公开(公告)号：US20210260281A1

公开(公告)日：2021-08-26

申请号：US17254994

申请日：2019-05-27

Applicant: KOREA AEROSPACE RESEARCH INSTITUTE

Inventor： Poo Min PARK ,  Hyung Mo KIM ,  Tae Choon PARK ,  Young Seok KANG ,  Jae Sung HUH ,  Doo Yong LEE

IPC: A61M5/168

Abstract: The present disclosure provides an infusion flow regulator, including: a main body (10) having an inlet through which fluid is introduced and an outlet through which the fluid is discharged; and a rotary dial (30) rotatably coupled to the main body, with a sealing member (20) interposed therebetween, so as to regulate the flow rate of the fluid, in which the rotary dial includes a regulating flow path (31) having a shape of a recessed groove in cross section with a first width and a first height, and the regulating flow path (31) includes a first region in which the width is constant and the height is decreased, and a second region in which both the width and height are decreased. By the configuration described above, the device for regulating infusion solution according to the present disclosure has an effect of accurately regulating the flow rate even in a region where the flow rate of the infusion solution is a very small.

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。