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2.3.3 Propeller Geometry Development Through CAD<br />

After the blade design is detennined to be satisfactory, the program will create a text file<br />

(OpenPVL_CADblade.txt) to export the propeller blade geometry. The file provides a<br />

series of points that deseribe each foil section ofthe blade. This file was then used as an<br />

input for the CAD software RHINO, which generates the points for the foil sections. The<br />

propeller geometry is generated by creating closed splines for each sections and<br />

connecting the sections to generate a blade. The hub design is the following step, and then<br />

based on the designed number ofblades to add all blades onto the hub [20]. After the<br />

propeller geometry is generated, a file can be created by RHINO to fabricate a prototype<br />

for testing by a rapid prototyping (RP) machine (.STL fonnat). The RP part can then be<br />

tcstc..'d. If the testing results arc not satisfied, designers can go back to modify the<br />

propeller geometry in RHINO or regenerate a new design in OpenPVL, and then<br />

prototype and test again. These fabrication-tesling·modification procedures arc repeated<br />

until a satisfactory propeller is created.<br />

In 2007, D'Epagnier designed an AUV propeller using OpenPVL code, and the AUV<br />

Propeller has the following characteristics [20]:<br />

The propeller has three blades.<br />

The propeller is operated on the vehicle at 120 RPM in order 10 reach a speed of<br />

1.0m/s.<br />

The diameter of the propeller is 0.6096 m.<br />

The required forward thrust ofthe propeller is 75 N.<br />

26

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