Show your calculations please.
I'm not the person you're replying to, but there's a 3000MJ/h limit to the fuel energy flow in the regulations. Now MJ/h (unit of mechanical work per unit of time) is obviously a unit of power, so 3000 MJ/h = 833 kW.
Agree that minimizing pulse blow-back is a must, If the turbocharger exhaust turbine type used in formula 1 wasn't a pressure turbine, there will not be pulse blow-back to minimize, because the usual pulse blow-back wouldn't be present to eliminate by the usual exhaust piping design, the design standard thing. A number (more than 'one') Individual cylinder-to-exhaust turbine exhaust stacks/pipes/primaries all individually/separately discharging into the exhaust recovery turbine, would render the exhaust turbine a 'blow-down' type of turbine, and would have eliminated pulse blow-back as well as exhaust gas back pressure.PlatinumZealot wrote: β20 Jan 2026, 02:22It uses some form of pulse effect because they would all stay with log manifolds if it were only a pressure turbine.saviour stivala wrote: β19 Jan 2026, 06:30Yes. Agree that the 'twin-scroll' exhaust turbine housing design minimizes the effect of mixing all exhaust pulses into one collector, by dividing said pulses into two collectors. As the formula 1 ICE is a V-6 cylinder, using a twin-scroll exhaust turbine housing means that two sets of three selected cylinders will each blow their respective exhaust gas through a primary, with all three primary in the set pumping into a collector, with each of the two collectors pumping into the nozzle aimed at the turbine. The system of multi primaries (more than one) pumping into a collector with the collector pumping into the turbine nozzle aimed at the turbine, will still render the exhaust turbine a 'pressure turbine'. The fact that a variable opening waste-gate is used, provides the exhaust gases from cylinders to turbine with two paths, when the waste-gate is opened exhaust gas pressure is at atmospheric pressure, and no turbine recovery is possible, When it is closed, exhaust gas is above atmospheric pressure and turbine recovery is possible.gruntguru wrote: β19 Jan 2026, 04:54The turbine used in F1 utilises both pressure and blowdown pulses. Have you heard of a company call GARRETT? They know a thing or two about turbochargers. Here is an article posted on their website. https://www.garrettmotion.com/wp-conten ... vanced.pdf
The exhaust lengths do indeed seem to be tuned, and notice each runner meets at nearly zero degrees to minimize pulse blow-back.
The 1,000hp includes power (up to160hp) from the battery system, so should not be included in the TE calculation.johnnycesup wrote: β20 Jan 2026, 03:53Just to add to the previous discussion, using a common LHV for gasoline (44.3MJ/kg), the previous ruleset had a total fuel energy flow of 1230kW. If the 1000hp rumours are true, that would be a total thermal efficiency of 60,6%, which is pretty incredible.
Actually it makes a lot of sense that the MGUH couldn't power the MGUK with pure harvesting, haven't really thought of that before. So peak efficiency should be around 56 or so %, that seems more reasonable.wuzak wrote: β20 Jan 2026, 04:53The 1,000hp includes power (up to160hp) from the battery system, so should not be included in the TE calculation.johnnycesup wrote: β20 Jan 2026, 03:53Just to add to the previous discussion, using a common LHV for gasoline (44.3MJ/kg), the previous ruleset had a total fuel energy flow of 1230kW. If the 1000hp rumours are true, that would be a total thermal efficiency of 60,6%, which is pretty incredible.
TE would be around 51%, assuming all power for the MGUK comes from the battery.
It would be ~56% if about half the energy comes from the MGUH to MGUK.
But didn't the maximum power occur when the MGUH was being powered by the battery, and not recovering energy?
Maximum power possible was deployed when when at full throttle and at full fueling and with waste-gate fully opened with both MGU-K and MGU-H sharing battery power. Apart from when maximum power possible could be deployed, wasn't the MGU-H used to generate electricity that could be send directly to the MGU-K, effectively boosting its power output beyond what the brakes could capture and store in ES, which allowed for longer deployment of electric boost, which in turn effectively extended the duration the MG-K could provide its ~120 kw boost?.wuzak wrote: β20 Jan 2026, 04:53The 1,000hp includes power (up to160hp) from the battery system, so should not be included in the TE calculation.johnnycesup wrote: β20 Jan 2026, 03:53Just to add to the previous discussion, using a common LHV for gasoline (44.3MJ/kg), the previous ruleset had a total fuel energy flow of 1230kW. If the 1000hp rumours are true, that would be a total thermal efficiency of 60,6%, which is pretty incredible.
TE would be around 51%, assuming all power for the MGUK comes from the battery.
It would be ~56% if about half the energy comes from the MGUH to MGUK.
But didn't the maximum power occur when the MGUH was being powered by the battery, and not recovering energy?
This is circular reasoning.saviour stivala wrote: β19 Jan 2026, 06:30[...]will still render the exhaust turbine a 'pressure turbine'. The fact that a variable opening waste-gate is used, provides the exhaust gases from cylinders to turbine with two paths, when the waste-gate is opened exhaust gas pressure is at atmospheric pressure, and no turbine recovery is possible, When it is closed, exhaust gas is above atmospheric pressure and turbine recovery is possible.
As I explained, the pressure type of exhaust turbine as used in formula 1 incorporates a variable opening waste-gate set-up into the design, even when the exhaust turbine is of the 'twin-scroll' type, The presence of the waste-gate will in turn provide the exhaust gases pre-turbine with two possible paths, one is with waste-gate closed where the exhaust gases goes through the turbine at above atmospheric pressure, and the other is with the waste-gate fully open, where the exhaust gases (pre-turbine) are at atmospheric pressure, the exhaust gases will follow the easy way out like water does, end exit though the waste-gate and therefore bypass the exhaust turbine, the exhaust gases exiting through the waste-gate will be at atmospheric pressure, meaning zero back pressure in the exhaust system, A situation which was capitalized on by running the turbocharger compressor in electrical mode to produce the highest possible power output.Abarth wrote: β20 Jan 2026, 09:23This is circular reasoning.saviour stivala wrote: β19 Jan 2026, 06:30[...]will still render the exhaust turbine a 'pressure turbine'. The fact that a variable opening waste-gate is used, provides the exhaust gases from cylinders to turbine with two paths, when the waste-gate is opened exhaust gas pressure is at atmospheric pressure, and no turbine recovery is possible, When it is closed, exhaust gas is above atmospheric pressure and turbine recovery is possible.
For example, if the pulses are at 25% and the 'constant' pressure is 75% of the total energy that the turbine can convert into mechanical work, opening the waste gate will lead to
a) the engine experiencing almost zero backpressure (it was an important feature for engines with MGU-H).
b) reducing turbine speed and charge air pressure to manageable levels, but not necessarily to zero. This was also the goal of introducing twin-scroll turbos: maintaining a higher turbine speed at low loads and harvesting pulse energy without negative effects on scavenging.
Lower backpressure at equal compressor power increases MEP without a consumption penalty, which is an obvious goal of engineering in this field.
Depend on how you look at it. All energy comes from the burning of the fuel. So if you're talking about the TE of the power unit, it should very much be included. If you only think about the ICE than obviously not, and it will be less.
Most of the quoted TE was never quantified in the sense that it was done in conditions actually used on track, or if the MGUH was involved, or it was a βheroβ TE run in the test cell to maximize bragging rights.wuzak wrote: β20 Jan 2026, 04:53The 1,000hp includes power (up to160hp) from the battery system, so should not be included in the TE calculation.johnnycesup wrote: β20 Jan 2026, 03:53Just to add to the previous discussion, using a common LHV for gasoline (44.3MJ/kg), the previous ruleset had a total fuel energy flow of 1230kW. If the 1000hp rumours are true, that would be a total thermal efficiency of 60,6%, which is pretty incredible.
TE would be around 51%, assuming all power for the MGUK comes from the battery.
It would be ~56% if about half the energy comes from the MGUH to MGUK.
But didn't the maximum power occur when the MGUH was being powered by the battery, and not recovering energy?
But while draining the battery is not a sustanaible mode.
Ok thank you. I see why you guys are wrong. Please have a look at the 2014 engine threads.johnnycesup wrote: β20 Jan 2026, 03:53I'm not the person you're replying to, but there's a 3000MJ/h limit to the fuel energy flow in the regulations. Now MJ/h (unit of mechanical work per unit of time) is obviously a unit of power, so 3000 MJ/h = 833 kW.
So considering the internal combustion engine can burn the fuel perfectly and nothing else is burned (so no oil burning shenanigans), a 470kW output is equivalent to 56,4% thermal efficiency. A bit optimistic IMO
EDIT:
Just to add to the previous discussion, using a common LHV for gasoline (44.3MJ/kg), the previous ruleset had a total fuel energy flow of 1230kW. If the 1000hp rumours are true, that would be a total thermal efficiency of 60,6%, which is pretty incredible.
Bt that's using fuel that is outside the current fuel flow.
It's still utilized for drive. I guess that just means you can't assess the efficiency of a PU by taking an arbitrary point in time.wuzak wrote: β20 Jan 2026, 15:17But that's using fuel that is outside the current fuel flow.
yes