turbo_bird wrote:
I'm still not sure on the theory behind the prechambers though.
The basic idea is to allow a rich mixture in the prechamber, which is lit and then proceeds to ignite a leaner (often too lean for normal spark ignition) mixture in the main chamber. It's usually more fuel-efficient than a normal combustion chamber.
It works just fine for gasoline engines, but it drives various regulated pollutants up very high; mostly oxides of nitrogen (NOx). Last time the prechambers came around predated three-way catalysts, which are helpful for NOx emissions.
A lot of things came and went, not because they weren't useful, but because they weren't practical at the time. Back when aircraft used short exhaust stacks, pilots would trim the fuel and spark until the flames went away and the smoke changed from black to white. That meant the engine was running right on the edge of the detonation zone; the entire fuel/air mix burned without a distinct flame front across the chamber. This increased the effieciency a lot. It was only practical on aircraft engines without exhaust manifolds, running at constant speed. It faded away when aircraft began using exhaust manifolds instead of stacks, mostly in the early 1940s.
The idea came back a few years ago as "Homogenous Charge Controlled Ignition", or HCCI. The engine management system is able to diddle the fuel and spark to the edge of detonation and keep everything under control with sensors and feedback loops.