vorticism wrote: ↑05 Jan 2026, 16:43
There seems to be a few surprise freedoms within the turbocharger regs:
https://i.postimg.cc/3N591Byg/turbo-regs.png
F.e. the turbine isn’t demanded to be single-sided, only the compressor is. A dual outlet turbine could provide some new options for wheel ramp profiles and oulet area (think of a double-sided compressor wheel). Also, directionality of flow is not specified, so a radial-outlfow turbine could be pursued. Is the inlet:outet area ratio of a turbocharger turbine considered to be a limiting factor in terms of geometry and packaging?
The periphery of a cylinder has more surface area than its faces. The turbine must fit within a cylinder 40mm long x 100mm dia. Perhaps something like multi-stage expansion can be simulated within one stage by increasing the potential expansion ration. I don't mean this as a strong suggestion, it just seems to be a geometric possibility.

alt link:
https://i.postimg.cc/KjttW0Nt/F126turbineconcepts.jpg
In general there is a looming question of: why is a gap of 7” permitted between the compressor and turbine wheels? And how could it be used. Another thought is it may have been requested by someone who wanted an over-the-shaft compressor inlet similar to previous years' Renault and Ferrari installations, except this time turned inward, presumably.