30.01.2013 Views

Aerodynamics and Design for Ultra-Low Reynolds Number Flight

Aerodynamics and Design for Ultra-Low Reynolds Number Flight

Aerodynamics and Design for Ultra-Low Reynolds Number Flight

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Chapter 6<br />

efficiencies are only a part of the total electo-mechanical efficiency of the power <strong>and</strong><br />

propulsion system, battery, wiring harness, <strong>and</strong> controller efficiencies further reduced the<br />

total system efficiency.<br />

For their small size, these motors provide very good per<strong>for</strong>mance both in terms of torque<br />

production <strong>and</strong> high rotational speeds. One limitation of this three-pole stepper motor is<br />

the need <strong>for</strong> additional circuitry to cycle power through the motor coils. This adds mass<br />

to the system; in the final configuration of the 15g vehicle, the controllers represent a<br />

mass fraction of 20% to 30%. Simple circuitry is required to run the motor without<br />

feedback, but the motor efficiency is greatly reduced <strong>and</strong> the maximum RPM under load<br />

drops considerably, in this case from well over 50,000 RPM to below 25,000 RPM.<br />

Feedback is required to account <strong>for</strong> phase lags in the coil/shaft position induced by the<br />

rotational inertia of the shaft <strong>and</strong> rotor, friction, <strong>and</strong> aerodynamic drag. The feedback<br />

circuitry does not add considerably to the mass, but the complexity of the circuity<br />

increases. Small traditional or coreless DC motors, such a pager motors, are not a viable<br />

alternative. Although they require no additional circuity, these motors provide<br />

insufficient torque <strong>and</strong> rotational speed at his scale. Their efficiencies are also typically<br />

much lower, often as low as 5% to 10%. It may be possible that a design-specific<br />

traditional DC motor could be built with per<strong>for</strong>mance closer to the level of the 5mm<br />

Smoovy, but this is beyond the scope of this work.<br />

6.2.2 Astroflight Firefly Motor<br />

The ten inch diameter rotor is powered by the Astroflight Firefly coreless DC motor with<br />

an integrated 16:1 gearbox, Model #800 [39]. This motor <strong>and</strong> gearbox have a combined<br />

mass of 12g <strong>and</strong> a manufacturer’s indicated efficiency of 83%. The Firefly <strong>and</strong> gearbox<br />

are pictured in Figure 6.2. This, once again, is not the total system electro-mechanical<br />

efficiency, simply that of the motor <strong>and</strong> gear box. This factor of two to four increase in<br />

efficiency relative to the 5mm Smoovy illustrates some of the practical difficulties<br />

associated with developing very small flight vehicles. In each case these motors<br />

represent the upper levels of per<strong>for</strong>mance at their respective scales.<br />

98

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

Saved successfully!

Ooh no, something went wrong!