IP Library › Granted Patent US 12,030,405
Granted Patent B2
US 12,030,405 · App. 17/041,557 · Granted Jul 9, 2024

Unmanned aerial vehicle

Inventors: Chihiro Wake (Tokyo, JP); Hiroshi Yanagishita (Tokyo, JP)
Assignee: NILEWORKS INC.
B60L58/22B60L58/13B64C39/024B64D1/18B64D27/24B60L2200/10B64D2045/0085B64U10/13B64U50/19B64U2101/60
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Quick Facts
Patent No.
US 12,030,405
App. No.
17/041,557
Granted
Jul 9, 2024
Kind
B2
Abstract

An unmanned aerial vehicle and a battery, possible to be disabled when a phenomenon to cause a functional disorder, are provided. The battery includes a battery pack having a battery cell, sensors detecting a phenomenon that impairs a function of the battery pack, a memory storing a detection signal of the sensors, and block circuits blocking output of the battery pack by the detection signal. The unmanned aerial vehicle includes the battery and air frame side sensors, and operates the block circuit, which the battery includes, by the detection signal of the airframe side sensors.

Claims (58)

1. An unmanned aerial vehicle driven by an electric motor, comprising: a plurality of batteries as a drive power source for the electric motor, wherein

the plurality of batteries are connected in parallel and each include a monitoring unit to detect an abnormality or deterioration of the corresponding battery and a storage amount detection unit to detect a storage amount of the corresponding battery,

the unmanned aerial vehicle is configured to perform a plurality of emergency evacuation actions which are different depending on the storage amount of each battery,

an operation is switched to one of the plurality of emergency evacuation operations when a detection signal is output from the monitoring unit, and

the operation is switched to a first emergency evacuation operation according to the storage amount detected by the storage amount detection unit of a second battery when the storage amount detected by the storage amount detection unit of a first battery falls below a specified amount.

2. The unmanned aerial vehicle according to claim 1 , wherein the emergency evacuation operations include performing an emergency return, an emergency landing, and an emergency stop in order when the storage amount detected by the storage amount detection unit of the second battery decreases.

3. The unmanned aerial vehicle according to claim 2 , wherein the emergency return is performed in a power saving mode.

4. The unmanned aerial vehicle according to claim 3 , wherein the power saving mode is performed by restricting or releasing a part of a posture control.

5. The unmanned aerial vehicle according to claim 3 , wherein the power saving mode restricts a control in a yaw direction.

6. The unmanned aerial vehicle according to claim 3 , the unmanned aerial vehicle further comprising:

a chemical tank storing chemical liquid for spraying; and

a chemical nozzle discharging the chemical liquid;

wherein the unmanned aerial vehicle flies during the power saving mode while discharging the chemical liquid.

7. An unmanned aerial vehicle driven by an electric motor comprising:

a plurality of batteries as a drive power source for the electric motor, wherein

the plurality of batteries are connected in parallel and each include a battery monitoring unit in each battery to detect an abnormality or deterioration of the corresponding battery, a storage amount detection unit to detect a storage amount of the corresponding battery, and a detection unit monitoring unit to monitor an operation of the storage amount detection unit,

the unmanned aerial vehicle is configured to perform a plurality of emergency evacuation actions which are different depending on the storage amount of each battery,

an operation is switched to one of the plurality of emergency evacuation operations when a detection signal is output from the battery monitoring unit, and

the operation is switched to a first emergency evacuation operation when the detection unit monitoring unit of a first battery detects an abnormality in the operation of the storage amount detection unit.

8. The unmanned aerial vehicle according to claim 7 , wherein the operation is switched to the first emergency evacuation operation when the storage amount of each battery detected by each storage amount detection unit falls below a specified amount.

9. An unmanned aerial vehicle, comprising:

a plurality of rotor blades;

a plurality of electric motors individually rotating and driving each of the plurality of rotor blades;

a plurality of batteries as a power source for the electric motors;

a plurality of distribution units adjusting a power of each of the batteries to appropriate voltages and distributing the power to each of the electric motors; and

monitoring unit monitoring the plurality of distribution units;

wherein the unmanned aerial vehicle is configured to perform a plurality of emergency evacuation actions which are different depending on the storage amount of each battery,

wherein the monitoring unit monitors operation of the plurality of distribution units, and

wherein an operation is switched to a first emergency evacuation operation when an abnormality occurs in at least one of the plurality of distribution units.

10. The unmanned aerial vehicle according to claim 9 , wherein the emergency evacuation operation is an emergency return.

11. The unmanned aerial vehicle according to claim 9 , wherein the emergency evacuation operation is an emergency landing or an emergency stop.

12. An unmanned aerial vehicle, comprising:

a plurality of rotor blades;

a plurality of electric motors individually rotating each of the plurality of rotor blades;

a plurality of batteries as a power source for the electric motors;

a distribution unit adjusting a power of each of the plurality of batteries to appropriate voltages and distributing the power to each of the electric motors; and

a plurality of flight controllers controlling a flight of the unmanned aerial vehicle,

wherein the unmanned aerial vehicle is configured to perform a plurality of emergency evacuation actions which are different depending on the storage amount of each battery

wherein the plurality of flight controllers monitor each other or are monitored by an external monitor, and

wherein an operation is switched to a first emergency evacuation operation when an abnormality occurs in at least one of the plurality of flight controllers.

13. The unmanned aerial vehicle according to claim 12 , wherein the emergency evacuation operation is an emergency return.

14. The unmanned aerial vehicle according to claim 12 , wherein the emergency evacuation operation is an emergency landing or an emergency stop.

15. An unmanned aerial vehicle comprising:

a plurality of rotor blades;

a plurality of electric motors individually rotating each of the plurality of rotor blades;

a plurality of batteries as a power source for the electric motors;

a distribution unit adjusting a power of each of the batteries to appropriate voltages and distributing the power to each of the electric motors;

a flight controller controlling a flight of the unmanned aerial vehicle; and

a plurality of control communication lines connected to the flight controller for communicating with a sensor,

wherein the unmanned aerial vehicle is configured to perform a plurality of emergency evacuation actions which are different depending on the storage amount of each battery,

wherein an operation is switched to a first emergency evacuation operation when an abnormality occurs in at least one of the plurality of the control communication lines.

16. The unmanned aerial vehicle according to claim 15 , wherein the sensor includes at least one of a sonar, a barometric pressure sensor, a camera, and a six-axis gyro sensor.

17. An unmanned aerial vehicle driven by an electric motor, comprising:

a plurality of batteries as a drive power source for the electric motor,

wherein the plurality of batteries are connected in parallel to each other and each include a monitoring unit to detect an abnormality of the corresponding battery and an abnormality or deterioration of the corresponding battery, and a block unit to block an output of the corresponding battery when a detection signal is output from the corresponding monitoring unit,

wherein the unmanned aerial vehicle is configured to perform a plurality of emergency evacuation actions which are different depending on the storage amount of each battery,

wherein an operation is switched to a first emergency evacuation operation in a power saving mode, powered by other batteries, when an output of at least one of the plurality of the batteries is blocked by at least one of the block units, respectively, and

wherein the power saving mode is performed by restricting a posture control of the first emergency evacuation operation of one rotating axis, or by correcting an operation target value to a value smaller than a normal mode.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 17, 2020
From: WAKE, CHIHIRO; YANAGISHITA, HIROSHI
To: NILEWORKS INC.
Reel/Frame 054383/0732 →
Priority Claims (1)
JP 2018-061882 · Mar 28, 2018 · national
Continuity (1)
Related Publication 20210309122A1 · Oct 7, 2021