept with the MGUH at the same levels. Boost required to keep AMF will be lower, but that's not related to the point.
Tommy Cookers wrote:
mgu-k recovery is torque limited by rule so that 161 hp recovery is only allowable over about 5500 crank rpm, below that it falls
surely there will be little or no capacity provided eg in the motor drives to allow higher total power (than this 161 hp) from storage ?
I don't follow. If you mean there is no energy in the batteries to power both MGUK and MGUH consistently during a race in the max power mode, then I fully agree with you. If you mean you can't ever draw 250hp from the batteries, I don't agree. You can for short burst. There is no limit to that, not in the rules, not in the physics, as long as you plan for it.
there is a level of exhaust turbine power recovery that doesn't increase mean exhaust pressure
so there is no loss of crankshaft power ie on the exhaust scavenge upstroke (this level we might call the blowdown level)
according to Wright, who made 10000+ such engines, to NACA who researched it, and to Buchi who invented it ?
they show that around 10% power can be added by the tc without loss of crankshaft power or any increase in fuel consumption
they used axial flow turbines, mechanically driven centrifugal superchargers and rather low CRs
in 2014 we are using some of the turbine power to drive a centrifugal supercharger ie turbocharging
this will give a nice forward pressure when we choose to allow this ie at low mgu-h recovery
increasing turbine power % is possible, but forward pressure is reduced as mean exhaust pressure must rise
increase beyond this gives backpressure, some crankshaft power is lost, but compounded power is maintained and sfc increased
so the crankshaft power temporarily liberated by wasting exhaust and supercharging electrically depends on the operating condition
ie compounding does not necessarily mean any raising of exhaust pressure (this was my original point)
as rpm rises over 10500 rpm less supercharging power will be needed, gain from cutting the compounding may be less than hoped
the motors are not driven directly from the battery
to provide always the desired torque at every PU rpm the motor voltage must be continuously varied
this requires a motor drive, the designer will choose some limit to its useable current and related losses (self-heating)
also inversion will likely be needed, and the drives are bidirectional
your eg 250 hp drives regime will need to be bigger and will need more cooling than eg a 160 hp drive regime
transistors in the drive will have low thermal time constants, there is little scope for temporarily overload (unlike the MGs)
given that the dominant jobs of the electrical system are near-continuous motor action of an MG limited to 160 hp
and near-continuous generator action of an MG surely sized for this at around 100 hp
I just can't see it having particularly a 250 hp capability for some cunning but occasional activity of poor efficiency