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This does not sound like as airframe related problem to me...
Well I don't know but then I'm neither an aero engine nor airframe engineer.
I can only assume that Nallinger,as a director of Daimler Benz, was and knew what he was talking about.
In the minutes of the meeting he says,on several points,that other airframe manufacturers agree with Daimler Benz and take a similar position as regards Messerschmitt. Of course it may be that Nallinger and the engineers from those other companies were all wrong and that you know something now that they didn't then.
The DB 603 installation in the Me 410 was a subject of this meeting because it was causing problems,not trouble free. In a meeting in March 1943 there were problems reported,particularly with low oil pressure. There were also problems with the radiators. General Vorwald reported that cooperation between Messerschmitt and Daimler Benz was "very bad."
4. The DB 605 was larger then the DB 601 this lead to significant problems with the first two sparking plugs at the front (only in the airframe of the Bf 109 ), because they overheated and new cooling solution must be developed.
No it was not larger. It's basically an up-bored the DB 601E (mighty 4 mm larger cylinders, booo-hoo!).
Exactly.Lol other airframes could produce a oilpressure of 2.6 ata, this is a home made problem of Messerschmitt and the Bf 109 and not from DB.
Lol other airframes could produce a oilpressure of 2.6 ata, this is a homode problem of Messerschmitt and the Bf 109 and not from DB.
Also the Bf 109 G was very clearly a step back from aerodynamics compare the F model. The F-model was much cleaner then the G model.
Only the Erla hood and later the Bf 109 G14 and K-4 were near back to the clean aerodynamic of the F-model!
Anyway the Bf 109 G and K model had also other significant disadvantages compare to the othe topfighters at 1944 and 1945.
The Bf 109 wasn't good at the sticks at highspeed, it was very difficult to fly a Bf 109 G or K at the vertical in high speed turns.
The Bf 109 G was significant outclassed at diving (speed)
and also it was difficult to handle a highspeed dive and come out with significant control because at highspeed diving it was a real beast at the sticks.
Thje Bf 109 G was in a disadvantage from speed, altitude, diving
and she was much more worse to the sticks then for example a P51, P47, Spitfire or F4U-4,
the big advantage was it's acceleration and climb performance but that wasn't by far enough at 1944 and 1945!
That what was Nallinger was claiming. Other airframes - like? Oh, you must mean the He 177. Well that was indeed, trouble free and in direct contrast to those flawed Messerschmitt aiframes.
You should read some specs for example:
Kurfurst - Your resource on Messerschmitt Bf 109 performance
The DB 605 was larger then the DB 601, significant at the lengths. (also with crankshaft)
I cannot see how a airframe should be responsible for a low oil pressure, wasn't the oil pressure provided by the oil pumps which belonged to the motor?There were main problems with the airframe of the Bf 109 G with the DB 605. (Also there were homemade problems from DB itself)
1. DB maintains an Oilpressure of 2.6 technical atmosphere (today Pascal/at) in the airframe by using a DB 605.
The Bf 109 G and K could only reach 2.3 at the whole war.
2. The oil whizzer of the Bf 109 G for the DB 605 was crap at the beginning and much to small, this problem needed a long time for fixing through the small airframe.
3. The pressure retention valve (comes from Messerschmitt)of the Oil tank was also crap at the beginning and couldn't be fixed till end of 1943
4. The DB 605 was larger then the DB 601 this lead to significant problems with the first two sparking plugs at the front (only in the airframe of the Bf 109 ), because they overheated and new cooling solution must be developed.
Also stona has posted the main criticism from Prof. Nallinger and DB.
I cannot see how a airframe should be responsible for a low oil pressure, wasn't the oil pressure provided by the oil pumps which belonged to the motor?
If the oil tank is too small and oil cooler too small , or air flow thru the oil cooler insufficient, the oil temperture will run higher, which will result in lower oil pressure.I cannot see how a airframe should be responsible for a low oil pressure, wasn't the oil pressure provided by the oil pumps which belonged to the motor?
Cimmex
Talking about the DB605 and here is the horseshoe shaped oil tank just in front of the engine around the reduction gear and the oil cooler below the motor in the lower engine cowling. All suction and circulating oil pumps are inside the motor and driven by the motor. So please explain how the airframe was responsible for a bad lubrication.This engines consumed a lot of oil during the flight. I don't have at the moment the precise specs, but a Bf 109 carried something about 60 Liter oil at the oil tank. The oil was permantly circulated first to the oil cooler and second from the oil tank to the engine to replace the consumed oil.
There was a lot of oil circulation outside the engine and inside the airframe.
Edit:
To make it more precise:
With the oil tank I don't refer to an engine oil tank (because the DB engines had a dry sump and no oil basement), it was a normal tank in the fulsage or wing.
So you have the circulation between engine and oil cooler and engine and oil "replacement tank" and here was also a problem with the pressure retention valve.
This all has not much to do with the oil pumps in the engine.