UWE Bristol Engineering showcase 2015
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Mathew Swinburne<br />
Mechanical <strong>Engineering</strong> MEng – Part B<br />
Project Supervisor<br />
Neil Larsen<br />
“When Competition Aerodynamics Fail” – Part B<br />
Literature Survey<br />
This paper’s empirical research consisted of two methods for measuring the pitch of the vehicle regardless of the gradient of a slope;<br />
using an accelerometer with a mathematical model and using a laser displacement sensor to measure the displacement between the<br />
front of the vehicle and the surface of the track. It found that both were viable options however concerns were raised over both<br />
methods which could not be resolved without further investigation; the accelerometers mathematical model requires the change in<br />
acceleration not to equal zero, the laser displacement sensor would require testing on a track surface to determine if the described<br />
preventions such as polarised filter and focused beam would suppresses errors associated with measuring the displacement to a rough<br />
surface.<br />
Accelerometers are found all around the home, from inside your smart phone, to your Nintendo Wii’s remote, even<br />
in the ignition device associated with airbags, but what are they? An accelerometer is a device, which can either be<br />
mechanical or electromechanical used to measure acceleration or deceleration. A mechanical version of the device<br />
uses a mass, spring and damper system. An electromechanical device can be either a slide wire, strain gauge,<br />
variable inductance or a piezoelectric or similar device that can measure the effects of acceleration.<br />
A mathematical model was derived that could calculated the pitch of the vehicle regardless of the gradient of the<br />
hill from the z and x components of the accelerometer.<br />
A laser displacement sensor (LDS) works by firing a laser beam at the object under study, the beam is fired at a slight angle,<br />
this beam bounces off the target object, where it then strikes a charged couple device (CCD). Unlike traditional<br />
displacement sensors, because there is no physical contact with the object, a LDS is not prone to wear and tear.<br />
A change in the displacement of a target object is recorded as a change in position on the charged coupled device pixels.<br />
the laser displacement sensor would require testing on a track surface to determine if the described preventions such as<br />
polarised filter and focused beam would suppresses errors associated with measuring the displacement to a rough surface.<br />
Proposed Concept<br />
Finally a design was proposed that took into consideration all relevant design constraints. The design<br />
consisted of two bars riveted to the flap with an arm on the bar at an angle of 20 ° to the horizontal<br />
axis. When this arm was pulled by an actuator contracting, it forced the flap open to 20 °, the optimum<br />
flap angle as discovered in the Part A paper. The design itself is simplistic and therefore has the least<br />
potential for failure.<br />
Project Abstract<br />
Part A validated the concept of using roof<br />
mounted flaps to prevent the phenomenon of<br />
lift-off, as experienced by a number of world<br />
endurance championship prototypes over the<br />
years. Part B looks at potential methods for<br />
measuring and calculating the pitch by using<br />
an accelerometer or the innovative concept<br />
of using a laser displacement sensor. This<br />
paper briefly looks at a control system for the<br />
deployment of the flap in the event of such<br />
an incident and finally a design is proposed<br />
that takes into account the stated design<br />
considerations. It was concluded that<br />
although either the accelerometer and laser<br />
displacement sensor were viable options in<br />
measuring or calculating the pitch further<br />
investigation was required before either could<br />
implemented with an acceptable level of<br />
error. The control system was produced in<br />
MATLAB using a simple ‘if’ function,<br />
determining the critical pitch before lift-off at<br />
a given velocity and comparing it to the pitch<br />
obtained from one of the chosen sensors,<br />
calculating whether the flap should be<br />
deployed or not. Finally a potential concept<br />
was designed in SolidWorks, composing of<br />
two bars riveted to the flap, which was<br />
opened by the contracting of two actuators.