The FW 190 could carry a 300 Ltr. drop tank, that was pressurized by supercharger bleed air. Fuel was transferred from the drop tank to the (292 Ltr.) Rear Main Tank, when the quantity of that tank was below 240 Ltr. Otherwise it was inhibited by a float valve. An electrical pump was built into the ETC 501 carrier rack. This pump was called EP-1 E and was meant to keep the pressure up, when flying at low manifold pressure and the supercharger was delivering at or below ambient pressure. The main tanks were not pressurized, but the drop tank was and so fuel transfer took place eventhough the EP-1 E was not running. As long as the supercharger bleed air was above ambient. Of course this bleed air connection had a check valve and a pressure relief valve.
I am interested in data about the EP-1E.
I cannot find anything about it. Not even a single actual photo.
I would like to know it's output pressure and capacity.
I am interested in data about the EP-1E.
I cannot find anything about it. Not even a single actual photo.
I would like to know it's output pressure and capacity.