Turbo-Compound
radial engine. A power recovery turbine with silver blades is shown in slight center left. Early work on exhaust power-recovery turbines began in the 1940s. By the 1950s, blowdown turbines had become a characteristic feature of the last generation of long-range American piston airliners, particularly those powered by turbo-compound Wright R-3350 engines. The
Rolls-Royce Crecy was among the early aircraft engines investigated with an exhaust power-recovery turbine. A turbine geared to the rear of the crankshaft took exhaust from the four exhaust manifolds, providing enough power to overcome the consumption of the supercharger and assist the crankshaft. This arrangement projected a 15 to 35 percent fuel-economy advantage over the
Merlin, depending on loading and altitude. Turbo-compounding was used on several
airplane engines after
World War II, including the
Napier Nomad and the
Wright R-3350. Wright sources stated that the complete exhaust system of the turbo-compound
Wright R-3350 Duplex-Cyclone was equivalent to a well-designed jet-stack installation in the way it influenced engine operation. Near the end of the exhaust stroke, exhaust pressure dropped below atmospheric, rather than creating harmful
Back pressure, thereby aiding scavenging, while the turbo-compound system recovered about at cruise settings and about at takeoff power over a similar non-turbocompounded R-3350. Turbo-compound versions of the
Napier Deltic,
Rolls-Royce Crecy, and
Allison V-1710 were constructed, but none were developed beyond the prototype stage. A turbo-compound
Rolls-Royce Griffon was likewise proposed, though it remained an unbuilt paper project. Turbo-compound aero engines were later supplanted by
turboprop and
turbojet engines. Some modern heavy-truck diesel manufacturers have incorporated turbo-compounding into their designs. Examples include the
Volvo D13TC engine, the
Detroit Diesel DD15, and Scania's 11-liter DTC1101 turbocompound diesel, as used in the
R113.400. Starting with the 2014 season, Formula One adopted 1.6-liter turbocharged V6 hybrid power units. These incorporated a motor generator unit–heat (MGU-H), defined by the FIA as an electrical machine linked to the exhaust turbine of the pressure-charging system, and a motor generator unit–kinetic (MGU-K) linked to the drivetrain as part of the energy recovery system. The MGU-H recovered energy from the exhaust-driven turbocharger as electrical energy, which could be stored in the energy store, used to power the MGU-K, or used to control turbocharger speed and reduce turbo lag. ==List of types==