IP Library › Granted Patent US 12,415,498
Granted Patent B2
US 12,415,498 · App. 18/315,756 · Granted Sep 16, 2025

Hybrid engine system and method of controlling the same

Inventor: Chun Taek Kim (Daejeon, KR)
Assignee: KOREA AEROSPACE RESEARCH INSTITUTE
B60W10/08B60W10/06B60W10/26B60W2710/0666
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Quick Facts
Patent No.
US 12,415,498
App. No.
18/315,756
Granted
Sep 16, 2025
Kind
B2
Abstract

A hybrid engine system includes: an engine; a generator driven by the engine to output electrical energy; a battery configured to store electrical energy produced by the generator or supply electrical energy together with the generator; and a controller configured to control the engine, wherein the controller includes a torque meter for measuring torque of an output shaft of the engine and a current meter for measuring output current of the generator, and is further configured to change a control mode of the engine when a reduction rate of at least one of the torque and the current is greater than a set value while the engine is operating in a fly mode.

Claims (20)

1. A hybrid engine system comprising:

an engine;

a generator driven by the engine and configured to output electrical energy;

a battery configured to store the electrical energy produced by the generator or supply the electrical energy together with the generator; and

a controller configured to control the engine,

wherein the controller includes a torque meter configured to measure a torque of an output shaft of the engine and a current meter configured to measure an output current of the generator, and the controller is further configured to change a control mode of the engine when a reduction rate of at least one of the torque and the current is greater than a set value while the engine is operating in a fly mode.

2. The hybrid engine system of claim 1 , wherein the controller is further configured to drive the engine in a stop mode in which the engine is stopped for a set time when a reduction rate of the torque is greater than a first torque reduction rate or a reduction rate of the current is greater than a first current reduction rate.

3. The hybrid engine system of claim 2 , wherein the controller is further configured to idle the engine after the set time has elapsed in the stop mode and then drive the engine in the fly mode.

4. The hybrid engine system of claim 1 , wherein the controller is further configured to drive the engine in an idle mode in which the engine is idled for a set time when a reduction rate of the torque is greater than a second torque reduction rate or a reduction rate of the current is greater than a second current reduction rate.

5. The hybrid engine system of claim 1 , wherein the controller is further configured to drive the engine in a deceleration rate control mode in which a set value of a maximum deceleration rate of the engine is increased when a reduction rate of the torque is greater than a second torque reduction rate or a reduction rate of the current is greater than a second current reduction rate.

6. A method of controlling a hybrid engine system, the method comprising:

a fly mode driving operation of driving an engine in a fly mode;

a reduction rate determination operation of measuring torque of an output shaft of the engine and output current of a generator connected to the output shaft of the engine and comparing a reduction rate of the torque and a reduction rate of the current with a set value; and

a mode change operation of changing a control mode of the engine according to the reduction rate determination operation.

7. The method of claim 6 , wherein the reduction rate determining operation includes a first reduction rate determination operation of comparing the reduction rate of the torque with a first torque reduction rate and comparing the reduction rate of the current with a first current reduction rate, wherein, when the reduction rate of the torque is greater than the first torque reduction rate or the reduction rate of the current is greater than the first current reduction rate, the control mode is changed, in the mode change operation, to a stop mode in which the engine is stopped for a set time.

8. The method of claim 7 , wherein the engine is idled after the set time has elapsed in the stop mode and then is driven in the fly mode.

9. The method of claim 7 , wherein the reduction rate determination operation includes a second reduction rate determination operation of comparing the reduction rate of the torque with a second torque reduction rate and the reduction rate of the current with a second current reduction rate when, in the first reduction rate determination operation, the reduction rate of the torque is not greater than the first torque reduction rate and the reduction rate of the current is not greater than the first current reduction rate, wherein, when the reduction rate of the torque is greater than the second torque reduction rate or the reduction rate of the current is greater than the second current reduction rate, the control mode is changed, in the mode change operation, to an idle mode in which the engine is idled for a set time.

10. The method of claim 7 , wherein the reduction rate determination operation includes a second reduction rate determination operation of comparing the reduction rate of the torque with a second torque reduction rate and the reduction rate of the current with a second current reduction rate when, in the first reduction rate determination operation, the reduction rate of the torque is not greater than the first torque reduction rate and the reduction rate of the current is not greater than the first current reduction rate, wherein, when the reduction rate of the torque is greater than the second torque reduction rate or the reduction rate of the current is greater than the second current reduction rate, the control mode is changed to a deceleration rate control mode in which a set value of a maximum deceleration rate of the engine is increased.

11. The method of claim 6 , wherein the reduction rate determination operation includes a second reduction rate determination operation of comparing the reduction rate of the torque with a second torque reduction rate and comparing the reduction rate of the current with a second current reduction rate, wherein, when the reduction rate of the torque is greater than the second torque reduction rate or the reduction rate of the current is greater than the second current reduction rate, the control mode is changed, in the mode change operation, to an idle mode in which the engine is idled for a set time.

12. The method of claim 6 , wherein the reduction rate determination operation includes a second reduction rate determination operation of comparing the reduction rate of the torque with a second torque reduction rate and comparing the reduction rate of the current with a second current reduction rate, wherein, when the reduction rate of the torque is greater than the second torque reduction rate or the reduction rate of the current is greater than the second current reduction rate, the control mode is changed to a deceleration rate control mode for increasing a set value of a maximum deceleration rate of the engine.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 11, 2023
From: KIM, CHUN TAEK
To: KOREA AEROSPACE RESEARCH INSTITUTE
Reel/Frame 063613/0387 →
Priority Claims (1)
KR 10-2022-0075687 · Jun 21, 2022 · national
Continuity (1)
Related Publication 20240067154A1 · Feb 29, 2024
References Cited (10)
US 8875519B2 · Dooley · 2014 [cited by examiner]
US 10112723B2 · Rossotto et al. · 2018 [cited by applicant]
US 20130291830A1 · Doering · 2013 [cited by examiner]
US 20220135018A1 · Sheidler · 2022 [cited by examiner]
US 20220290606A1 · Matsumoto et al. · 2022 [cited by applicant]
EP 3613674 · 2020 [cited by applicant]
JP 2000097063 · 2000 [cited by applicant]
JP 4108450B2 · 2008 [cited by examiner]
JP 2022137452 · 2022 [cited by applicant]
KR 20170018671 · 2017 [cited by applicant]