New Locking Mechanism for Safe Landing

dc.contributor.authorRakshith, N.
dc.date.accessioned2026-02-06T06:35:47Z
dc.date.issued2022
dc.description.abstractA study shows that 53% of all aviation accidents while landing occur because of human error. There is a high possibility that the orientation of the landing gear mechanism changing/moving from the position required for proper landing the aircraft (toggle/extreme position) because of loads along or opposite to the direction of motion of the landing gear. To avoid this, the pilot has to take extra precautions and follow a really complex procedure for landing, and this mitigates the risk but does not eliminate the possibility of motion completely as human error cannot be eliminated. In this paper, I aim to propose an approach of locking the landing gear mechanism in its extreme position and eliminate the risk of it changing its orientation while landing, by using an additional set of slider crank mechanisms which restricts the motion of the landing mechanism. By doing this, we eliminate the risk of motion of the landing gear during landing and thus reduce the risk of an accident during landing. © 2022, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
dc.identifier.citationLecture Notes in Mechanical Engineering, 2022, Vol., , p. 161-169
dc.identifier.issn21954356
dc.identifier.urihttps://doi.org/10.1007/978-981-16-2794-1_14
dc.identifier.urihttps://idr.nitk.ac.in/handle/123456789/30055
dc.publisherSpringer Science and Business Media Deutschland GmbH
dc.subjectLanding gear mechanism
dc.subjectOrientation
dc.subjectSlider crank
dc.titleNew Locking Mechanism for Safe Landing

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