01.06.2017 Views

UWE Bristol Engineering showcase 2015

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

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.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!