AIRBORNE KINETIC ENERGY CONVERSION SYSTEM
Methods and apparatus to harvest renewable energy are provided herein. In some embodiments, a wind-powered aircraft includes an airframe suitable for untethered flight in an open airspace; and an airborne kinetic energy conversion system attached to the airframe, the airborne kinetic energy conversion system comprising a turbine, a generator connected to the turbine, and an energy storage means connected to the generator.
1 . A wind-powered aircraft, comprising:
an airframe suitable for untethered flight in an open airspace; and
an airborne kinetic energy conversion system attached to the airframe, the airborne kinetic energy conversion system comprising a turbine, a generator connected to the turbine, and an energy storage means connected to the generator.
2 . The aircraft of claim 1 , wherein the wind-powered aircraft is an unmanned aircraft.
3 . The aircraft of claim 1 , further comprising flight control electronics suitable for controlling a flight path of the aircraft.
4 . The aircraft of claim 3 , further comprising flight sensors.
5 . The aircraft of claim 4 , wherein the flight control electronics comprises an electronic autopilot system programmed to perform a flight maneuver for harvesting wind power in presence of one or more of a vertical updraft, horizontal wind shear, a wind gust, or a cloud zone.
6 . The aircraft of claim 5 , wherein the electronic autopilot system is configured to receive and analyze data from the flight sensors to recognize the presence of one or more of the vertical updraft, the horizontal wind shear, the wind gust, or the cloud zone.
7 . The aircraft of claim 6 , wherein the electronic autopilot system is configured to search for one or more of the vertical updraft or the horizontal wind shear.
8 . The aircraft of claim 1 , further comprising a photovoltaic solar power system.
9 . The aircraft of claim 8 , further comprising power control electronics configured to control power flow among the energy storage means, the generator, and the photovoltaic solar power system.
10 . The aircraft of claim 1 , further comprising a propulsion system.
11 . The aircraft of claim 10 , wherein the propulsion system comprises an electric motor and a propeller that are configured to be able to function as the generator and the turbine.
12 . The aircraft of claim 11 , further comprising a two-way speed controller.
13 . The aircraft of claim 11 , wherein the propeller is a variable pitch propeller.
14 . The aircraft of claim 1 , further comprising a water collector.
15 . The aircraft of claim 1 , further comprising a plurality of generators.
16 . The aircraft of claim 15 , wherein the plurality of generators are configured to operate independently of each other.
17 . The aircraft of claim 1 , wherein the airframe comprises a lightweight wing made from a carbon fiber material.
18 . The aircraft of claim 1 , wherein the airframe comprises a wing having a downward bow shape.
19 . The aircraft of claim 1 , wherein the airframe comprises a wing having a capability to change one of its shape and relative position.
20 . A wind-powered aircraft, comprising:
an airframe suitable for untethered flight in an open airspace; and
an airborne kinetic energy conversion system attached to the airframe, the airborne kinetic energy conversion system comprising:
a turbine;
a mechanical converter connected to the turbine; and
mechanical energy storage means connected to the mechanical converter.