Mystery solved.
https://fr.media.renaultgroup.com/actua ... e3532.html
Shows how little they had to change to get to the split turbo. The axle was already there and likely long enough. They just removed the compressor from the back, shifted the turbine forward the distance of the now absent compressor and connected it to the compressor on the front onto the same axle.AR3-GP wrote: ↑05 Apr 2022, 20:42Interesting. So that's how they can run the MGU-H shaft through the compressor. This solution seems to have more flow losses than the split turbo. The old solution has a boundary layer on the outer diameter and the inner diameters. With the new split turbo layout, there is only the boundary layer on the outer diameter of the compressor inlet piping. There is probably a consequential benefit there.
Or overnight parts from Japan.
You know. The design of that inlet makes a lot of sense if you think about flow losses. You can't compare it to a pipe bend really. The entry is split into sectors that take air from the circumference and not from the centre line. On the circumference has a bigger cross section, thus its a lower air speed before it gradually accelerates to the middle so less turblulent losses.AR3-GP wrote: ↑05 Apr 2022, 20:42Interesting. So that's how they can run the MGU-H shaft through the compressor. This solution seems to have more flow losses than the split turbo. The old solution has a boundary layer on the outer diameter and the inner diameters. With the new split turbo layout, there is only the boundary layer on the outer diameter of the compressor inlet piping. There is probably a consequential benefit there.
Yeah and the split turbo may have theexact same design just on the other side.PlatinumZealot wrote: ↑06 Apr 2022, 15:31You know. The design of that inlet makes a lot of sense if you think about flow losses. You can't compare it to a pipe bend really. The entry is split into sectors that take air from the circumference and not from the centre line. On the circumference has a bigger cross section, thus its a lower air speed before it gradually accelerates to the middle so less turblulent losses.AR3-GP wrote: ↑05 Apr 2022, 20:42Interesting. So that's how they can run the MGU-H shaft through the compressor. This solution seems to have more flow losses than the split turbo. The old solution has a boundary layer on the outer diameter and the inner diameters. With the new split turbo layout, there is only the boundary layer on the outer diameter of the compressor inlet piping. There is probably a consequential benefit there.
It's smart. I have seen this design before though. Smart way to get around a tight bend.
I wonder if Ferrari is using this?
I wasn't referring to losses due to a bend. I was referring to losses due to the secondary wall of the annulus design. Pipe flow losses come from walls. There are two walls in the annulus design of the non-split turbo.PlatinumZealot wrote: ↑06 Apr 2022, 15:31You know. The design of that inlet makes a lot of sense if you think about flow losses. You can't compare it to a pipe bend really. The entry is split into sectors that take air from the circumference and not from the centre line. On the circumference has a bigger cross section, thus its a lower air speed before it gradually accelerates to the middle so less turblulent losses.AR3-GP wrote: ↑05 Apr 2022, 20:42Interesting. So that's how they can run the MGU-H shaft through the compressor. This solution seems to have more flow losses than the split turbo. The old solution has a boundary layer on the outer diameter and the inner diameters. With the new split turbo layout, there is only the boundary layer on the outer diameter of the compressor inlet piping. There is probably a consequential benefit there.
It's smart. I have seen this design before though. Smart way to get around a tight bend.
I wonder if Ferrari is using this?
I said this over on the teams thread, this was a comment from Otmar, that was more of a comment that the PU is no excuse...we can compete. Than it was a factual we're down 10 HP from the best.
And viewtopic.php?p=954073#p954073AR3-GP wrote: ↑05 Apr 2022, 20:42Interesting. So that's how they can run the MGU-H shaft through the compressor. This solution seems to have more flow losses than the split turbo. The old solution has a boundary layer on the outer diameter and the inner diameters. With the new split turbo layout, there is only the boundary layer on the outer diameter of the compressor inlet piping. There is probably a consequential benefit there.