The BMW 803 was BMW's attempt to build a high-power aircraft engine by "coupling" two BMW 801s back-to-back driving contra-rotating propellers. The result was a 28-cylinder 4-row radial engine, like the contemporary American Pratt & Whitney R-4360 Wasp Major, but unlike the American engine, due to cooling concerns, the 803 engine was liquid cooled.[1]
[edit] Design and development
One problem with scaling up any engine design is that eventually a point is reached where the crankshaft becomes a major engineering challenge. This was a problem that affected almost all engines of the 2,500 hp (1,900 kW) class, including BMW's own 18-cylinder BMW 802 project. For the 803 the engineers decided to avoid this problem by simply not using a common crankshaft, and driving a set of independent contra-rotating propellers. The front engine drove the front propeller directly, while the rear engine drove a number of smaller shafts that passed between the cylinders of the front engine before being geared back together to drive the rear prop. This layout resulted in a rather large gearbox on the front of the engine, and the front engine needing an extended shaft to "clear" the gearbox.
With no common crankshaft all of the accessories had to be powered by one engine alone, in this case the rear engine. The supercharger itself used up several hundred horsepower, so the rear prop ended up delivering considerably less power than the front one.
The engine weighed a staggering 2,950 kg (6,490 lb) dry, and 4,130 kg (9,086 lb) fully loaded, displacing a massive 83.5 litres. For all this weight it delivered 3,900 PS (metric hp) (2,868 kW). Although this made it the most powerful German engine design, its power-to-weight ratio was not at all impressive, at about 0.60 hp/lb, comparing rather poorly with other large designs like the Junkers Jumo 222 at 1.04 hp/lb. Specific power was likewise poor, at about 34.4 kW/l, compared to the 222's 40 kW/l, as was specific fuel consumption, at 380 g/kWh (0.63 lb/hp·h), comparable to late generation turboprops.
As with most coupled engines, like the earlier Daimler-Benz DB 606 "power system" of two mechanically coupled DB 601 inverted V12 inlines driving a single propeller shaft, but which was produced for front-line use, the 803 never really worked right on the test bench, and did not enter production.
[edit] Aircraft projected for BMW 801/802/803
The engine was intended to be used only on the largest of designs, notably the Focke-Wulf Fw 238, the Focke-Wulf Ta-400 6 engine (the so called "New-York or Amerika Bombers") and other large bombers. The big, 6-engined Ta 400 was in 1942 designed in an "extended long-range version" to attack New York City. The projected range was enough for the round trip from France to New York, but it was of course never realized. FW used it in single-seat fighter design, and it also appeared on several Blohm & Voss designs as well. None of these designs was particularly inspiring, and as the engine never matured the project was cancelled. A single example remains in the Deutsches Museum.
[edit] Specifications (BMW 803)
The large gearbox at the front is evident. The display on the left of the engine shows how the overhead cams were driven off the crank via a series of driveshafts
General characteristics
- Type: 28-cylinder four-row radial engine
- Bore: 156 mm (6.14 in)
- Stroke: 156 mm (6.14 in)
- Displacement: 83.5 L (5,095 in³)
- Diameter: 160 cm (63 inches)
- Dry weight: 4 130 kg (9,100 lbs)
Components
Performance
[edit] See also
- Comparable engines
- Related lists
[edit] References
[edit] Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
[edit] External links
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