Analysis on Axial Displacements of an Engine Main Shaft in Complex Temperature Environments

Author:

Pan Jian Zhi1,Cao Deng Qing1,Chu Shi Ming1

Affiliation:

1. Harbin Institute of Technology

Abstract

Considering the characteristics of an aero-engine whose main rotor, as an asymmetric structure, operating in a non-uniform temperature environment, a new dynamical modal of shaft is established for axial displacement analysis based on temperature internal force of non-uniform temperature field. The influence of non-uniform temperature field and the temperature changing are quantified. Based on the influence of temperature internal forces, the analytical formulae of axial displacement of a specified point in the shaft under a continuous temperature field and a discretized temperature field are derived, respectively. At last, the acceleration warming formula is used to simulate the warming up and stable time period, and its variation regularity is compared and analyzed. The relationship between strains of rotor main shaft and temperature internal forces are obtained through the new model and its analytical formulae. Furthermore, the feasibility and relevance of the new model are verified by an equivalent conclusion.

Publisher

Trans Tech Publications, Ltd.

Reference7 articles.

1. M. Deng: Principle and Structure of Aviation Fuel Gas Turbine Engines (National defense industry press, China 2008) p.1. (In Chinese).

2. B.C. Wen, et al.: Higher Rotor Dynamics (China Machine Press, China 1999) p.1. (In Chinese).

3. Y.E. Zhong, et al.: Rotor Dynamics (Tsinghua University Press, China 1987) p.1. (In Chinese).

4. J.A. Visser and A. Bekker: Natural/Forced Convection and Combustion Simulation, (1992), p.633.

5. A. Weller: Review of Scientific Instruments, Vol. 54 (1983) No. 8, p.952.

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