Item 1773

OTHER: Helicopter - Inside - Coaxial - Electrotor- MicroLite

Drawing:

For a larger view click on the above drawing, then click on the mouse (magnifying glass) for a clearer view.

Helicopter Specifications page 1, Helicopter Specifications page 2

In the above Spec pages 2-blades per rotor and a pitch of 9.28º requires 29.9 HP to hover at 300 lb GW.

In the above Spec pages 3-blades per rotor and a pitch of 7.28º would requires 24.6 HP to hover at 300 lb GW.

The implication is that we should go with the 2 extra blades and 10 more lbs and thereby eliminate the 2P vibration also.

Design rotor hubs to take 2 and 3 blades each.

Bill of Material

Targeted Objectives:

Potential Improvements to the MicroLite

~ Reliability, Simplicity, Controllability and Safety - by Deconstruction ~

Future R&D:

Development that builds upon the Electrotor-SloMo motor work.

Alternative Drive:

Introduction Page | SynchroLite Home Page | Electrotor Home Page | UniCopter Home Page | Nemesis Home Page | AeroVantage Home Page:

Initially displayed: October 02, 2009~ Last Revised: November 12, 2009

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