Next Generation Rotorcraft

Utilizing the natural advantages of bilateral symmetry.

The Intermeshing and Interleaving configurations, plus PropRotor

SynchroLite

UniCopter

Nemesis

AeroVantage

The following design information is openly offered on the Web;
  1. To provoke thought about improved rotorcraft.
  2. To solicit constructive criticism, ideas and/or technical assistance. ~ jackson.dave@shaw.ca
  3. To support others in the design and development of Intermeshing and Interleaving helicopters.

Rotorcraft Projects:

Developing Rotorcraft Attributes:

 

 

 

SynchroLite:

UniCopter:

Nemesis:

AeroVantage:

 

Configurations:

 

 

 

 

 

 

Intermeshing Configuration:

 

 

 

 

Interleaving Configuration:

 

 

 

2x4 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):

 

 

 

 

Other:

 

 

 

 

 

 

Electric Drives:

 

 

 

Variable Speed Rotors and Propeller:

 

 

 

 

 

Vibration - Rotor Induced - Control:

 

 

 

 

Unmanned Arial Vehicles:

All material is constantly being expanded and revised. ~ It contains many errors.

Additions, corrections and technical suggestions requested. ~ jackson.dave@shaw.ca