Rolls-Royce RB211-22 Turbofan Engine, Cutaway

Image of this Object

This is the first foreign-made engine chosen as the basic power plant for a major U.S.-built airliner, the Lockheed L-1011 TriStar, receiving its certification from the Federal Aviation Administration in 1973 for use on that three engine aircraft. In addition, it powered some models of the Boeing 747 transport.

The RB211 differed from other engines in its class in having three instead of two shafts. Each shaft has a compressor on its forward end and a turbine on its aft end. This design permitted each compressor to run nearer its optimum speed and efficiency and reduced the number of blades and other parts required in the engine. The static thrust varied from 160 KN (36,000 pounds) to 245 KN (55,000 pounds).

This RB211-22 engine powered the Lockheed L-1011 TriStar. It has been cutaway to show the relationship of the internal parts.

Gift of Rolls-Royce Ltd

Physical Description:
Type: Turbofan, 3-shaft
Thrust : 187,000 N (42,000 lb)
Compressor: Single-stage fan, 7-stage intermediate pressure, 6-stage high pressure
Combustor: Annular chamber
Turbine: Single-stage axial high pressure, single-stage intermediate pressure, 3-stage low pressure
Weight: 3,267 kg (7,203 lb)

Country of Origin
United Kingdom

Designer
Dr. S. G. Hooker
Manufacturer
Rolls-Royce Ltd. (Derby, U.K.)

Date
1973

Location
National Air and Space Museum in Washington, DC
Exhibition
America by Air

Type
PROPULSION-Turbines (Jet)

Materials
Metal
Dimensions
3-D: 303.3 × 217.2cm, 4170.8kg (119 7/16 × 85 1/2 in., 9194 15/16lb.)
Support: 285.8 × 156.2 × 243.8cm (112 1/2 in. × 61 1/2 in. × 96 in.)

This is the first foreign-made engine chosen as the basic power plant for a major U.S.-built airliner, the Lockheed L-1011 TriStar, receiving its certification from the Federal Aviation Administration in 1973 for use on that three engine aircraft. In addition, it powered some models of the Boeing 747 transport.

The RB211 differed from other engines in its class in having three instead of two shafts. Each shaft has a compressor on its forward end and a turbine on its aft end. This design permitted each compressor to run nearer its optimum speed and efficiency and reduced the number of blades and other parts required in the engine. The static thrust varied from 160 KN (36,000 pounds) to 245 KN (55,000 pounds).

This RB211-22 engine powered the Lockheed L-1011 TriStar. It has been cutaway to show the relationship of the internal parts.

Gift of Rolls-Royce Ltd

Physical Description:
Type: Turbofan, 3-shaft
Thrust : 187,000 N (42,000 lb)
Compressor: Single-stage fan, 7-stage intermediate pressure, 6-stage high pressure
Combustor: Annular chamber
Turbine: Single-stage axial high pressure, single-stage intermediate pressure, 3-stage low pressure
Weight: 3,267 kg (7,203 lb)

Country of Origin
United Kingdom

Designer
Dr. S. G. Hooker
Manufacturer
Rolls-Royce Ltd. (Derby, U.K.)

Date
1973

Location
National Air and Space Museum in Washington, DC
Exhibition
America by Air

Type
PROPULSION-Turbines (Jet)

Materials
Metal
Dimensions
3-D: 303.3 × 217.2cm, 4170.8kg (119 7/16 × 85 1/2 in., 9194 15/16lb.)
Support: 285.8 × 156.2 × 243.8cm (112 1/2 in. × 61 1/2 in. × 96 in.)

ID: A19820072000