AV_ElectricCyclic

AeroVantage - Control (Flight & Power) - Cyclic by Sectored Torque-Pitch

Overview:

To utilize and extend the features of the Electrotor-SloMo - Control Flight - Auto-Collective by Torque-Pitch

Currently the Auto-Collective is intended to work with a weight-shift direction control to provide a very simple flight control system.

However, the operational features of the 'Auto-Collective by Torque-Pitch' [linked to above] offer the foundation and principal for providing cyclic control, and also for providing higher harmonic control; by an enhancement to the method of electrical driven torque-pitch.

This feature would probably be most applicable to large rotorcraft. However, it could also be applied to ultralight rotorcraft that desire the lower disk loading that is provided by rotors with a greater radius.

It will also eliminate the tilting of the fuselage that is necessary to weight-shift the rotors.

Working Papers:

DESIGN:

B603

MAKE:

Eventually, go to Rotor - Hub, Motor & Motor Control.

BUY:

Items:

DESIGN:

	Name	Item
	Aerovantage - Control (Flight & Power) - Cyclic by Sectored Torque-Pitch - Overview	1932

MAKE:

	Name	Drg.	BOM
	Eventually go to Rotor - Hub, Motor & Motor Control pages.

Initially displayed: July 31, 2010~ Last Revised: January 1, 2012

The above utility invention is openly and publicly disclosed on the Internet to negate an entity from patenting it, to the exclusion of all others whom may wish to use it. ~ Reference patent law 35 U.S.C. 102 A person shall be entitled to a patent unless - (a) the invention was known ... by others in this country, ..., before the invention thereof by the applicant for patent.