The figures posted in this thread show a setting of 1,58 ata for the low gear and 1,65 ata for the high gear - but as far as I understand it shouldn't be used in high gear and the engine should be at 1,65 ata when used (and not 1,58 ata).
The two stage supercharger is not set by the pilot. It is an automatic function that kicks in when the ambient pressure drops and increased pressure is required to feed the motor.
I'm new to the forum and a bit confused about the subject. In the flight manual of the Fw 190 A is written that the "increased emergency power" should only be used in heights up to 1 km. It also states that the engine runs at 1,65 ata and consumes 70 litre of C3 in 5 minutes at "increased emergency power".
It should not be used BELOW 1 km.
Can someone tell more about this ? Was the usage only restricted in early versions (in the A5) and a changed system without these restrictions installed to later versions (as the A8) ? Are the restrictions posted in the manual only for the A5 ? The manual is the "Bedienungsvorschrift-Fl Fw 190 A-1 bis A-8 L.Dv.T. 2190 A-1 bis A-8/Fl".
Yes the FW-190A went thru several engines. The BMW801C is found in the FW-190A thru FW-190A2. The BMW-801D is found in the FW-190A3 thru FW-190A8. The BMW 801D2 recieved several upgrades during it's lifespan including an increase in compression ratio.
The engine operating restrictions were changed throught the lifecycle of the design just as allied engines did as well. All the 801 series radial motors were fuel injected.
Original Engine restrictions are:
1.32ata @ 2400 U/min for 30 minutes (climb and combat power)
1.42ata @ 2700U/min for 3 minutes (emergency power)
The FW-190A5 was "derated" to operate 1.58ata/1.65ata @ 2700U/min for 10-15 minutes IF it was equipped with C3 "emergency power". The C3 system injected fuel directly into the supercharger NOT to burn it in the engine but to use it to keep the heads cool. Same principal as MW-50 and Water injections systems found on LW and Allied Aircraft. It did not actually "boost" the manifold pressure. It just allowed the engine to run at higher power settings for longer periods of time.
Otherwise the FW-190 power restrictions were the same as the Previous FW-190's.
The FW-190A8 was "derated" to operate 1.58ata/1.65ata for 10 minutes WITHOUT any other system installed. Just the basic BMW 801D2.
With the C3 "emergency power" it could operate 1.58/1.65ata "as long as the emergency lasts" or until your fuel ran out. This is why a 115 liter internal auxilary tank is offered as kit in the FW-190A8. A similar 115 liter tank was installed when the FW-190A8 was equipped with GM-1 NOX.
The 115 liter tank was not a popular installment.
As Crumpp already pointed there was a difference in the fuel injection beween the A5 and the A8, are there other differences in the system as well ?
No as far as I can tell that is the only difference.
You have to purchase the individual FW-190 Flugzeug-Handbuch.
Crumpp