Long range electric aircraft and method of operating same

• US 9,815,563 B2
• Filed: 04/04/2016
• Issued: 11/14/2017
• Est. Priority Date: 03/30/2012
• Status: Active Grant

• Current Assignee: Ampaire, Inc.
• Original Assignee: W.Morrison Consulting Group, Inc.
• Inventors: Yates, William M., Ussery, Robert, Young, Byron
• Primary Examiner(s): Sanderson, Joseph W
• Application Number:
  US15/090,571
• Publication Number:
  US 20160288918A1
• Time in Patent Office: 589 Days
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: B64D 39/00 Refuelling during flight filling or emptying fuel tanks B64D37/14
• CPC Class Codes: B64D 5/00 Aircraft transported by aircraft, e.g. for release or reberthing during flight flying units formed by separate aircraft B64C37/02
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/10 Wings
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: B64U 70/60 Take-off or landing of UAVs from a runway using their own power

Abstract

Electric aircraft, including in-flight rechargeable electric aircraft, and methods of operating electric aircraft, including methods for recharging electric aircraft in-flight, through the use of unmanned aerial vehicle (UAV) packs flying independent of and in proximity to the electric aircraft.

Claims

1. An in-flight method of charging a first aircraft having a propulsion system at least partially powered by electricity, said method comprising:

flying a second aircraft in proximity to the first aircraft;

coordinating the flight movements of the first aircraft and second aircraft by wirelessly controlling actuators located on the second aircraft by transmitting control signals from the first aircraft to the second aircraft;

establishing an electrical connection between the first aircraft and the second aircraft; and

transferring electricity from the second aircraft to the first aircraft through the electrical connection.

2. The method of claim 1, wherein the second aircraft is a manned aircraft.

3. The method of claim 1, wherein the second aircraft is a UAV.

4. The method of claim 1, wherein establishing an electrical connection between the first aircraft and the second aircraft comprises:

extending one of a charging cable or a boom between the first aircraft and the second aircraft, and wherein the electricity is transferred from an electricity source associated with the second aircraft to the first aircraft through the charging cable or boom.

5. The method of claim 4, wherein extending the charging cable or boom between the first aircraft and the second aircraft comprises:

extending the charging cable or boom from the second aircraft to the first aircraft, and wherein the first aircraft is behind the second aircraft and the charging cable or boom becomes mechanically connected to the first aircraft.

6. The method of claim 5, wherein the second aircraft tows the first aircraft after the charging cable or boom becomes mechanically connected to the first aircraft.

7. The method of claim 4, wherein extending the charging cable or boom between the first aircraft and the second aircraft comprises:

extending the charging cable or boom from the first aircraft to the second aircraft, and wherein the second aircraft is behind the first aircraft and the charging cable or boom becomes mechanically connected to the second aircraft.

8. The method of claim 1, wherein the control signals are transmitted to the second aircraft prior to and after the establishment of the electrical connection between the first aircraft and the second aircraft, and wherein the control signals reflect pilot control inputs on the first aircraft.

9. The method of claim 1, wherein establishing an electrical connection between the first aircraft and the second aircraft comprises extending a charging cable between the first aircraft and the second aircraft, and wherein the method further comprises:

monitoring the tension on the charging cable; and

maintaining a desired tension level on the charging cable by adjusting forward propulsion of the first aircraft, second aircraft or both.

10. The method of claim 9, wherein monitoring the tension on the charging cable comprises:

determining the tension using a strain gauge.

11. The method of claim 9, wherein monitoring the tension on the charging cable comprises:

determining and comparing relative positions of the second aircraft and the first aircraft.

12. The method of claim 11 further comprising:

transmitting position information between the first aircraft and the second aircraft over a wireless connection.

13. The method of claim 9, wherein monitoring the tension on the charging cable comprises:

determining and comparing relative speeds of the second aircraft and the first aircraft.

14. The method of claim 13 further comprising:

transmitting speed information between the first aircraft and the second aircraft over a wireless connection.

15. The method of claim 1, wherein the control signals are processed by a flight computer on the first aircraft prior to transmission to the second aircraft.

16. The method of claim 1, wherein actuators on the second aircraft control the movement of the fight control surfaces on the second aircraft.

17. The method of claim 16, wherein the control signals are received and processed by a flight computer onboard the second aircraft prior to being transmitted to the actuators.

18. An in-flight method of charging an unmanned aerial vehicle (UAV) having a propulsion system at least partially powered by electricity, said method comprising:

flying a second aircraft in proximity to the UAV;

coordinating the flight movements of the UAV and second aircraft by wirelessly controlling actuators located on the second aircraft by transmitting control signals from the UAV to the second aircraft;

establishing an electrical connection between the UAV and the second aircraft; and

transferring electricity from the second aircraft to the UAV through the electrical connection.

19. The method of claim 18, wherein the second aircraft is a manned aircraft.

20. The method of claim 18, wherein the second aircraft is a UAV.