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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.
Date
1973
Country of Origin
United Kingdom
Type
PROPULSION-Turbines (Jet)
Designer
Dr. S. G. Hooker Manufacturer
Rolls-Royce Ltd. (Derby, U.K.) 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)
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.) Materials
Metal Inventory Number
A19820072000
Credit Line
Gift of Rolls-Royce LtdNational Air and Space Museum, Smithsonian Institution.
Data Source
National Air and Space Museum
Restrictions & Rights
Open Access (CCO)
For more information, visit the Smithsonians Terms of Use.