2014-2020 Formula One 1.6l V6 turbo engine formula

All that has to do with the power train, gearbox, clutch, fuels and lubricants, etc. Generally the mechanical side of Formula One.
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WhiteBlue
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Re: Formula One 1.6l V6 turbo engine formula

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wuzak wrote:I was under the impression that AC motor/generators did not use permanent magnets.
The fact that you refer to it being a "self induced" design would seem to indicate that you concur. If there are magnets there is no need for induction (passing a current through one part to create a current to generate a magnetic field).
http://en.wikipedia.org/wiki/Servomotor
Google "AC servo motors" and look at Wikipedia for the ultimate performance, brush less AC variety. That is the thing.
For ultimate performance in a compact package, brushless AC motors with permanent magnet fields are used...
I have to admit that self induction was misleading. The motors do have magnets but no brushes. The induction is done by power inverters which is also explained by a wiki article linked on the same page. http://en.wikipedia.org/wiki/Power_elec ... te_devices The drives used are vector type inverters typically with IGPTs, at least in those applications that I have seen where the machine is an MGU.
Formula One's fundamental ethos is about success coming to those with the most ingenious engineering and best .............................. organization, not to those with the biggest budget. (Dave Richards)

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ringo
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Re: Formula One 1.6l V6 turbo engine formula

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You guys are looking at this from a motor with a load that is steady and induced by the motor itself. Such as drilling through a material or pumping water. Where that load does what the motor insists and the load has no other connection to anything else.
What you are not looking at is that the MGU motor/generator is the load on the turbine. even with a closed loop control system it will always be a load. No matter the complexity, the only way it will control the turbos speed is by braking the turbo.

If you have an operating parameter you want this motor to stick to, it will either power the turbo to speed it up, or brake the turbo to slow it down. This is all understood by me.
But in both of those cases the turbine is a load. It is a load on the battery when it is speeding up the turbo.
And it a load on the turbine when it is behaving like a brake. This is energy consumption, in the case of braking yes it storing some energy.

Now where i see a problem, is that 90% of the time you will be using MGUH as a brake. It's not many instances where a turbo is too slow. So you will be increasing back pressure and thus increase pumping losses on the pistons whenever the MGUH is behaving in this constantly corrective way, trying to control a turbo (which i don't see the point of constant control). Anyhow, i don't even think it has the physical capability to do this anyway. That thing will be heat soaked in no time, duty cycle will be a big factor. (Notice the rules permit a clutched MGUh, they know the thing can't constantly be engaged)

Real turbine control, comes from mass flow control. this has no adverse effects on temperatures or back pressure, which is healthy for overall power output and also component life. I am of the belief the wastegate will still be present because of the reduced cost in r&d and also the reliability, simplicity, reduced cooling demand, and also no negative impact on ICE efficiency.

before i forget as well, if your mguh has a low power rating, it will not be able to do complete boost control. You will still need a waste gate. The only way you wont need a waste gate is if at the peak power at 10,500rpm the MGUH capacity plus the compressor's power is such that the turbine will be at a reasonably steady state and wont over speed with those two loads applied. Now we all know this will only work at one engine speed range.
What happens at other speed ranges? You may find that you have too big or too small a turbine, and your dependency on MGUH motoring will be too high (this remember is draining energy from your ES to drive the turbine and compressor, it's not free energy) or you will have a very inflexible turbine selection, that was simply sized around a generator load and wasn't sized for the engine itself.
That's where the wastegate comes in. It allows you to cheat this system by mass flow control. it's effectively giving you a million turbine sizes, at different pressure ratios, at any time you feel. Simply because the turbine sees only mass flow and pressure.
A motor cannot manipulate a turbines mass flow or inlet pressure. It can only motor it or load it. This doesn't change it's mass flow. It's only after it slows the turbine, backing up the flow, raising the temperatures, fatiguing the blades, then reducing the boost, which goes to the engine then a lower powered pulse comes out the valves do you get any semblance of mass flow reduction. It's quite clunky if you ask me, and a bit of hammer and tongs. It's not as delicate and finely controlled if you ask me.
All that motor control technology which is all interesting, only looks good on the motor side of things. It doesn't say much about what it is doing to the turbine and compressor package. It doesn't take into account turbine operation and nature.

Now it would be interesting if we get into the physical structure of the motor?
Tommy, are you suggesting DC servo motors, which have the windings on the stator?
For Sure!!

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WhiteBlue
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Re: Formula One 1.6l V6 turbo engine formula

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Windings will be on stator because it will be better for dynamics. Less mass. And it will be AC.
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chip engineer
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Re: Formula One 1.6l V6 turbo engine formula

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ringo wrote: But in both of those cases the turbine is a load. It is a load on the battery when it is speeding up the turbo.
And it a load on the turbine when it is behaving like a brake. This is energy consumption, in the case of braking yes it storing some energy.

Now where i see a problem, is that 90% of the time you will be using MGUH as a brake. It's not many instances where a turbo is too slow. So you will be increasing back pressure and thus increase pumping losses on the pistons whenever the MGUH is behaving in this constantly corrective way, trying to control a turbo (which i don't see the point of constant control). Anyhow, i don't even think it has the physical capability to do this anyway. That thing will be heat soaked in no time, duty cycle will be a big factor.
But while the MGUH is braking the turbo, that power can be going to the MGUK to accelerate the car, which should be a win despite increasing back pressure. Also, the efficiency of brushless motor-generators can be very high (maybe >90% not counting the drive electronics). So it should be able to take 120 kW from the turbo and still need less than 12 kW cooling.

dlstanf2
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Re: Formula One 1.6l V6 turbo engine formula

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I've listened to Mercedes V-6. Even with all the talk about the exhaust being LOUD so it doesn't matter the sound. No so.

The V-12 has a very pleasing mixture of mechanicals and firing order.
The V-10 had the same.
The V-8 Had more a growl and I loved the torque sound of it pulling out od a corner.

The V-6 Turbo is quitter and the driver is constantly 'blipping' the throttle to keep the turbo spooled. The V-6, in my option, sounds like a 2-stroke chainsaw motor and is not very pleasant. It does not even compare to the 'Banshee' scream of the motorcycle engines used in Midget Racing.

F1 may be losing more than one fan with this ''Green Option" motor.

Between Bad Tires and irritating engines doesn't become hard to change the channel or not purchase a ticket. Are these engines going into their flagship models?

wuzak
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Re: Formula One 1.6l V6 turbo engine formula

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ringo wrote:You guys are looking at this from a motor with a load that is steady and induced by the motor itself. Such as drilling through a material or pumping water. Where that load does what the motor insists and the load has no other connection to anything else.
What you are not looking at is that the MGU motor/generator is the load on the turbine. even with a closed loop control system it will always be a load. No matter the complexity, the only way it will control the turbos speed is by braking the turbo.
Correct, the MGUH is a load on the turbine the same way as the compressor is a load on the turbine.

Also correct that the way the MGUH controls the turbo is by controllingits speed - ie braking the turbo.

ringo wrote:Now where i see a problem, is that 90% of the time you will be using MGUH as a brake. It's not many instances where a turbo is too slow. So you will be increasing back pressure and thus increase pumping losses on the pistons whenever the MGUH is behaving in this constantly corrective way, trying to control a turbo (which i don't see the point of constant control). Anyhow, i don't even think it has the physical capability to do this anyway. That thing will be heat soaked in no time, duty cycle will be a big factor. (Notice the rules permit a clutched MGUh, they know the thing can't constantly be engaged)
The turbine and MGUH will, of course, be sized to match the requirements of the engine. If there is too much back pressure during operation then they have screwed up the sizing of the turbine.

It seems self evident that at 10,500rpm, the point where maximum fuel flow kicks in, the turbine will be producing its maximum power. The compressor will be demanding its maximum amount of power at that point too (max boost).

The mass flow of the engine is far in excess of that required to simply drive the compressor. Thus the turbine is sized to take advantage of this, and the MGUH "brakes" the turbine to maintain speed control.

I would imagine at this point the back pressure is no more than for a conventional turbo.

As the engine speed increases the fuel flow remains the same and the engine air mass flow rate remains constant or nearly so. But there is less boost on the intake side, so there is less energy for the turbine. If the turbine were to maintain the same speed the back pressure would be reduced.

It is my opinion that the power generated by the turbine will fall off less than the demand for the compressor. Thus, as revs increase the MGUH will be able to make more power. I would think that backpressure would be maintained, rather than increased, as the ICE rpm rises.

As to the use of the clutch. This is not because the MGUH can't handle the duty cycle. It is because at certain load conditions the turbine power will match the compressor demand. If the MGUH remained connected always it would be a drag on the system, and would prevent the turbo from accelerating or, perhaps, would even slow it down, which would be undesirable.

The MGUH will be liquid cooled, and that will be a very important system.

ringo wrote:Real turbine control, comes from mass flow control. this has no adverse effects on temperatures or back pressure, which is healthy for overall power output and also component life. I am of the belief the wastegate will still be present because of the reduced cost in r&d and also the reliability, simplicity, reduced cooling demand, and also no negative impact on ICE efficiency.
You could argue that control of the compressor provides mass flow control. Remember that the engine will give nearly constant air mass flow from 10,500rpm to 15,000rpm, and this is controlled by the boost/air mass flow from the compressor, which is controlled by the MGUH.

A wastegate may be included as insurance against MGUH failure. But I don't believe it will be used for primary control.

Using a wastegate maybe simpler, easier and (as of now) more reliable, but it is also a waste of energy.

You could, conceivably, use a wastegate in conjunction with the MGUH, but I'm not sure why you would. To get any benefit from the MGUH the bypass from the wastegate would need to be small. Almost pointless, in fact.

ringo wrote:before i forget as well, if your mguh has a low power rating, it will not be able to do complete boost control. You will still need a waste gate. The only way you wont need a waste gate is if at the peak power at 10,500rpm the MGUH capacity plus the compressor's power is such that the turbine will be at a reasonably steady state and wont over speed with those two loads applied. Now we all know this will only work at one engine speed range.
What happens at other speed ranges? You may find that you have too big or too small a turbine, and your dependency on MGUH motoring will be too high (this remember is draining energy from your ES to drive the turbine and compressor, it's not free energy) or you will have a very inflexible turbine selection, that was simply sized around a generator load and wasn't sized for the engine itself.
Why would you design this system and then stick on an MGUH with insufficient generating capacity?

Why would you size the turbine incorrectly? Why would you do R&D for 3 years only to completely mess up the fundamental turbine/compressor/MGUH sizing?

ringo wrote:A motor cannot manipulate a turbines mass flow or inlet pressure. It can only motor it or load it. This doesn't change it's mass flow. It's only after it slows the turbine, backing up the flow, raising the temperatures, fatiguing the blades, then reducing the boost, which goes to the engine then a lower powered pulse comes out the valves do you get any semblance of mass flow reduction. It's quite clunky if you ask me, and a bit of hammer and tongs. It's not as delicate and finely controlled if you ask me.
As clunky as dumping excess energy out the exhaust?

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WhiteBlue
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Re: Formula One 1.6l V6 turbo engine formula

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What does the board think of the proposed rpm band that is seen in the Merc simulation of Monza? Is it realistic? I feel it is a starting point even if we consider that publishing this sound file may be a bit of a smoke screen. Personally I was of two minds about the rev band they would be using. In this video they do not use the revs between 4.000 and 8.000. They would only be used for safety cars in this engine setting.

How would they adapt to fuel saving mode when they are over the fuel curve? By short shifting or by going to a lower than 8.000 base rpm?

Also, I have not seen any evidence that there is any artificially high revs in cornering in order to burn fuel for electricity generation. What do you think of this?
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Tommy Cookers
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Re: Formula One 1.6l V6 turbo engine formula

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dlstanf2 wrote: Are these engines going into their flagship models?
of course
this will be hybridisation by the back door
electric driving in cities, then urban areas, then suburban areas
and then not just the flagship models
European (+ Japan ?) protectionism by the back door
anti-competitive

Tommy Cookers
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@ ringo
all our 'turbo' experience has been without backpressure
assuming we haven't needed to lower the CR, this gives a relatively small amount of free power (for supercharging or compounding)
this was the basis of the world's only significant turbocompounding programme, giving on average less than 10% free power
and it would give a similar result in 2014 F1 ?

higher exhaust pressure (ie a substantial backpressure) loses crankshaft power but allows corresponding increase in recovered power
because the usual (necessary evil) large pressure/KE losses around the exhaust valve are reduced by backpressure
NACA tests showed a much larger gain in bsfc from this (15-20% better than the engine in turbocharged form)

so for 2014, backpressure is no longer a bad thing ?
and promises more combined power
if/when there is a correspondingly larger recovery system

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WhiteBlue
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Tommy Cookers wrote:NACA tests showed a much larger gain in bsfc from this (15-20% better than the engine in turbocharged form)
so for 2014, backpressure is no longer a bad thing ?
and promises more combined power if/when there is a correspondingly larger recovery system
Do you have a public source for that info? The kinetic energy point sounds convincing to me, although it should happen in a conventional small turbo as well. But when the turbine gets twice the size the effect would be more prominent.
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wuzak
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Re: Formula One 1.6l V6 turbo engine formula

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WhiteBlue wrote:
Tommy Cookers wrote:NACA tests showed a much larger gain in bsfc from this (15-20% better than the engine in turbocharged form)
so for 2014, backpressure is no longer a bad thing ?
and promises more combined power if/when there is a correspondingly larger recovery system
Do you have a public source for that info? The kinetic energy point sounds convincing to me, although it should happen in a conventional small turbo as well. But when the turbine gets twice the size the effect would be more prominent.
This may be a start.

wuzak
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wuzak
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http://www.cranfield.ac.uk/sas/pdf/engi ... ngpost.pdf

This one says about 7% energy recovered in a 4 cylinder engine.

7% of 450kW (603hp) ~ 31.5kW (42hp).

It says:
It is important to note that the gear ratio of the mechanical linkage was optimised to get the highest value possible for the power at 8,500 rpm. Furthermore, the ratio was the same for all speeds. A higher output can be obtained if the gear ratio is variable and is optimised at each speed.
The MGUH gives that variable speed control.

Also
The study also revealed that an axial turbine induces less backpressure than a radial turbine and is therefore better suited for this application.

Tommy Cookers
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the NACA report 822 is what I had in mind
its tabulated results show that raising the exhaust pressure moves power from crankshaft to turbine roughly 1:1
power remains roughly constant, but efficiency is greatly improved
and the focus of the work is these large BSFC gains from raised exhaust pressure

Google NACA UK Archive 1945
or NACA report 822
(its in the archive at Cranfield)
or naca.larc.nasa.gov/

http://www.enginehistory.org/Wright?TC%20Facts.pdf
should get the Wright brochure that covers the rather different position of the version they sold to airlines in the 50s
they sold engines with high power and reasonable bsfc, not engines with high bsfc and reasonable power

Google this
turbo compounding the rotary
it should get Join aircraft rotary engine newsletter
which has loads incl Fig 15 recovery energy balance from 1954 SAE Transactions 'Development of the R-3350 Turbo Compound Engine'
Paul Lamar points out the large pressure loss at the exhaust valve
this inspires him - see his upload to Youtube

at leanish cruise the Wright TC has 2655 hp sensible exhaust energy
of which 1735 hp is unusable by any expander
an expander (eg turbine) can only use the KE (920 hp available)
of this 525 hp is dumped bt the exhaust going from cylinder to exhaust port
the net recovery after all losses is 160 hp
and the combined output is 1840 hp

BTW both the production TurboCompound engines and the 500,000 ? so-called turbocharged engines the USA made in WW2 always had mechanically driven superchargers, categorised in the papers referenced above as auxiliary superchargers
(so the turbocharger was always in any production engine a second stage of supercharging)
Last edited by Tommy Cookers on 06 Aug 2013, 12:12, edited 5 times in total.

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wuzak wrote:http://www.cranfield.ac.uk/sas/pdf/engi ... ngpost.pdf

This one says about 7% energy recovered in a 4 cylinder engine.

7% of 450kW (603hp) ~ 31.5kW (42hp).
...
That seems very reasonable to me.
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