Methods and apparatus for reducing energy consumed by drones during flight

Patent metadata

Field	Value
Publication number	US-10386833-B2
Application number	US-201615565035-A
Country	US
Kind code	B2
Filing date	Dec 7, 2016
Priority date	Dec 7, 2016
Publication date	Aug 20, 2019
Grant date	Aug 20, 2019

Abstract

Methods and apparatus for reducing energy consumed by drones during flight are disclosed. A drone includes a housing, a motor, and a route manager to generate a route for a flight of the drone based on wind data. The wind data includes turbine-generated wind data provided by turbines that detect airflows received at the turbines. The turbines are located in an area within which a segment of the flight of the drone is to occur. The route is to be followed by the drone during the flight to reduce energy consumed by the drone during the flight.

First claim

What is claimed is:

1. A drone, comprising:
a housing;
a motor; and
a route manager to generate a route for a flight of the drone based on wind data, the wind data including turbine-generated wind data provided by turbines that detect airflows received at the turbines, the turbines located in an area within which a segment of the flight is to occur, the wind data further including airborne drone-generated wind data provided to the drone by an airborne drone located in the area, the airborne drone-generated wind data to be determined by an inertial measurement unit of the airborne drone, the route to be followed by the drone during the flight to reduce energy consumed by the drone during the flight.

2. A drone as defined in claim 1 , wherein the turbine-generated wind data includes a direction of airflow detected by a first one of the turbines, a speed of the airflow detected by the first one of the turbines, and a location of the first one of the turbines.

3. A drone as defined in claim 1 , wherein the route passes through a tailwind area within which the drone is to engage a tailwind during the flight, the tailwind to be detected by at least one of the turbines.

4. A drone as defined in claim 1 , wherein the route passes through an updraft area within which the drone is to engage an updraft during the flight, the updraft to be detected by at least one of the turbines.

5. A drone as defined in claim 1 , wherein the airborne drone-generated wind data includes a direction of airflow detected by the inertial measurement unit, a speed of the airflow detected by the inertial measurement unit, and a location of the airborne drone.

6. A drone as defined in claim 1 , wherein the drone is to be launched via a launch booster.

7. A drone as defined in claim 6 , wherein the launch booster is to increase at least one of a height of the drone or a speed of the drone.

8. A drone as defined in claim 6 , wherein the launch booster includes at least one of a catapult, a slingshot, a balloon, a rocket, or a vacuum chamber.

9. A drone, comprising:
a housing;
a motor;
a route manager to generate a route for a flight of the drone based on wind data, the wind data including turbine-generated wind data provided by turbines that detect airflows at the turbines, the turbines located in an area within which a segment of the flight is to occur, the route to be followed by the drone during the flight to reduce energy consumed by the drone during the flight, the drone to be launched via a launch booster; and
a power manager to provide power to the motor of the drone in response to detecting an apex of the launch of the drone.

10. A drone, comprising:
a housing;
a motor;
a route manager to generate a route for a flight of the drone based on wind data, the wind data including turbine-generated wind data provided by turbines that detect airflows at the turbines, the turbines located in an area within which a segment of the flight is to occur, the route to be followed by the drone during the flight to reduce energy consumed by the drone during the flight, the drone to be launched via a launch booster; and
a shape manager to change a shape of the drone in response to detecting an apex of the launch of the drone.

11. A method to reduce energy consumed by a drone during a flight of the drone, the method comprising:
obtaining, by executing a computer readable instruction with a processor, wind data including turbine-generated wind data provided by turbines that detect airflows received at the turbines, the turbines located in an area within which a segment of the flight is to occur, the wind data further including airborne drone-generated wind data obtained by the drone from an airborne drone located in the area, the airborne drone-generated wind data determined by an inertial measurement unit of the airborne drone; and
generating, by executing a computer readable instruction with the processor, a route for the flight of the drone based on wind data, the route to be followed by the drone during the flight to reduce the energy consumed by the drone during the flight.

12. A method as defined in claim 11 , wherein the turbine-generated wind data includes a direction of airflow detected by a first one of the turbines, a speed of the airflow detected by the first one of the turbines, and a location of the first one of the turbines.

13. A method as defined in claim 11 , wherein the airborne drone-generated wind data includes a direction of airflow detected by the inertial measurement unit, a speed of the airflow detected by the inertial measurement unit, and a location of the airborne drone.

14. A method as defined in claim 11 , further including launching the drone via a launch booster.

15. A method as defined in claim 14 , wherein the launching of the drone via the launch booster includes at least one of launching the drone via a catapult, launching the drone via a slingshot, launching the drone via a balloon, launching the drone via a rocket, or launching the drone via a vacuum chamber.

16. A method to reduce energy consumed by a drone during a flight of the drone, the method comprising:
obtaining, by executing a computer readable instruction with a processor, wind data including turbine-generated wind data provided by turbines that detect airflows at the turbines, the turbines located in an area within which a segment of the flight is to occur;
generating, by executing a computer readable instruction with the processor, a route for the flight of the drone based on wind data, the route to be followed by the drone during the flight to reduce the energy consumed by the drone during the flight;
launching the drone via a launch booster; and
providing power to a motor of the drone in response to detecting an apex of the launch of the drone.

17. A method to reduce energy consumed by a drone during a flight of the drone, the method comprising:
obtaining, by executing a computer readable instruction with a processor, wind data including turbine-generated wind data provided by turbines that detect airflows at the turbines, the turbines located in an area within which a segment of the flight is to occur;
generating, by executing a computer readable instruction with the processor, a route for the flight of the drone based on wind data, the route to be followed by the drone during the flight to reduce the energy consumed by the drone during the flight;
launching the drone via a launch booster; and
changing a shape of the drone in response to detecting an apex of the launch of the drone.

18. A tangible machine-readable storage medium comprising instructions that, when executed, cause a processor to at least:
obtain wind data including turbine-generated wind data provided by turbines that detect airflows received at the turbines, the turbines located in an area within which a segment of a flight of a drone is to occur, the wind data further including airborne drone-generated wind data obtained by the drone from an airborne drone located in the area, the airborne drone-generated wind data determined by an inertial measurement unit of the airborne drone; and
generate a route for the flight of the drone based on wind data, the route to be followed by the drone during the flight to reduce energy consumed by the drone during the flight.

19. A machine-readable storage medium as defined in claim 18 , wherein the turbine-generated wind data includes a direction of airflow detected by a first one of the turbines, a speed of the airflow detected by the first one of the turbines, an

Assignees

• Intel Corp

Inventors

• Yang Songnan
• Abozaed Muhammad
• De La Guardia Gonzalez Rafael
• Gomez Gutierrez David
• Wong Hong

Classifications

• B64U70/70

  Launching or landing using catapults, tracks or rails (launching from storage containers B64U70/50) · CPC title

• B64U2201/10

  autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

• G01P13/045

  with speed indication · CPC title

• G01C21/20

  Instruments for performing navigational calculations (G01C21/24, G01C21/26 take precedence) · CPC title

• G01P5/06

  using rotation of vanes (measuring speed of rotating shafts G01P3/00) · CPC title