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UWE Bristol Engineering showcase 2015

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Marcius Antonio<br />

Meng Mechanical <strong>Engineering</strong><br />

Project Supervisor<br />

Dr. Tushar Dhavale<br />

Design of a storage rack for aircraft wheel and tyre assemblies<br />

Introduction<br />

The increasingly number of aircrafts, be it for civil<br />

or military purpose has increased large enterprises’<br />

concerns with respect to the management,<br />

maintenance and care with components that are<br />

replaced or removed from these aircrafts.<br />

Based on these needs aircraft company’s hangars<br />

raised the need of a system to accommodate<br />

replaced assemblies of aircrafts. In the aircraft<br />

industry, there is the recurring need that the wheel<br />

assemblies be stored in adjustable racks. It is also<br />

required that the rack presents a feature allowing<br />

assemblies to be rotated and inspected easily<br />

about every two or three months<br />

Aircraft tyre care and maintenance<br />

It is crucial for the proper tyre performance that<br />

had taken the necessary precautions with the<br />

assembly regarding to its storage and<br />

transportation. Due to operational carelessness,<br />

or negligence to follow the instructions, some<br />

defects may develop on the tyre, as follows:<br />

Design of structure<br />

The main frame of the rack has a rectangular<br />

shape. This layout was chosen mainly due to the<br />

fact that it should be stackable. Two types of<br />

frames were modelled to execute simulations and<br />

evaluate which would be the definitive frame.<br />

Once the structure<br />

was designed with<br />

hollow profiles (1020<br />

steel) having 30x40x2<br />

mm the main profile<br />

and 30x30x2 mm the<br />

trusses, applicable<br />

B.C for static loads<br />

were set.<br />

Simulation results<br />

The mechanism works similarly to dumpers,<br />

however, without any viscous fluid inside. The<br />

spring, with not very high stiffness, is coupled to a<br />

rounded plate in one side and the other end is<br />

fixed to an adjustable plate. A soft roller engaged<br />

to the inner edge is responsible for supporting the<br />

assembly in an upright position and rotates<br />

together with the tyre.<br />

Traceability device and program<br />

When started up, the program stores user name.<br />

Only authorised personnel must be allowed to<br />

access the registry and make any change and then<br />

give five buttons with the following features:<br />

store or remove a wheel, logoff, shut down the<br />

device and research on database. In order to<br />

store, the user must fill the serial number of the<br />

tyre, internal pressure, current date, the number<br />

of rack and in which bay it will be stored. There is<br />

also the possibility to add extra information about<br />

the tyre condition, such as defects or<br />

imperfections noticed by the operator.<br />

Project summary<br />

This work aims to design from an storage rack<br />

for tyre and wheel assemblies to be used in<br />

aircraft hangars and develop a device and<br />

software to assist the assemblies traceability<br />

and management.<br />

Project Objectives<br />

• Design an optimum rack to store and<br />

protect aircraft tyres<br />

• Design mechanisms assist stored tyre<br />

rotation manually or automatically<br />

• Develop traceability device and program<br />

• Implement components that will fill<br />

requirements<br />

Project specifications and requirements<br />

• Protection from UV light;<br />

• protection from damage when moving tyre<br />

• protection from spilled degrading fluids;<br />

• Place tyre on flat surface to prevent permanent<br />

distortion<br />

• do not allow tyre to rest one upon the other.<br />

removal turns a difficult task.<br />

• storeroom must be free from air current, as<br />

these bring in fresh sources of ozone;<br />

• Store away from fluorescent lights and electric<br />

generators, battery chargers.<br />

The highest Von Mises stress observed for the left<br />

frame is approximately 6.237x10 7 N/m² and<br />

3.567x10 7 N/m² for the right side one, which gives<br />

almost 10 of factor of safety.<br />

Rotation mechanisms<br />

The manual rotation will be performed using a crank<br />

system engaged directly to the roller shaft (when<br />

black pin is out). When the pin is inserted, the outer<br />

translucent cylinder, welded to the pulley, will<br />

transfer the torque to the crank handle shaft, which<br />

is engaged to the roller’s shaft; thus, the drill, with<br />

hexagonal tip can engage to the hexagonal hole and<br />

perform the rotation.<br />

Final Design<br />

It has a relatively<br />

compact area in relation<br />

to the amount of<br />

assemblies that it can<br />

store. The total<br />

dimensions of the rack<br />

are 2.020x3.629x1.898<br />

m, which is suitable to<br />

airplanes’ hangars.<br />

Project Conclusion<br />

The project goals were achieved satisfactorily,<br />

fulfilling most of the requirements that were<br />

stablished by the aviation companies and tyre care<br />

and maintenance manual. The deliverable at the<br />

end of the project is a design of a storage rack for<br />

aircraft tyre and wheel assemblies, which were<br />

developed according to specifications and<br />

requirements from the stakeholder and conditions<br />

for proper storage.<br />

The traceability program and device were<br />

successfully developed with robustness and an<br />

interface with easy operation.

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