公开(公告)号：US20240067154A1

公开(公告)日：2024-02-29

申请号：US18315756

申请日：2023-05-11

Applicant: KOREA AEROSPACE RESEARCH INSTITUTE

Inventor： Chun Taek KIM

IPC: B60W10/08 ,  B60W10/06 ,  B60W10/26

CPC classification number: B60W10/08 ,  B60W10/06 ,  B60W10/26 ,  B60W2710/0666

Abstract: Provided are a hybrid engine system capable of protecting an engine from overspeeding when the load of a generator rapidly decreases, and a method of controlling the hybrid engine system.
The 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.

公开(公告)号：US20200003657A1

公开(公告)日：2020-01-02

申请号：US16453314

申请日：2019-06-26

Applicant: KOREA AEROSPACE RESEARCH INSTITUTE

Inventor： Chun Taek KIM

IPC: G01M15/14 ,  G01M15/02 ,  F01P7/14

Abstract: Provided is a cooler and an engine testing apparatus having the same. The cooler includes a guide unit configured to make a gas flow, a liquid supply unit arranged in the guide unit to supply a liquid into the guide unit, a liquid column guide unit connected to the guide unit and having a column of the liquid, and a liquid storage unit connected to the liquid column guide unit and storing the liquid.

公开(公告)号：US20160297544A1

公开(公告)日：2016-10-13

申请号：US15031933

申请日：2013-10-29

Applicant: KOREA AEROSPACE RESEARCH INSTITUTE

Inventor： Keun Bae KIM ,  Bo Hwa LEE ,  Poo Min PARK ,  Chun Taek KIM ,  Seok Min AHN ,  Soon Bae CHUNG ,  Dong Sung KIM

IPC: B64D47/00 ,  H02J9/06 ,  H02J7/35 ,  H02J3/38

CPC classification number: B64D47/00 ,  B64D27/24 ,  B64D2041/005 ,  B64D2211/00 ,  B64D2221/00 ,  H02J1/00 ,  H02J3/383 ,  H02J3/387 ,  H02J7/0068 ,  H02J7/34 ,  H02J7/35 ,  H02J9/06 ,  H02J2001/004 ,  Y02E10/563 ,  Y02T50/64 ,  Y02T90/36

Abstract: As a component of an aerial vehicle, a power management system having an active power control device is provided. The system includes a solar cell converting solar energy into electric energy; a fuel cell provided in the aerial vehicle and converting fuel energy into electric energy by electrochemical reaction; a battery compensating for a lack of electric power supplied from the solar cell and the fuel cell to the aerial vehicle and storing surplus electric power; and an active power control device connecting with all the solar cell, the fuel cell and the battery and combining and distributing electric power generated in the solar cell, the fuel cell and the battery to loads. The system efficiently distributes the power from the respective power sources through the controllable output of the fuel cell in accordance with power required by the aerial vehicle and the solar cell's performance depending on weather.

Abstract translation: 作为飞行器的组件，提供了具有有功功率控制装置的电力管理系统。 该系统包括将太阳能转换为电能的太阳能电池; 燃料电池，其设置在飞行器中并通过电化学反应将燃料能量转化为电能; 补偿从太阳能电池和燃料电池供给到飞行器的电力不足而存储剩余电力的电池; 以及与所有太阳能电池，燃料电池和电池连接并且将太阳能电池，燃料电池和电池中产生的电力组合和分配的有源电力控制装置负载。 根据天气要求，系统根据飞行器所需的功率和太阳能电池的性能，有效地分配来自各个电源的功率通过燃料电池的可控输出。