Abstract
The structural integrity analysis of a quill shaft of an aero engine fuel pump is carried out through finite element method. Maximum operating condition, over-load condition to account for any malfunction of fuel control system or over-speed of engine rotors and 400% loading for production acceptance are the three major conditions which have been analyzed for ensuring structural integrity of the shaft. Nodal analysis is also carried out to examine the natural frequency of the quill shaft and to verify that it is in a safe distance from the operating speed of rotating components in fuel pump and gear box.
Similar content being viewed by others
References
H.A. Spang III, H. Brown, Control of jet engines. Control Eng. Pract. 7(9), 1043–1059 (1999)
C.E. Pearson, T.J. Higgins, Inventors; General Electric Co, Assignee. Gas turbine fuel system. United States patent US 4,467,610. 28 Aug 1984
R.D. Zagranski, J. Mannarino, C. Crainic, Inventors; Pratt, Whitney Canada Corp, Goodrich Pump, Engine Control Systems Inc, Assignee. Fuel control system for gas turbine engines. United States patent US 7,136,738. 14 Nov 2006
J. Li, D. Fan, V. Sreeram, SFC optimization for aero engine based on hybrid GA-SQP method. Int. J. Turbo Jet-Engines 30(4), 383–391 (2013)
S.T. Lin, L.W. Yeh, Intelligent control for the main fuel flow of the F-100 turbofan engine. Int. J. Turbo Jet Engines 16(3), 127–140 (1999)
R. Langton, Gas turbine fuel control systems. Encycl. Aerosp. Eng. (2010). https://doi.org/10.1002/9780470686652.eae467
D. Xie, Y. Xiong, H. Zhang, Y. Yang, Dynamic analysis of a rig shafting vibration based on finite element. Front. Mech. Eng. 8(3), 244–251 (2013)
L. Murawski, Axial vibrations of a marine shaft line: calculations–measurements comparison. WIT Trans. Built Environ. 25, 53 (2001)
R.L. Norton, Machine Design: An Integrated Approach, 2nd edn. (Pearson Education, Hong Kong, 2001), pp. 366–383
C.M. Sonsino, H. Kaufmann, J. Foth, F. Jauch, Fatigue strength of driving shafts of automatic transmission gearboxes under operational torques. SAE Trans. 1, 635–648 (1997)
Author information
Authors and Affiliations
Corresponding author
Additional information
Publisher's Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Rights and permissions
About this article
Cite this article
Kumar, V., Mishra, R.K. Finite Element Analysis of Quill Shaft of an Aero Engine Fuel Pump for Structural Integrity. J Fail. Anal. and Preven. 20, 348–352 (2020). https://doi.org/10.1007/s11668-020-00838-5
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s11668-020-00838-5