ANALYSIS OF AN SC-17M DESIGNED MAIN LANDING GEAR LOADING ACTION

Authors

  • Sunny, O. U.,

    Air Force Institute of Technology Kaduna. Nigeria

  • Obinnaya, N.,

    Air Force Institute of Technology Kaduna. Nigeria

  • Japheth, G. C.

    Nigerian Defence Academy, Kaduna.

  • Nnaemeka, J. A.

    Air Force Institute of Technology Kaduna. Nigeria.

  • Bello, Y.

    Air Force Institute of Technology Kaduna. Nigeria.

DOI:
https://doi.org/10.51459/futajeet.2022.16.1.625
Keywords:
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Abstract

The concept of SC-17M aircraft design was initiated to address the shortfalls on the DO-228 and Hawker Beechcraft King Air 350i aircraft. Until recently by using a standard specification, an SC-17M landing gear design has been carried out. Detailed study of sub-part C of the certification standard aided the application and determination of the necessary loads on the landing gear. The comprehensive design employed 300M steel as the best structural material to be used in the fabrication of the landing gear. The maximum bending moment in the shock absorber and wheel axle were calculated and validated with the use of Strand7 software in the model stress analysis. The reserve of strength calculated shows that the landing gear was able to withstand the applied loads without experiencing any failure.

Author Biographies
  1. Sunny, O. U.,, Air Force Institute of Technology Kaduna. Nigeria

    Dept of Aircraft Engineering

  2. Obinnaya, N.,, Air Force Institute of Technology Kaduna. Nigeria

    Dept of Aircraft Engineering,

  3. Japheth, G. C., Nigerian Defence Academy, Kaduna.

    Dept of Mechanical Engineering, 

  4. Nnaemeka, J. A., Air Force Institute of Technology Kaduna. Nigeria.

    Dept of Mechanical Engineering,

  5. Bello, Y., Air Force Institute of Technology Kaduna. Nigeria.

    Dept of Mechanics Engineering, 

References

Abbe, G.E. (2018). Loading Action, Landing Gear Loads, UK: College of Aeronautics Aerospace Vehicle Design Cranfield University.

Abbe, G. E and Udu, A. G. (2018). Surveillance/Commuter Aircraft SC-17M Project Specification Kaduna : Air Force Institute of Technology.

EASA, (2013). CS-23 as Amended, United Kingdom: European Aviation Safety Agency .

Garth P (2018). Aerospace Structure, South Wares Australia: Mechanical and Manufacturing Engineering, University of South Wares Australia.

Rod, C. (2009). Main Landing Gear Design for the A-8 Hummingbird , UK: Cranfield University .

Uguzo S. O. (2010). A-9 Dragonfly Nose Landing Gear Design , UK: School of Engineering, Aerospace Vehicle Design Crandfield University .

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Published
2022-05-30
Issue
Vol. 16 No. 1 (2022): FUTA Journal of Engineering and Engineering Technology
Section
Articles
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How to Cite

ANALYSIS OF AN SC-17M DESIGNED MAIN LANDING GEAR LOADING ACTION. (2022). FUTA JOURNAL OF ENGINEERING AND ENGINEERING TECHNOLOGY, 16(1), 20-26. https://doi.org/10.51459/futajeet.2022.16.1.625

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