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The design report

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Landing gear fabrication 5.5<br />

<strong>The</strong> <strong>design</strong> layout of the landing gears was very basic in detail and the manufacture of<br />

them was taken into little consideration during the <strong>design</strong> stages. <strong>The</strong> fuselage was<br />

<strong>design</strong>ed in order to hold the 4 basic gears in place with the front gears being able to fit<br />

into the same compartment as their corresponding servo. <strong>The</strong> landing gears by<br />

themselves had not been thought out so during fabrication, many decisions had to be<br />

made. <strong>The</strong> gears had to be strong in tension and compression yet light enough to stick to<br />

weight estimations. Thus, steel rods which were easily available were opted for.<br />

Figure 5.5.01<br />

<strong>The</strong> bending of landing gears in order to hold the wheels were more complicated than<br />

expected. Since no special machinery was available and due to time constraints, it was<br />

decided that they would just be done by hand at the laboratory instead of seeking<br />

assistance at any local metal working store. This meant that the landing gears were not<br />

bent to an exact right angle. <strong>The</strong>y also did not have a clear and defined bend, but rather<br />

curved upwards to meet the required angle. This proved fatal later during ground tests<br />

and the fact the metal itself was not stable on tarred road but performed better on<br />

flatter concrete proved that the coefficient of friction between the two different surfaces<br />

made a significant difference on the forces experienced by the gears.<br />

<strong>The</strong> major improvement that was implemented into the <strong>design</strong> was a suspension<br />

system for the rear gears that was holding approximately 75% of the total load. This<br />

system is shown in figure 5.5.01 and 5.5.02. <strong>The</strong> suspension had to be limited to a 1cm<br />

spring due to its lack of earlier addition to the <strong>design</strong>. <strong>The</strong> fuselages were not <strong>design</strong>ed<br />

to allow for such a system and the bottom plate of the fuselages restricted the allowance<br />

for the suspension spring. <strong>The</strong> spring was placed between the gear holder placed in the<br />

fuselage above and a stopper below. Finding screws and stoppers also seemed a<br />

challenge at the time as hex key that was required to use some of the stoppers were not<br />

available. We overcame this by using a Philips screw driver to force out the hex screw<br />

on the stoppers.

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