Method And System For Safely Landing A Battery Powered Electric VTOL Aircraft In A Low Charge Condition

Patent metadata

Field	Value
Publication number	US-2022011782-A1
Application number	US-202117364442-A
Country	US
Kind code	A1
Filing date	Jun 30, 2021
Priority date	Jun 30, 2020
Publication date	Jan 13, 2022
Grant date	—

Abstract

A system and method for use with a VTOL aircraft with batteries in a state of deep discharge which prepares the aircraft for a safe vertical landing despite the deep discharge initial condition. The method may include preparing the batteries for an intense burst of power as may be needed during the vertical landing. The method may include idling the battery, thermally conditioning the battery, and may further include charging the batteries by regenerative use of the rotors. The preparation of the batteries may then allow for a burst of power used for landing the aircraft.

First claim

What is claimed is:

1 . A method for the landing of an electrically powered aircraft in a deep discharge battery condition, said method comprising the steps of:
preparing the battery or batteries for flare control; controlling the vehicle descent rate; and arresting the vehicle motion.

2 . The method of claim 1 wherein the step of preparing the battery or batteries for flare control comprises thermally conditioning the battery.

3 . The method of claim 1 wherein the step of preparing the battery or batteries for flare control comprises idling the battery.

4 . The method of claim 1 wherein the step of preparing the battery or batteries for flare control comprises regenerating energy using the rotors of the aircraft.

5 . The method of claim 1 wherein the step of arresting the vehicle motion comprises the steps of:
determining the translational velocity of the aircraft;
determining the maximum instantaneous power of the battery or batteries; and
controlling the rotors at up to the maximum instantaneous power to arrest the vertical rate of the aircraft.

6 . The method of claim 3 wherein the step of arresting the vehicle motion comprises the steps of:
determining the translational velocity of the aircraft;
determining the maximum instantaneous power of the battery or batteries; and
controlling the rotors at up to the maximum instantaneous power to arrest the vertical rate of the aircraft.

7 . The method of claim 4 wherein the step of arresting the vehicle motion comprises the steps of:
determining the translational velocity of the aircraft;
determining the maximum instantaneous power of the battery or batteries; and
controlling the rotors at up to the maximum instantaneous power to arrest the vertical rate of the aircraft.

8 . The method of claim 1 further comprising the steps of:
determining a landing approach mode; and
determining a descent trajectory.

9 . The method of claim 4 further comprising the steps of:
determining a landing approach mode; and
determining a descent trajectory.

10 . The method of claim 7 further comprising the steps of:
determining a landing approach mode; and
determining a descent trajectory.

11 . A method for the landing of an electrically powered vertical take-off and landing aircraft, said method comprising the steps of:
determining satisfaction of a deep discharge condition; preparing the battery or batteries for flare control; controlling the vehicle descent rate; and arresting the vehicle motion.

12 . The method of claim 11 wherein the step of preparing the battery or batteries for flare control comprises thermally conditioning the battery.

13 . The method of claim 11 wherein the step of preparing the battery or batteries for flare control comprises idling the battery.

14 . The method of claim 11 wherein the step of preparing the battery or batteries for flare control comprises regenerating energy using the rotors of the aircraft.

15 . The method of claim 11 wherein the step of determining satisfaction of a deep discharge condition comprises a determination that there is no significant hover time remaining.

16 . The method of claim 14 wherein the step of determining satisfaction of a deep discharge condition comprises a determination that there is no significant hover time remaining.

17 . The method of claim 11 wherein the step of arresting the vehicle motion comprises the steps of:
determining the translational velocity of the aircraft;
determining the maximum instantaneous power of the battery or batteries; and
controlling the rotors at up to the maximum instantaneous power to arrest the vertical rate of the aircraft.

18 . The method of claim 17 wherein the step of arresting the vehicle motion comprises the steps of:
determining the translational velocity of the aircraft;
determining the maximum instantaneous power of the battery or batteries; and
controlling the rotors at up to the maximum instantaneous power to arrest the vertical rate of the aircraft.

19 . The method of claim 11 further comprising the steps of:
determining a landing approach mode; and
determining a descent trajectory.

20 . The method of claim 19 further comprising the steps of:
determining a landing approach mode; and
determining a descent trajectory

Assignees

• Joby Aero Inc

Inventors

• Mikic Gregor Veble
• Bevirt Joeben
• Stoll Alex
• Uznanski Brian Matthew

Classifications

• H02J7/82

  Control of state of charge [SOC] · CPC title

• H02J2105/32

  for aircrafts · CPC title

• H02J7/865

  Battery or charger load switching, e.g. concurrent charging and load supply (H02J7/50 takes precedence) · CPC title

• H02J7/80

  including monitoring or indicating arrangements · CPC title

• B64D31/06

  actuated automatically · CPC title