Flying electric generators with clean air rotors
First Claim
1. A flying electric generator comprising a fuselage, wherein the fuselage includes a centralized housing, at least a first pair of boom arms extending forward from and laterally outwardly of the housing and have outer ends, at least a first pair of counter rotating first rotors being mounted along the outer ends of the at least first pair of boom arms, at least a second pair of boom arms extending aft and laterally outwardly from the housing and having outer ends, at least a first pair of second counter rotating rotors mounted along the outer ends of the at least second pair of boom arms and wherein each of the rotors is mounted to the fuselage such that when the at least first pair of first rotors are leading into the wind, each of the at least first pair of first rotors and the at least first pair of second rotors is positioned so as to receive a direct path to an undisturbed flow of wind regardless of angle of attack or pitch angle of the flying electric generator, and wherein the housing defines a center of gravity of the flying electric generator.
2 Assignments
0 Petitions
Accused Products
Abstract
Flying electric generator aircraft that include groupings of four rotors mounted to booms extending fore and aft of a fuselage structure wherein the rotors are placed so that when the aircraft is facing the wind, each rotor has a direct path to an undisturbed flow of air, regardless of pitch angle and during all flight maneuvers of the aircraft. The rotors are placed in counter-rotating pairs with the booms preferably angled so that the rotors in the front of the aircraft are spaced at a distance from one another that is different than a spacing of the rotors at the rear of the aircraft.
99 Citations
10 Claims
- 1. A flying electric generator comprising a fuselage, wherein the fuselage includes a centralized housing, at least a first pair of boom arms extending forward from and laterally outwardly of the housing and have outer ends, at least a first pair of counter rotating first rotors being mounted along the outer ends of the at least first pair of boom arms, at least a second pair of boom arms extending aft and laterally outwardly from the housing and having outer ends, at least a first pair of second counter rotating rotors mounted along the outer ends of the at least second pair of boom arms and wherein each of the rotors is mounted to the fuselage such that when the at least first pair of first rotors are leading into the wind, each of the at least first pair of first rotors and the at least first pair of second rotors is positioned so as to receive a direct path to an undisturbed flow of wind regardless of angle of attack or pitch angle of the flying electric generator, and wherein the housing defines a center of gravity of the flying electric generator.
Specification