Mike Williams
Senior Airman
- 572
- Oct 19, 2006
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My best info is that the US books from Amazon customer orders are on US soil now.
State of:
-1942: Jumo 211J (intercoled version of 211F) ~1150 PS at 5.5 km, 30 min rating, 2400 rpm, the DB 601E a bit less there, but it was allowed for 2700 rpm operation that gave ~1220 PS at 5.5 km for 5 minutes. DB 605A 30 min rating was ~1260 PS at 5.5 km, 2600 rpm (5 min rating at 2800 rpm was banned due to major reliability issues); second half of 1942 also sees Merlin 61 with excellent hi-alt performance, and late 1942 is the time the V-1710 finally gotten the faster turning impeller to narrowly beat the altitude power of the pre-war Merlin III...
- 1943: Jumo 211N - 2500 rpm gave 1170 PS at 5.2 km, 30 min rating; 211P (intercooled 211N) 30 min rating was 1280 PS at 4.6 km (works to around 1150 PS at 5.5 km); DB 605A is still at old values until October of 1943 finally saw the 2800 rpm operation being allowed
- late 1943: Jumo 211R, that to my knowledge never saw service (Jumo 213 production start interferred - corrections are welcomed), faster spinning impeller* than the earlier models at least by judging by a somewhat lower take-off power, 1130 PS at 7.2 km (!!) 30 min power; DB 605A 30 min rating 1020 PS for at that altitude
Jumo 211 engines used 1 min take off power (higher rpm, a bit higher boost than for 30 min next-best setting).
My guess is that lack of 5 min power setting, looking by manuals for engines (past the 211A), were more a reflection of the engine use that were mostly bombers, rather than something to do with suitability of engine for such a bit more aggresive power setting. The perceived weakness in power of 211 vs. 601 was probably just that - a perceived weakness, especially between the start of the war and mid-1942.
* or perhaps a bigger impeller??
Do you know what the features of the Jumo 211R were? My readings of the Ta 154 "moskito" show that repeated analysis of the aircrafts performance showed that it could not deal with the Dehaviland Mosquito unless it were equiped with Jumo 213 engines instead of Jumo 211N.
Do you know what the features of the Jumo 211R were? My readings of the Ta 154 "moskito" show that repeated analysis of the aircrafts performance showed that it could not deal with the Dehaviland Mosquito unless it were equiped with Jumo 213 engines instead of Jumo 211N.
Postage to Europe from the U.S.A. is prohibitive. Not sure why, but the postage to, for instance, Ireland, is more than the cost of the things we send for Christmas.
I supposed the reverse postage from there to here was just as bad and Callum just confirmed that. Interesting that it was ecominical in the 1960's to send things back and forth when there were a lot of ships going back and forth, but it is now way too expensive when it is mostly airplanes.
Well Calum, my Amazon copy is somewhere "in transit." After reading your post, it ws easier to get it from Amazon ... though it won't be autopgraphed, it still has your name on it.
Barometric control of the Föttinger hydraulic coupling sounds good in theory but is woefully inefficient and results in an already thirsty engine becoming more so, i.e. less range plus they suffered from overheating issues of the fluid.Jumo vs DB:
standard supercharger with different speeds vs variable coupling
3 valves per cylinder vs 4
more automatic engine controls on the DB
The DB engines as installed in the Bf 109 employed a dual-coolant circuit - more reliable in the event of battle damage.I am sure I read somewhere that the DB engines had a more efficient pressurised cooling system whereas the Jumo was atmospheric pressure.
Can you supply documentary evidence that the KommadoGerat system was extended to the DB and Jumo? I was only ever aware that this was exclusive to the BMW 801, only. (And cost a fortune to develop!).There are a lot of myths regarding the superiority of the DB engines over Jumo but in reality are not true.
-All the German engines BMW801, DB60x series and Jumo implemented integrated 'kommandogeraet' controls that provided tightly integrated single throttle automatic control of engine power, RPM, propeller pitch, boost and mixture control. These were so advanced they even prevented engine over speed in a dive.
-The DB engines tended to use higher compression ratios, variable speed superchargers. The higher compression ratios with the DB resulted in superior specific fuel consumption figures per shaft horsepower however the Jumo engines tended to operate at lower compression ratios but higher boost levels (at least DB603 versus Jumo 213) this resulted in higher jet thrust that probably made the Jumo 213 the better engine for the same shaft horsepower. The Jumo 213 had better 'ehp' equivalent horse power. The Early DB601/605 engines had access to higher octane fuels due to their association with the Me 109 figher.
DB technology was
-No head bolts, used the cyclinder liner as a giant threaded bolt. This allowed a much larger swept volume, hence DB engines didnt need as much pressure to create power and so had good altitude performance.
-Variable length inlet manifolds ensured end gases were scanvenged and prevented preignition and allowed more mixture.
-infinitely variable speed supercharger.
Jumo technology was
Higher Compression, more jet thrust
Higher RPM
Variable inlet guide vanes for supercharger (copied from Russian engines) to control inlet flow effficiently.
Multispeed superchargers.
Succeeded with intercoolers earlier
Ran well on B4 fuel.
Curiosity question Calum: in your extensive researches for your book did you manage to dig up any material on DB's intriguing Wankel Disc Rotary-Valve cylinder-head conversion for the '601? I vaguely recall it might have been dubbed the 'L' model.Hmmm well I did spend 6 years putting it all in a book to clear up these points.... was rather hoping someone might have read it by now !
1) The Jumos until the 213 dont have an actual "kommandogerat" (my definition of that is ONE single "box" which does everything in ONE unit), prior to the 213
they`re like the DB, in that they have a couple of distributed systems which broadly achieve the same thing as the "kommandogerat", but its not
all stuck into one unit. So the 211 for example has separate boost control and fuel control boxes. They can be described as "single-lever" for the most part,
but this is not achieved by a single-master control box (the kommandogerat).
2) The DB doesnt have a "variable length inlet manifold".
3) The lack of head bolts on the DB does not permit greater swept volume, the limit to engine length and bore size/spacing is always the minimum
gap needed between the cylinders where they meet in the middle, not where the bolts are. The 211 is actually larger in capacity than the 601,
and nearly as large as the 605. I think you`ve got mixed up comparing the very early 210 with the 601.
4) The Jumo does have lower CR, and indeed the DB had higher CR to improve fuel economy and altitude performance, but,
due to other factors this still left the DB with at best equal and usually slightly worse fuel economy than the Jumo.
other points about pressure cooling and valves are correct, except for the assertion that it doesnt matter how many you have because
"american engines only had 2 and were ok". Indeed, and they would have been "even more ok" with 3 or 4.... however its a huge pain
with the valvegear on a radial to have more than 2, so most dont.
Broadly:
601A < Jumo211A (due to very poor "box" type supercharger of the jumo)
601E = Jumo211J (pretty comparable, 211J has much better supercharger)
605A > Jumo211J (605 has slight advantage in swept volume)
605A < Jumo213A (213 is a much later developed, more modern engine, so is naturally a bit better overall)
All Jumo`s had outstandingly good oil systems, which helped them avoid the worst of the bearing troubles which DB experienced.
There is a lot more to it, but in all seriousness if you`re interested in stuff like this you really do need my book!
The Jumo engines had wet cylinder liners (i.e., the coolant directly contacted the cylinder liner). The DB engines had dry liners - the cylinder liner was screwed into the aluminum cylinder block and this was designed so that the cylinder liner was surrounded by aluminum. The wet liner arrangement was better for cooling. DB had thermal problems with the DB601E/F and DB605 - for some time both engines had to be derated. This was likely part of the motivation for the extreme valve overlap on these engines - forcing pure air through the exhaust valves during part of the intake cycle would have provided some extra cooling.DB had pressurized cooling from the 601E on, Jumo from 211F/J. Both available in 1941 although i believe DB was rather mid 41 and Jumo late 41.
Can you supply documentary evidence that the KommadoGerat system was extended to the DB and Jumo? I was only ever aware that this was exclusive to the BMW 801, only. (And cost a fortune to develop!).
Curiosity question Calum: in your extensive researches for your book did you manage to dig up any material on DB's intriguing Wankel Disc Rotary-Valve cylinder-head conversion for the '601? I vaguely recall it might have been dubbed the 'L' model.
Barometric control of the Fottinger hydraulic coupling sounds good in theory but is woefully inefficient and results in an already thirsty engine becoming more so, i.e. less range plus they suffered from overheating issues of the fluid.
Postage to Europe from the U.S.A. is prohibitive. Not sure why, but the postage to, for instance, Ireland, is more than the cost of the things we send for Christmas.
I supposed the reverse postage from there to here was just as bad and Callum just confirmed that. Interesting that it was ecominical in the 1960's to send things back and forth when there were a lot of ships going back and forth, but it is now way too expensive when it is mostly airplanes.