Wright R-2160 Tornado

{{Refimprove|date=January 2009}}

{{Infobox Aircraft Begin

|name = R-2160 Tornado

|image = Wright_Tornado_R-2160.jpg

|caption = Wright Tornado R-2160

}}{{Infobox Aircraft Engine

|type= Six-row liquid-cooled inline radial engine

|manufacturer= Curtiss-Wright

|national origin= United States

|first run=

|major applications= Republic XP-69

|number built =

|program cost =

|unit cost =

|developed from =

|developed into =

|variants with their own articles =

}}

The Wright R-2160 Tornado was an experimental 42-cylinder, 7-cylinder per row, 6-row liquid-cooled inline radial aircraft engine. It was proposed in 1940 with 2,350 hp (1,752 kW) for experimental aircraft such as the Lockheed XP-58 Chain Lightning, Vultee XP-68 Tornado, and the Republic XP-69.

Specifications

{{pistonspecs

|type=42 cylinder inline radial engine. (6 rows with 7 cylinders in each row)

|bore=4.25 in (107.9 mm)

|stroke=3.625 in (92 mm)

|displacement=2,160 in³ (35.39 L)

|length=96 in (2438 mm)

|diameter=35.5 in (901.6 mm)

|width=

|height=

|weight=2,400 lb (1088.6 kg)

|valvetrain=Single overhead camshaft, Two valves per cylinder

|supercharger= 2 x turbosuperchargers

|turbocharger=

|fuelsystem=Direct injection

|fueltype=100/130

|oilsystem=Dry sump

|coolingsystem=Liquid cooled

|power=2,350 hp (1,752 kW) at 4,150 rpm for takeoff

|specpower=1.08 hp/in³

|compression=

|fuelcon=

|specfuelcon= 0.67 lb/(hp*h) (0.407 kg/(kW*h)) at takeoff

|oilcon=

|power/weight= 1.59 kW/kg (0.97 hp/lb)

}}

See also

References

  • Kim McCutcheon, Tornado: Wright Aero's Last Liquid-cooled Piston Engine {{ISBN|978-0-9710847-0-4}}