Which country designed the best engines for WWII?

Which country designed the best aircraft engines for WWII?


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Be advised that you're replying to a post from 2008 and to a member who was banned a long time ago.
 
I was replying to red admiral's post..I believe he is not banned..The thread is old but still alive

Thank you for the link. Although a a bit long it is nowhere near long enough to cover the subject thoroughly and the author seems a bit biased or is pushing a certain view point.
The US did start from behind and the gift of the British jets was an incredible benefit. However no mention is made of the Westinghouse J-30 engine or the GE J-35 Axial engines. Both of which owed little to the British engine/s.
One should also note that the Americans were flying quite a number of different pressurized piston powered air liners in the late 40s eve if the pressure differential wasn't as great as it would be on the jets. In fact the US had lead the way on Pressurized transports.
First being the Boeing 307.


Unfortunately for the British aircraft and jet engines had reached such a state of complication that a few smart people with brains were no longer enough to deliver a working product in a reasonable amount of time. You needed large numbers of not so smart people (but no where near dumb) working under them to sort out the thousands if not tens of thousands of little problems. The Americans had such a work force, the British did not, in large part just due to the size of the populations of both countries.
 
The key powers US, Germany, Japan and England all made great engines.
Speaking for liquid cooled Germany, Allison and Merlin in that order.
US or Germans Liquid cooled engines were just more rugged.
Merlin was called the Watchmakers Engine..it performed well because of a great Supercharger system that Allison never quite caught up.
Germany had the variable Supercharger which was a huge asset.

Radials ..everyone had a good radial.
 

Would you care to post the time/s to overhaul for the German Liquid cooled engines?
Or other evidence of how rugged they were?

The variable supercharger (actually variable drive) was not quite the huge asset it is made out to be. It was variable between a high and low limit that wasn't that much different than some two speed superchargers (although it did eliminate the "notch") and if the compressor is crap it doesn't matter what kind of drive mechanism you use. The 109 for most of it's career had good altitude performance because they stuck a big engine in a small plane. Not because the engine was a technological marvel.
 
Metropolitan-Vickers F.2 never successfully passed a PFTR nor did it ever enter production... its an example of what we call a "failed attempt" to build a axial flow turbojet engine...

In fact M-V F.2 was developed into 3,500 lb F.2/4 Beryl, first ran Jan 1945 and passed a 100-hour type test that year. Built in small numbers, IIRC around 30, and in the end produced 4,000 lb thrust. Powered Saunders-Roe S.R./A.1 flying boat fighter prototypes.

Juha
 
Mike Nixon of Vintage V-12s has told me the DB 601/605 has very good internals. The biggest problem was feeding them NO2 and over-boosting them to get powers that weren't conductive to long engine life. You can only push powers so high until something breaks and they needed more power without the time to strengthen the engine sufficiently.
 
The overhauls / TBOs of the db60x series were on the order of 100-150hrs. Whereas the overhauls of late series Allisions were 700hrs in combat zones, in training, a thousand hours or more. Merlins were somewhere in between, about 400hrs.

The Db601/5 is a large displacement engine which when ran at high power levels was very stressed. It weighs about the same as a Allison or Merlin, and is 33L or 35L displacement, as compared to the Allison or Merlin which is 27L displacement.

A lot of the difficulty's with high power levels have to do with the fuel octane rating the engine is designed for. As the surface area of the piston tops increase, and the Db601 and especially the 605 has bigger pistons than the Allison or Merlin, the difficulty with an even fuel air mix becomes greater. Resulting in detonation more easily as lean/hot spots develop across the piston top. DB mitigated this somewhat with direct fuel injection, increasing fuel/air homogenicity, but still had issues in their pushing of the cylinder compression to the max possible with 87oct fuel - resulting in pistons with holes in them, burnt valves, and compression losses of all kinds.

Really, a lot of attention has been paid to the variable supercharger on the db601/5, but the real design genius was in the direct fuel injection and RPM/boost matching system. And that cognitive error goes back even to the wartime years. The variable supercharger was simply effective, cheap, and light. Nothing too special about it. As SR says, the 109 was a very small airplane with a very big engine, and that's where it got its performance.
 
The maximum emergency time at power with these systems engaged was actually quite a bit LONGER than when at 1.42ata, which remained through the war the maximum boost level permitted without MW50 or other system like GM-2.

Again, this is because the limiting factor was not structural, but rather chemical - read: detonation - as the engine was simply designed for 87oct fuel (excepting very minor variants) and the design pushed the limitations of what that fuel could provide in the way of maximum permissible supercharger boost. As it approached the absolute maximum permissible boost, the safety margin between normal combustion and detonation became razor thin. This was far less of an issue for late (or even mid) war allied aircraft which had the advantage of higher octane fuel (and the more clumsily operated but more adjustable fuel mixture and prop control systems which were not tailored for a specific fuel octane).

 
For me this is an easy one and i can even whittle it down to just two main types....
1) The British/US Rolls Royce PV12/Packard 1650 "Merlin" inlines.
2) The Pratt & Whitney R2800 radial.

Honourable mentions include Daimler Benz DB series. The Bristol Hercules & Centaurus radials. The Junkers Jumo 200 series inline. BMW radial & Napier Sabre inlines. Curtis inline & Wright Cyclone radial. Maybe some Nakajima's but they were woefully underpowered.....
I'd mention Russia but they were all just copies of copies of copies and not even very good at that.
 
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I think your quote about Sabre engines is a little harsh. Yes early Napier's were very unpredictable and suffered a litany of problems especially with fire during engine start, and a few other minor gremlins that were concerning the RAF. But at that time Britain had to work with what it had, and later Sabre variants (Especially Tempest V's powered by the Sabre ll) Had almost all problems eradicated, and many Luftwaffe pilots stated the Tempest was one of, if not the best fighter the allies possessed towards the end of the war. Further development of the British H-24-cylinder, liquid-cooled, sleeve valve, piston aero engine, designed by Major Frank Halford and built by D. Napier & Son, would surely have given the Merlin or Griffon serious consideration and respect. As for Britain having just a few types of modern powerful aero engines i think is irrelevant. From inline to radials, Britain could hold its own with any other country during ww2. Plus a lot of people forgey the Napier Sabre H-24 Mkl was first tested way back in 1939.
 
[QUOTE="As the surface area of the piston tops increase, and the Db601 and especially the 605 has bigger pistons than the Allison or Merlin, the difficulty with an even fuel air mix becomes greater. Resulting in detonation more easily as lean/hot spots develop across the piston top. DB mitigated this somewhat with direct fuel injection, increasing fuel/air homogenicity, but still had issues in their pushing of the cylinder compression to the max possible with 87oct fuel - resulting in pistons with holes in them, burnt valves, and compression losses of all kinds.[/QUOTE]

References please.
 
Look at the Luftwaffe technical notes about maximum permissible boost on the Db605 and the 1.3ata limit (instead of 1.42) until piston tops could be reinforced, for starters. As pistons were being burned through. They did eventually solve this but I would note that the solution was simply to add more mass to the top of the pistons...
 

The thicker pistons just meant it took a few more hours for the detonation to eat through the piston crowns.
 
Exactly,
But also more mass also means the piston sinks heat better, theoretically
Tradeoff being increase in reciprocating mass and the stress is equal to the square of the engine speed times the mass being reciprocated...
 
Exactly what ?

Hardly a solution then is it ? - and also totally unrelated to the piston crown area being the case, which was your proposition - for which you`ve provided no evidence.
 
As the piston creates a vacuum it generates vortices of distubed air at the top of it in the low pressure zone, increases in diameter of the piston results in bigger low pressure area, means increases in inhomogenicity, well known general fact in engine building. Direct injection increases fuel air homogenization as less volume to traverse before combustion area (you don't get lean cylinders etc) which is another beneficial effect and helps prevent detonation.

Ok go talk to an engine builder if you're more interested in specifics on general principles. Sorry not every piece of knowledge is able to be historically sourced, except maybe extrapolated from texts in engine design
 
The thicker pistons just meant it took a few more hours for the detonation to eat through the piston crowns.
I burned through many pistons on two strokes, I know it is different technology but when the process starts it takes seconds or minutes not hours.
 

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