F1 season is no write-off for Renault
Unfortunately it seems they still haven't understood their reliability issues, I hope they will do soon.
You have misunderstood how turbines perform. It isn't turbine speed which cause the expansion ratio to increase (which is what you refer to as backpressure), but exhaust flow. Increase the exhaust flow and the expansion ratio will increase for any given turbine, and this is not really dependent on turbine speed. A turbine behaves similar to a nozzle, the more gas you try to push through the greater the pressure on the inlet side. Want to blow more gas without the increased inlet pressure - get a bigger nozzle.stevesingo wrote:From a purely turbo point of view I would agree. But the MGU-H is driven by the turbine also.
So we have two loads applied to the turbine Compressor and MGU-H
Power generation from the MGU-H is unlimited in the regulations. Boost is unlimited in the regulations, but is effectively limited by the fuel flow at about 2.75 Bar and mass air flow <1500kg/hr. As power is a function of force over distance and in the case of a generator torque applied over rotational speed, we can either apply high torque to the turbine at a lower speed or low torque at a higher speed. There will be a compromise of where in the scale of MGU-H tq/rpm gives the least backpressure to MGU-H benefit.
My thinking is, the work done by the turbine should favour the unlimited output-MGU-H. The turbine can have a finite amount of load applied before losses from increased back pressure exceed the gains from MGU-H.
Could the Turbine be sized where it makes up to 125k rpm at 7krpm engine speed or even at part throttle. In normal circumstances the compressor will surge, but if we bleed off excess mass air flow we could prevent surge. Yes there will still be load applied to the turbine by this work done, but there may be a balance to be had where total load applied to the turbine is less than the gains from MGU-H generation.
I am just theorising here and the 125k rpm may not be attainable, but I believe there will be a balance to be had, which will be forever changing with load and engine speed, where MGU-H power might take priority over compressor function and in the case of too much boost, then that could be bled off in order to prioritise MGU-H function?
Haven't you entirely missed the thermal part of the equation. For illustration, use appropriate part of formula.Edis wrote:You have misunderstood how turbines perform. It isn't turbine speed which cause the expansion ratio to increase (which is what you refer to as backpressure), but exhaust flow. Increase the exhaust flow and the expansion ratio will increase for any given turbine, and this is not really dependent on turbine speed. A turbine behaves similar to a nozzle, the more gas you try to push through the greater the pressure on the inlet side. Want to blow more gas without the increased inlet pressure - get a bigger nozzle.stevesingo wrote:From a purely turbo point of view I would agree. But the MGU-H is driven by the turbine also.
So we have two loads applied to the turbine Compressor and MGU-H
Power generation from the MGU-H is unlimited in the regulations. Boost is unlimited in the regulations, but is effectively limited by the fuel flow at about 2.75 Bar and mass air flow <1500kg/hr. As power is a function of force over distance and in the case of a generator torque applied over rotational speed, we can either apply high torque to the turbine at a lower speed or low torque at a higher speed. There will be a compromise of where in the scale of MGU-H tq/rpm gives the least backpressure to MGU-H benefit.
My thinking is, the work done by the turbine should favour the unlimited output-MGU-H. The turbine can have a finite amount of load applied before losses from increased back pressure exceed the gains from MGU-H.
Could the Turbine be sized where it makes up to 125k rpm at 7krpm engine speed or even at part throttle. In normal circumstances the compressor will surge, but if we bleed off excess mass air flow we could prevent surge. Yes there will still be load applied to the turbine by this work done, but there may be a balance to be had where total load applied to the turbine is less than the gains from MGU-H generation.
I am just theorising here and the 125k rpm may not be attainable, but I believe there will be a balance to be had, which will be forever changing with load and engine speed, where MGU-H power might take priority over compressor function and in the case of too much boost, then that could be bled off in order to prioritise MGU-H function?
Turbine efficiency is however dependent on turbine speed, or more specifically the blade to gas speed ratio. In other words, if you operate with a low amount of "backpressure", the gas velocity in the nozzle will be low and as a result the turbine speed should be low too. Of course, the amount of work that can be extracted from the exhaust gas by the turbine is dependent on the expansion ratio, so the more backpressure the engine can handle, the more power can be provided by the turbine.
If you bleed charge air you're wasting turbine power that could drive the generator instead.
#aerogollumturbof1 wrote: YOU SHALL NOT......STALLLLL!!!
This is probably a bot. So report and ignore until moderation/admins will take care of it.rapha-78 wrote:Honestly ocaviosa what's the point of disturbing F1 fans who just talk to each other about their passion ??? WTF ?
Sounds like like they are too proud to use Mario's design, as if they didn't have enough egg on their faces already!peterg wrote:Renault decide not to adopt Ilmor prototype?
http://www.motorsport.com/f1/news/renau ... pe-option/?
So prove me wrong? Calling my assessment of the situation "baseless" without providing evidence to show that is the case and down-voting my comment is frankly pure hypocrisy!Cold Fussion wrote:Could you perhaps leave such baseless statements for the general section of the forums and not pollute the technical suggestions as well?