Wednesday, December 03, 2008

AI-22

Origin
Russia

Program Status:
Under Development

Contractor/s
Ivchenko-Progress
Motor Sich

Description: The AI-22 is a turbofan engine derived from DV-2 engine core and designed to power the next-generation short-range airliners Tu-324 and Yak-48. The AI-22 modular design consists of 10 modules with highly developed monitoring and diagnosis systems to ensure on-condition operation. The AI-22 by-pass engine is provided with FADEC control system and rated at 8,421-lb at takeoff.

Specifications
Dimensions: Height 1,548 mm, Length 3 m, Width 1,398 mm

Weights: Dry Weight 765 kg (1,687 lb)

Engine/s Performance: Contingency Thrust 4,340 kg (9,568 lb), Max Cruise Thrust 775 kg (1,709 lb), Max Takeoff Thrust 3,820 kg (8,422 lb)

Other: Service Life (Flight Hours) 40,000

Image Gallery

Internet Resources
ivchenko-progress.com

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)

Last Updated: Saturday, November 22, 2008

Leave Feedback >>