مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

645
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

0
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

Optimization Methods for the Weight of Agusta Helicopter Main Gearbox

Pages

  347-354

Abstract

 Nowadays, one of the most important challenges in engineering sciences is optimization of the existing designs due to the competitive industrial market. In aviation industry, weight and life of components are important criterions in their design. As an example, optimizaing the weight of main gearbox of helicopters with acceptable performance and Fatigue life are major concerns. In this paper, design parameters of Agusta helicopter main gearbox has been determined by three different optimization methods: Genetic Algorithm (GA), Particle Swarm Algorithm (PSO) and the Gravitational Search Algorithm (GSA). The objective function is the weight of the gears with appropraiate constrains which are based on geometrical limitations. Alsosafety factors according to the AGMA standards are considered. The design parameters are gear width as a continuous variable and normal module as a discrete parameter. Comparison of the results show that all three optimization methods are able to minimize the weight of the gearbox in the range of 23 to 27% comparing with the existing one; but, GSA not only gives the best optimized solution it also has the highest convergence rate.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    Vakili Tahami, F., Rasoulian, A., & Saadatmand Hashemi, S.. (2018). Optimization Methods for the Weight of Agusta Helicopter Main Gearbox. JOURNAL OF MECHANICAL ENGINEERING, 48(3 (84) ), 347-354. SID. https://sid.ir/paper/270169/en

    Vancouver: Copy

    Vakili Tahami F., Rasoulian A., Saadatmand Hashemi S.. Optimization Methods for the Weight of Agusta Helicopter Main Gearbox. JOURNAL OF MECHANICAL ENGINEERING[Internet]. 2018;48(3 (84) ):347-354. Available from: https://sid.ir/paper/270169/en

    IEEE: Copy

    F. Vakili Tahami, A. Rasoulian, and S. Saadatmand Hashemi, “Optimization Methods for the Weight of Agusta Helicopter Main Gearbox,” JOURNAL OF MECHANICAL ENGINEERING, vol. 48, no. 3 (84) , pp. 347–354, 2018, [Online]. Available: https://sid.ir/paper/270169/en

    Related Journal Papers

    Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button