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Old 17th May 2007, 19:18
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Dave_Jackson
 
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Adam,

Reducing the RPM of the rotor will require that the pitch of the blades be increased to maintain the same thrust. This is an advantage in that the efficiency (power/thrust) is increased.

Unfortunately, this also increases the risk that a perturbation, malfunction, etc. will cause the rotor to loose all lift.

The Boeing Hummingbird is an Unmanned Aerial Vehicle therefore its crash would be unfortunate but not tragic. The loss of life in a helicopter crash is much more serious. With all regards for the relatives and associates of the deceased, helicopter fatalities have also resulted in the demise of a number of aspiring helicopter manufacturers.

IMHO, and subject to elaboration or correction by others.

Dave
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