IP Library › Granted Patent US 12,339,157
Granted Patent B2
US 12,339,157 · App. 17/928,380 · Granted Jun 24, 2025

Flight device

Inventors: Yasutoshi Ono (Ota, JP); Mitsuru Ishikawa (Ota, JP)
Assignee: ISHIKAWA ENERGY RESEARCH CO., LTD.
G01G19/08B64C39/024B64U50/19B64U50/30G05D1/0816B64U10/14B64U2101/40B64U2101/45B64U2201/20
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Quick Facts
Patent No.
US 12,339,157
App. No.
17/928,380
Granted
Jun 24, 2025
Kind
B2
Abstract

The present invention provides a flying apparatus that can accurately measure a weight of a transported objected in a simple configuration. The flying apparatus 10 includes rotors 11 , motors 12 , a flight sensor 13 , an electric power conversion unit 14 , and a computation control unit 15 . The flight sensor 13 measures physical quantities acting on a fuselage base portion 16 . The computation control unit 15 generates instruction signals based on the physical quantities to cause the fuselage base portion 16 to be at a predetermined position in a predetermined attitude. The electric power conversion unit 14 adjusts amounts of electric power supplied to the motors 121 and the like based on the received instruction signals. Moreover, the computation control unit 15 calculates an estimated weight that is an estimation value of a weight of the transported object, based on magnitudes of the instruction signals.

Claims (49)

1. A flying apparatus that transports a transported object, comprising:

a rotor;

a motor;

a flight sensor;

an electric power conversion unit;

a battery that supplies electric power to the electric power conversion unit; and

a computation control unit, wherein

the rotor is rotated to generate thrust for causing a fuselage base portion to go airborne,

the motor rotationally drives the rotor,

the flight sensor measures a physical quantity acting on the fuselage base portion,

the computation control unit generates an instruction signal based on the physical quantity to cause the fuselage base portion to be at a predetermined position in a predetermined attitude,

the electric power conversion unit adjusts an amount of electric power supplied to the motor based on the received instruction signal,

the computation control unit calculates an estimated weight that is an estimation value of a weight of the transported object, based on a magnitude of the instruction signal, and

the computation control unit calculates the estimated weight based on the instruction signal and a voltage value of the battery.

2. The flying apparatus according to claim 1 , further comprising a spraying device, wherein

the transported object is an agent sprayed by the spraying device,

the computation control unit calculates an estimated remaining amount that is an estimation value of a remaining amount of the agent, based on the magnitude of the instruction signal.

3. The flying apparatus according to claim 1 , wherein

the flying apparatus includes a plurality of the rotors, a plurality of the motors, and a plurality of the electric power conversion units, and

the computation control unit

generates a plurality of the instruction signals to be inputted into the respective electric power conversion units, and

estimates the estimated weight of the transported object based on an instruction signal average value that is an average value of the instruction signals.

4. The flying apparatus according to claim 1 , wherein a signal indicating the estimated weight is transmitted to a display device, and the estimated weight is displayed on a display unit of the display device.

5. A method of operating a flying apparatus that transports a transported object, the flying apparatus comprising:

a rotor;

a motor;

a flight sensor;

an electric power conversion unit; and

a battery that supplies electric power to the electric power conversion unit, wherein

the rotor is rotated to generate thrust for causing a fuselage base portion to go airborne,

the motor rotationally drives the rotor, and

the method comprises:

measuring a physical quantity acting on the fuselage base portion by the flight sensor,

generating an instruction signal based on the physical quantity to cause the fuselage base portion to be at a predetermined position in a predetermined attitude,

adjusting an amount of electric power supplied to the motor based on the received instruction signal by the electric power conversion unit, and

calculating an estimated weight that is an estimation value of a weight of the transported object, based on a magnitude of the instruction signal,

wherein the calculating step further comprises calculating the estimated weight based on the instruction signal and a voltage value of the battery.

6. The method according to claim 5 , wherein

the flying apparatus further comprises a spraying device, and

the transported object is an agent sprayed by the spraying device, and

the method includes calculating an estimated remaining amount that is an estimation value of a remaining amount of the agent, based on the magnitude of the instruction signal.

7. The method according to claim 5 , wherein

the flying apparatus includes a plurality of the rotors, a plurality of the motors, and a plurality of the electric power conversion units, and

the method comprises:

generating a plurality of the instruction signals to be inputted into the respective electric power conversion units, and

estimating the estimated weight of the transported object based on an instruction signal average value that is an average value of the instruction signals.

8. The method according to claim 5 , comprising:

transmitting a signal indicating the estimated weight to a display device, and

displaying the estimated weight on a display unit of the display device.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 29, 2022
From: ONO, YASUTOSHI; ISHIKAWA, MITSURU
To: ISHIKAWA ENERGY RESEARCH CO., LTD.
Reel/Frame 061906/0286 →
Priority Claims (1)
JP 2021-063661 · Apr 2, 2021 · national
Continuity (1)
Related Publication 20230221166A1 · Jul 13, 2023
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