Landing gear system structural design

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Reference no: EM13210585

Landing Gear System Structural Design

Problem Statement Consider the landing gear shown below. Working in teprns of two, come up with a single optimized design for given operational conditions and design considerations with a design factor of n=1.5.

Design objective: minimize Me structural weight

Design variabks: Dimensions of cylinder and axle (D_rod, D_{bore_or} and D_{axle_i})

Design considerations: yield failure, bucking, fatigue strength

923_Landing Gear System Structural Design.png

Maximum landing load = 250kg (consider the dynarnic effect factor = 2.0), Target life = 100000 Cycles Any other information needed for your design must be explaind and added as your assumption.

Reference no: EM13210585

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