System, assemblies and methods for mechanical-thrust power conversion multifans
A multi-rotor system for providing air thrust is disclosed comprising at least one multi-rotor assembly. The multi-rotor assembly comprising at least two rotors rotatable about a common axis wherein the outer radius of a first rotor is substantially similar to the inner radius of the second rotor. An airborne vehicle is also disclosed that is adapted to perform vertical takeoff and landing (VTOL). The airborne vehicle comprising at least two multi-rotor system disposed substantially symmetrically around the center of gravity of the vehicle.
1. A multi-rotor system comprising:
at least three rotors rotatable about a common axis,
wherein the outer radius of the first rotor is substantially similar to the inner radius of the second rotor, and
the outer radius of the second rotor is substantially similar to the inner radius of the third rotor; and wherein an air flow passing through one rotor of the at least three rotors does not pass through other rotors of the multi-rotor system; and
wherein the tip speed of all rotors is substantially the same.
2. The system of claim 1 wherein at least the second and the third rotors have an internal portion with no rotor blades.
3. The system of claim 1 wherein the at least three rotors have an internal portion with no rotor blades.
4. A multi-rotor system comprising:
at least three rotors rotatable about a common axis,
wherein the outer radius of the first rotor is substantially similar to the inner radius of the second rotor, and
the outer radius of the second rotor is substantially similar to the inner radius of the third rotor; and wherein an air flow passing through one rotor of the at least three rotors does not pass through other rotors of the multi-rotor system; and
at least one duct.
5. The system of claim 4 wherein the at least one duct is disposed around the outer radius of the outer rotor.
6. A multi-rotor system comprising:
at least three rotors rotatable about a common axis,
wherein the outer radius of the first rotor is substantially similar to the inner radius of the second rotor, and
the outer radius of the second rotor is substantially similar to the inner radius of the third rotor; and wherein an air flow passing through one rotor of the at least three rotors does not pass through other rotors of the multi-rotor system; and
wherein a duct is disposed around each of the at least three rotors.
7. A multi-rotor system comprising:
at least three rotors rotatable about a common axis,
wherein the outer radius of the first rotor is substantially similar to the inner radius of the second rotor, and
the outer radius of the second rotor is substantially similar to the inner radius of the third rotor; and wherein an air flow passing through one rotor of the at least three rotors does not pass through other rotors of the multi-rotor system; and
at least one flow stator to align the flow of air.
8. A multi-rotor system comprising:
at least three rotors rotatable about a common axis,
wherein the outer radius of the first rotor is substantially similar to the inner radius of the second rotor, and
the outer radius of the second rotor is substantially similar to the inner radius of the third rotor; and wherein an air flow passing through one rotor of the at least three rotors does not pass through other rotors of the multi-rotor system; and
at least one flow deflection shutter.
9. A multi-rotor system comprising:
at least three rotors rotatable about a common axis,
wherein the outer radius of the first rotor is substantially similar to the inner radius of the second rotor, and
the outer radius of the second rotor is substantially similar to the inner radius of the third rotor; and wherein an air flow passing through one rotor of the at least three rotors does not pass through other rotors of the multi-rotor system; and
wherein all the rotors rotate in the same rotational direction.
10. A multi-rotor system comprising:
a first rotor and a second rotor rotatable about a common axis;
wherein an outer radius of the first rotor is substantially similar to an inner radius of the second rotor;
wherein rotor blade tips of the first rotor and the second rotor are rotatable at substantially the same tangential speed; and
wherein the first rotor and the second rotor are rotatable in the same direction.
11. The system of claim 10 , wherein the tangential speed of the rotor blade tips of the first rotor and the second rotor is a maximal practical tangential speed for an operational profile of the multi-rotor system.
12. The system of claim 10 , wherein the first rotor and the second rotor are disposed and rotatable in a common plane.