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.