New Techniques in Jet Engine Balancing

Abstract

The design of jet engine parts makes particular claims on the balancing machines used: shortest spinning time in the balancing machine, e.g. no nulling and calibration runs—set up of the plane computer at stand still—exact plane setting even at close compensation plane distances and large bearing plane space—installation of rotors with their own operational ball or roller bearings without necessity of the parasitic mass of connection frames or squares.

Citation

REUTLINGER, W. and BOXBERGER, H. (1979), "New Techniques in Jet Engine Balancing", Aircraft Engineering and Aerospace Technology, Vol. 51 No. 6, pp. 14-17. https://doi.org/10.1108/eb035536