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Optimization of spur gear pairs for aerospace applications

  • Burak Ocak

    Burak Ocak, born in 1992, is currently a PhD student at Computational Mechanics Department, Middle East Technical University, Turkey. He received his MSc at Middle East Technical University. He is working in Power Transmission Systems Department, Turkish Aerospace, Ankara, Turkey. He was in charge of modeling, writing and editing of this manuscript.

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    , Zafer Evis ORCID logo and Fahrettin Ozturk ORCID logo EMAIL logo
Published/Copyright: November 4, 2022
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Abstract

High power applications at high speed create contact problems, increase heat sink values and transmission error (TE) during gear meshing. Hence, analyzing the gear mesh including helix angle effect, the optimization in terms of contact pressure and the transmission error reduction are all crucial for high-speed applications. In this study, meshing characteristics including helix angle based on different approaches, optimization of spur gears pairs in terms of the transmission error and contact stresses obtained from improved analytical method besides transmission design tools are all investigated for high-speed aerospace applications. Results reveal that significant transmission error reduction could be achieved by applying tip relief starting from the highest-point of single tooth contact for spur gears in aerospace applications. Hence, the need for higher contact ratio by helix angle inclusion for smoother transmission could be compensated by using tip-relief modified spur gears in gearbox since the heat sink values also need to be minimized by using relatively lower contact ratio. Results obtained from the improved analytical method by directly considering gear geometry including gear foundation effects based on direct deformation–summation approach are found in between AGMA (American Gear Manufacturers Association) standard and ISO (International Organization for Standardization) standard results.


Corresponding author: Fahrettin Ozturk, Mechanical Engineering, Ankara Yildirim Beyazit University, Etlik Ayvalı Street 7, Ankara, 06010, Turkey, E-mail:

Funding source: Presidency of Defense Industries, Turkey for funding the project in cooperation with Turkish Aerospace Industries, Inc.

Award Identifier / Grant number: (Project Number: DDDKA1)

About the author

Burak Ocak

Burak Ocak, born in 1992, is currently a PhD student at Computational Mechanics Department, Middle East Technical University, Turkey. He received his MSc at Middle East Technical University. He is working in Power Transmission Systems Department, Turkish Aerospace, Ankara, Turkey. He was in charge of modeling, writing and editing of this manuscript.

  1. Author contributions: All the authors have accepted responsibility for the entire content of this submitted manuscript and approved submission.

  2. Research funding: The authors would like to thank to Presidency of Defense Industries, Turkey for funding the project (Project Number: DDDKA1) in cooperation with Turkish Aerospace Industries, Inc.

  3. Conflict of interest statement: The authors declare no conflicts of interest regarding this article.

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Published Online: 2022-11-04
Published in Print: 2022-11-25

© 2022 Walter de Gruyter GmbH, Berlin/Boston

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