Shortround6
Lieutenant General
A lot to unpack here and may take several tries.
The Change from the letter "B" to the letter "D" signifies the addition of a hydraulic pump device for the Hispano-Suiza/Hamilton variable pitch propellers. And that pretty much gets us up to the 470kg engines.

The British didn't even have 100/130 fuel in the summer of 1940. Or more accurately, they had some but they didn't quite know were it was. They had fuel that was 100 octane lean and it was better than 100 octane running rich but they didn't quite know how much better because the Performance Number scale (PN) had not be developed yet and test procedures had not been developed yet. They might have some batches of fuel that would test to 100/130 once they had the scale and procedures and other batches that would test at 115-120.
US Fuel was 100/100???. when tested later there were few batches that actually performed worse running rich than running lean. Like 100/98.
1940 was a really big year for aviation fuel for the Allies. It also took a lot of 1941 to sort through things and come up with acceptable standards for both countries.
The Swiss were not interested in building either planes or engines by the hundreds. Which makes tooling up for small scale production easier and you don't need anywhere near the number of people in the shop/s.
There is also a problem with trying to improve engines and aircraft while simultaneously trying to equip a factory for mass production. Maybe you can buy and install 80% or 90% of the machine tools with no problems but some times you have to wait for certain machines to be delivered or you have order one or two new machines if you change certain parts too much late in the development process. RR did all of the development work and most of the small scale production work at headquarters. The more outlying factories built engines in large production runs/batches.
Famous story about P&W and the Napair Sabre engine. Napier, with the aid of Bristol (forced at practically bayonet point) had figured out the 'secret' to making sleeve valves. Now to make the sleeve valves in the quantity desired at the quality desired (scrap rate) they decided they needed 6 (?) large centerless grinders from a US company. The Grinders were found, packed and shipped on the Queen Mary (?) for rapid shipment to England where they were unloaded, sent to Napiers and all was well in sleeve valve land.
Things were not so good back in the USA where it took Strand (the Grinder company ?) about 6 weeks to build/replace the grinders and the completion of the P&W Kansas city plant, dedicated to making the R-2800 C series engines (P-47M & N, F4U-4s, and F8-1) was delayed 6 weeks and a 6 week delay might have meant several hundred fewer R-2800 engines of those types in 1944.
even the US did not have an inexhaustible supply of machine tools.
Had H-S had a problem. Too much had rested on Birkigt's shoulders. He was not only responsible for dozens of engine designs, he designed much of special tooling to make the engines. When he "retired" in 1936 they needed people to design any new tooling and going to 3 or 4 valve heads was going to require a lot of new tooling. It was possible to perform some the valve seat work on the V-12 engines using some of the machinery that Birkigt had designed to make the WW I V-8 engines.
This turns into a real problem with 12Z engines as there not a lot of agreement as to what was changed and in which factories, at east in English sources.
A lot also depends on when/where the stabilization of the lines takes place. H-S was evacuating machinery to a factory just north of the Spanish border and trying to set up a factory in tunnels outside of Bordeaux. So do you have 3 factories or 2 or sort of two 3/4 factories indifferent places?
That is indeed significant, but the Swiss achieved it in 2 years, and for all their skill, there just aren't that many Swiss (and even fewer as a percentage of their industrial base, working on aircraft engines).
It seems like the 12Y varied a fair bit in weight, with early versions weighing around 415-440 kg.
The older 12Y's had a letter code. Which changed a bit in 1932. In 1931 a "c" in the string of letters meant 'compressor' or supercharger. In 1932 they shifted to "s" meaning supercharged to about 4000 meters. If there was a "g" instead of the "s" the engine used a 200 mm impeller in the supercharger instead of 240mm impeller and was rated at 2000 meters instead of 4000. An engine than neither the "s" or the "g" had no supercharger. The letter "r" meant reduction gear. so the 415 and 440 kg engines had no superchargers,That is indeed significant, but the Swiss achieved it in 2 years, and for all their skill, there just aren't that many Swiss (and even fewer as a percentage of their industrial base, working on aircraft engines).
It seems like the 12Y varied a fair bit in weight, with early versions weighing around 415-440 kg. The 12Y-31 in the original MS.406 weighed 468 Kg, and the 12Y-51 which was the original basis for the YS-2, weighted 492 kg. So which of these are comparing the YS-2 with? I couldn't find the weight for the YS listed.
The Change from the letter "B" to the letter "D" signifies the addition of a hydraulic pump device for the Hispano-Suiza/Hamilton variable pitch propellers. And that pretty much gets us up to the 470kg engines.
Yes, and they flying a Prototype F4U in 1940. Lets not go into the American flat 12s and the Lycoming IV-1430.But the important bit is that the 12Z was already at least at a late enough of a stage to fly prototype aircraft with.
No they did not.The French apparently had 100/130 fuel by the way, I don't know if that was coming from the British or what.
The British didn't even have 100/130 fuel in the summer of 1940. Or more accurately, they had some but they didn't quite know were it was. They had fuel that was 100 octane lean and it was better than 100 octane running rich but they didn't quite know how much better because the Performance Number scale (PN) had not be developed yet and test procedures had not been developed yet. They might have some batches of fuel that would test to 100/130 once they had the scale and procedures and other batches that would test at 115-120.
US Fuel was 100/100???. when tested later there were few batches that actually performed worse running rich than running lean. Like 100/98.
1940 was a really big year for aviation fuel for the Allies. It also took a lot of 1941 to sort through things and come up with acceptable standards for both countries.
The Swiss were not quite as backwards as it might seem. They built a lot of precision machine tools for export. They had the first stationary gas turbine engine (electrical generation) and built their own electric locomotives and steam engines. They also had a small company called Oerlikon and few other gun companies, like Sig.France had a vastly larger and more developed aviation industry, population, much more resources in terms of raw materials, power etc., better available fuel etc.
The Swiss were not interested in building either planes or engines by the hundreds. Which makes tooling up for small scale production easier and you don't need anywhere near the number of people in the shop/s.
There is also a problem with trying to improve engines and aircraft while simultaneously trying to equip a factory for mass production. Maybe you can buy and install 80% or 90% of the machine tools with no problems but some times you have to wait for certain machines to be delivered or you have order one or two new machines if you change certain parts too much late in the development process. RR did all of the development work and most of the small scale production work at headquarters. The more outlying factories built engines in large production runs/batches.
Famous story about P&W and the Napair Sabre engine. Napier, with the aid of Bristol (forced at practically bayonet point) had figured out the 'secret' to making sleeve valves. Now to make the sleeve valves in the quantity desired at the quality desired (scrap rate) they decided they needed 6 (?) large centerless grinders from a US company. The Grinders were found, packed and shipped on the Queen Mary (?) for rapid shipment to England where they were unloaded, sent to Napiers and all was well in sleeve valve land.
Things were not so good back in the USA where it took Strand (the Grinder company ?) about 6 weeks to build/replace the grinders and the completion of the P&W Kansas city plant, dedicated to making the R-2800 C series engines (P-47M & N, F4U-4s, and F8-1) was delayed 6 weeks and a 6 week delay might have meant several hundred fewer R-2800 engines of those types in 1944.
even the US did not have an inexhaustible supply of machine tools.
Had H-S had a problem. Too much had rested on Birkigt's shoulders. He was not only responsible for dozens of engine designs, he designed much of special tooling to make the engines. When he "retired" in 1936 they needed people to design any new tooling and going to 3 or 4 valve heads was going to require a lot of new tooling. It was possible to perform some the valve seat work on the V-12 engines using some of the machinery that Birkigt had designed to make the WW I V-8 engines.
This turns into a real problem with 12Z engines as there not a lot of agreement as to what was changed and in which factories, at east in English sources.
A lot also depends on when/where the stabilization of the lines takes place. H-S was evacuating machinery to a factory just north of the Spanish border and trying to set up a factory in tunnels outside of Bordeaux. So do you have 3 factories or 2 or sort of two 3/4 factories indifferent places?