BMW 803

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The BMW 803 was BMW's attempt to build a high-power Aircraft engine by "coupling" two BMW 801's 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]

Contents

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 (shaft engine), at 380 g/kWh (0.63 lb/hp·h), comparable to late generation Turboprop.

As with most coupled engines, the 803 never really worked right, and did not enter production.

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 Bomber") and other large Bomber. The big, 6 engines i.e. TA-400 was in 1942 designed in an "extended long-range version" to attack New-York. The projected range was enough for the distance France to New-York and back again to France, but it was of course never realized. FW used it in single-seat Fighter aircraft design, and it also appeared on several Blohm und 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.


Specifications (BMW 803)


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)
<h3>Components
  • Valvetrain: One intake and one Sodium-cooled exhaust valve per cylinder
  • Fuel system: Fuel injection
  • Cooling system: Liquid-cooled
<h3>Performance
  • Power output: 2 940 kW (3,950 hp)
  • Specific power: 34.3 kW/L (0.75 hp/in³)
  • Compression ratio: 6.5:1
  • Brake specific fuel consumption: 380 g/kWh (0.63 lb/hp·h)
  • Power-to-weight ratio: 970 W/kg (0.59 hp/lb)

See also

Comparable engines

  • Pratt & Whitney R-4360
  • Lycoming R-7755
  • Wright R-3350

Related lists

  • List of aircraft engines

References

Notes

  1. Gunston 1989, p.27.

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9

External links

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