index

Next Generation Rotorcraft

Utilizing the natural advantages of bilateral symmetry.

The Intermeshing, the Interleaving and the PropRotor configurations

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 and 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:

SynchroLite: ~ Ultralight; Intermeshing and Interleaving ~ for Personal Aerial Vehicles.

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

AeroVantage: ~ Light, Medium and Heavy PropRotor - VTOL craft for High-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:
	Vibration - Rotor Induced - Control:

Other:

To do a search on this web side;