Next Generation Rotorcraft

The Intermeshing, the Interleaving and the PropRotor configurations

Electrotor-SloMo Electrotor-Plus

The following design information is openly offered on the Web;

To provoke thought about improving rotorcraft; from the perspective of their aerodynamic interface with the environment, plus electrical drives.

To solicit corrections, criticism, ideas and assistance. ~ jackson.dave@shaw.ca

To support others in the design and development of laterally symmetrical rotorcraft.

Rotorcraft Projects:

Electrotor-SloMo: ~ Electrically driven rotors w/ a 1:1 ratio between the motor and aero-rotor.

UniCopter: ~ Very-Light and Light Intermeshing ~ for In-flight Activities and scaled UAVs.

Nemesis: ~ Medium and Heavy lift Interleaving ~ for High-speed Transportation.

AeroVantage: ~ PropRotors w/ two-state disk area - for Higher-speed Transportation.

Developing Rotorcraft Attributes:

		SynchroLite:	UniCopter:	Nemesis:	AeroVantage:
Configurations:
	Intermeshing:
	Interleaving:
	PropRotor:
Rotors:
	3-blade CVJ w/ Hub Spring:
	3-blade Offset Teetering Rotor:
	Electrotors:
	'Absolutely' Rigid Rotors:
	Advancing Blade Concept:
	Active Blade Twist: - Independent Root & Tip Control:
	Large Chord and Low Tip Speed:
	Reverse Velocity Utilization:
	Aerodynamically Variable PropRotor: (AVPR):
Additional:
	Electric Drives:
	Variable Speed Rotors and Propeller:
	Unmanned Arial Vehicles:

Other:

To do a search on this web side;

Go to Google.
Enter into the search box [site:unicopter.com followed by the desired search criteria.] Such as: blade; blade AND pitch; blade OR pitch