Active magnetic bearings provide revolutionary advantages for gas turbine engine rotor support. These advantages include tremendously improved vibration and stability characteristics, reduced power loss, improved reliability, fault tolerance, and greatly extended bearing service life. The marriage of these advantages with innovative structural network design and advanced materials utilization will permit major increases in thrust-to-weight performance and structural efficiency for future gas turbine engines. However, obtaining the maximum payoff requires two key ingredients. The first is the use of modern magnetic bearing technologies such as innovative digital control techniques, high-density power electronics, high-density magnetic actuators, fault-tolerant system architecture, and electronic (sensorless) position estimation. This paper describes these technologies and the test hardware currently in place for verifying the performance of advanced magnetic actuators, power electronics, and digital controls. The second key ingredient is to go beyond the simple replacement of rolling element bearings with magnetic bearings by incorporating magnetic bearings as an integral part of the overall engine design. This is analogous to the proper approach to designing with composites, whereby the designer tailors the geometry and load-carrying function of the structural system or component for the composite instead of simply substituting composites in a design originally intended for metal material. This paper describes methodologies for the design integration of magnetic bearings in gas turbine engines.
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October 1995
Research Papers
Integration of Magnetic Bearings in the Design of Advanced Gas Turbine Engines
A. F. Storace,
A. F. Storace
General Electric Aircraft Engines, General Electric Company, Cincinnati, OH 45215
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D. Sood,
D. Sood
General Electric Aircraft Engines, General Electric Company, Cincinnati, OH 45215
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J. P. Lyons,
J. P. Lyons
Corporate Research and Development, General Electric Company, Schenectady, NY 12301
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M. A. Preston
M. A. Preston
Corporate Research and Development, General Electric Company, Schenectady, NY 12301
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A. F. Storace
General Electric Aircraft Engines, General Electric Company, Cincinnati, OH 45215
D. Sood
General Electric Aircraft Engines, General Electric Company, Cincinnati, OH 45215
J. P. Lyons
Corporate Research and Development, General Electric Company, Schenectady, NY 12301
M. A. Preston
Corporate Research and Development, General Electric Company, Schenectady, NY 12301
J. Eng. Gas Turbines Power. Oct 1995, 117(4): 655-665 (11 pages)
Published Online: October 1, 1995
Article history
Received:
February 19, 1994
Online:
November 19, 2007
Citation
Storace, A. F., Sood, D., Lyons, J. P., and Preston, M. A. (October 1, 1995). "Integration of Magnetic Bearings in the Design of Advanced Gas Turbine Engines." ASME. J. Eng. Gas Turbines Power. October 1995; 117(4): 655–665. https://doi.org/10.1115/1.2815450
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