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公开(公告)号:US11927974B2
公开(公告)日:2024-03-12
申请号:US17528365
申请日:2021-11-17
Applicant: Korea Aerospace Research Institute
Inventor: Kwang Kun Park , Jun Seong Lee , Kee Joo Lee
Abstract: The flow rate control device includes a main plate corresponding to an inner diameter and including a through hole which is formed at the center thereof and through which a fluid flows, a sub-plate corresponding to a size of the through hole, disposed in front of the main plate, and applied with a pressure of the flowing fluid, and an expansion and contraction flow path formed to connect the through hole and a circumference of the sub-plate to each other and expanded and contracted by the pressure applied to the sub-plate. The expansion and contraction flow path includes a plurality of holes which are formed in a side surface thereof and through which the flow flows, and has a cross-sectional area changed by the pressure to control a flow rate.
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公开(公告)号:US11691759B2
公开(公告)日:2023-07-04
申请号:US17546400
申请日:2021-12-09
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Sung Hyuck Im , Jun Seong Lee , Kee Joo Lee , Jae Sung Park
IPC: B64F1/02
CPC classification number: B64F1/0297
Abstract: A projectile landing apparatus for retrieving a projectile includes a plurality of grippers disposed to be spaced apart. The plurality of grippers may include a support, a guide having one side connected to one end of the support, and a shock absorber having one end connected to the other end of the support and having the other end connected to the guide. The plurality of grippers may guide a projectile, buffer a load, and safely retrieve the projectile.
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公开(公告)号:US20220163982A1
公开(公告)日:2022-05-26
申请号:US17528365
申请日:2021-11-17
Applicant: Korea Aerospace Research Institute
Inventor: Kwang Kun Park , Jun Seong Lee , Kee Joo Lee
Abstract: The flow rate control device includes a main plate corresponding to an inner diameter and including a through hole which is formed at the center thereof and through which a fluid flows, a sub-plate corresponding to a size of the through hole, disposed in front of the main plate, and applied with a pressure of the flowing fluid, and an expansion and contraction flow path formed to connect the through hole and a circumference of the sub-plate to each other and expanded and contracted by the pressure applied to the sub-plate. The expansion and contraction flow path includes a plurality of holes which are formed in a side surface thereof and through which the flow flows, and has a cross-sectional area changed by the pressure to control a flow rate.
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公开(公告)号:US11926441B2
公开(公告)日:2024-03-12
申请号:US17555848
申请日:2021-12-20
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Sung Hyuck Im , Jun Seong Lee , Kee Joo Lee , Jae Sung Park
Abstract: An orbit transition apparatus that transitions an orbit of a payload in outer space includes a rotating body, an adapter disposed on a center part of the rotating body for docking a payload, a launch module disposed outside of the rotating body for launching the payload, and a thruster for rotating the rotating body. The launch module may launch the payload to a target orbit.
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公开(公告)号:US20220258883A1
公开(公告)日:2022-08-18
申请号:US17546400
申请日:2021-12-09
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Sung Hyuck Im , Jun Seong Lee , Kee Joo Lee , Jae Sung Park
IPC: B64F1/02
Abstract: A projectile landing apparatus for retrieving a projectile includes a plurality of grippers disposed to be spaced apart. The plurality of grippers may include a support, a guide having one side connected to one end of the support, and a shock absorber having one end connected to the other end of the support and having the other end connected to the guide. The plurality of grippers may guide a projectile, buffer a load, and safely retrieve the projectile.
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