When a blowdown turbine is attached to an engine it will not reduce power due to exhaust gas flow restriction, since a blowdown turbine is a velocity turbine, not a pressure turbine as is a turbo supercharger. The exhaust restriction imparted by the three blowdown turbines used on the Wright 3350 Duplex Cyclone is equal to a well-designed jet stack system used on a conventional radial engine. However, the blowdown turbines recover about 550 horsepower at METO (maximum continuous except for take-off) power.
Turbo-compounding was used on on several airplane engines after World War II, the Napier Nomad and the Wright R-3350 being examples. In the case of the R-3350, maintenance crews sometimes nicknamed the turbine the "Parts Recovery Turbine" due to its negative effect on engine reliability. Turbo-compound versions of the Napier Deltic, Rolls-Royce Crecy, and Allison V-1710 were constructed but none was developed beyond the prototype stage. It was realized that in many cases the power produced by the simple turbine was approaching that of the enormously complex and maintenance-intensive piston engine to which it was attached. As a result, turbo-compound aero engines were soon supplanted by turboprop and turbojet engines.
Some modern heavy truck diesel manufacturers have incorporated turbo-compounding into their modern designs. Examples include: theDetroit Diesel DD15 engine that claims 5 percent better fuel economy with an additional 50 hp "free" compared to their previous engines, and Scania , in production from 2001.
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