TOPOLOGY OPTIMIZATION OF LANDING GEAR’S LEG FOR AERIAL VEHICLE USING ANSYS

Authors

  • AMUSURI SATISH PG scholar, Dept. of ME, ASR College of Engineering, Tanuku
  • V. RAVI Asst. Professor, Dept. of ME, ASR College of Engineering, Tanuku
  • B.CHANDRA SHEKAR Asst. Professor, Dept. of ME, ASR College of Engineering, Tanuku

Abstract

The landing gear is a structure that supports an aircraft on ground and allows it to taxi, take-off, and land. In fact, landing gear design tends to have several interferences with the aircraft structural design. Present research is going in the weight of landing gear has become an important factor and efforts are being made to reduce the weight of the aircraft landing gear to consequently increase the payload. This thesis presents an approach to optimize the weight of landing gear’s leg for an Un-manned Aerial Vehicle (UAV) made of aluminum ASM 7075 material adopted from aerospace specification materials. Loads are applied through a rigid boundary condition & screw boundary connection.

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Published

2018-07-14

How to Cite

SATISH, A., RAVI, V., & SHEKAR, B. . (2018). TOPOLOGY OPTIMIZATION OF LANDING GEAR’S LEG FOR AERIAL VEHICLE USING ANSYS. International Journal of Technical Innovation in Modern Engineering & Science, 4(7), 1046–1054. Retrieved from https://ijtimes.com/index.php/ijtimes/article/view/1296

Issue

Vol. 4 No. 7 (2018): Vol. 4 No. 7: Volume 4 Issue 7 (July-2018)

Section

Articles