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Journal of Failure Analysis and Prevention

, Volume 19, Issue 2, pp 308–313 | Cite as

Failure Analysis of a Cam Gear in the Torquemeter Assembly of a Turboprop Engine

  • R. K. MishraEmail author
  • D. Arul Kumaresan
  • C. Jagadish Babu
  • Vinay Kumar
Case History---Peer-Reviewed
  • 37 Downloads

Abstract

Failure analysis of a cam gear in the torquemeter assembly of a turboprop engine has been carried out to determine the root cause of the failure so that remedial measures can be adopted to prevent such failures in flight. During flight, one of the engine torques and turbine temperatures started fluctuating leading to the shutting off of the engine. Detailed defect investigation reveals that improper assembly and mounting of the gear have led to the shearing off gear teeth causing torque fluctuation.

Keywords

Turboprop engine Torquemeter Cam gear Fractography Fatigue failure 

Notes

Acknowledgments

The authors are very grateful to the Chief Executive (Airworthiness), CEMILAC for his kind permission for publishing this paper. They are also very thankful to the engineers of Hindustan Aeronautics Limited and Aeronautical Quality Assurance for their support during the present work.

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Copyright information

© ASM International 2019

Authors and Affiliations

  • R. K. Mishra
    • 1
    Email author
  • D. Arul Kumaresan
    • 1
  • C. Jagadish Babu
    • 1
  • Vinay Kumar
    • 1
  1. 1.Regional Centre for Military Airworthiness (Engines)BangaloreIndia

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