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公开(公告)号:US11118621B2
公开(公告)日:2021-09-14
申请号:US16126600
申请日:2018-09-10
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Dae Kwan Kim
IPC: F16C3/02 , F16F15/124
Abstract: A vibration reduction shaft includes a cylindrical outer shaft having an inner hollow portion, in which the outer shaft includes: a first member (110) and a second member (120) which are disposed to be spaced apart from each other in a longitudinal direction of the shaft; and a vibration reduction region (150) which is disposed between the first member and the second member, and multiple connecting members (151), which connect the first member and the second member in an axial direction, are disposed to be spaced apart from one another within the vibration reduction region.
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公开(公告)号:US12183983B2
公开(公告)日:2024-12-31
申请号:US17738338
申请日:2022-05-06
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Dae Kwan Kim
Abstract: A method of optimizing driving of an antenna for communication of an artificial satellite, by controlling a rotation angle of the antenna, according to an embodiment of the disclosure, includes: receiving a basic profile indicating a change in a rotation angle of the antenna such that a center line of the antenna points to a ground station in response to movement of the artificial satellite; determining a processing section with reference to points at which a rotation velocity of the antenna, for the basic profile, is zero; and generating an optimization profile that determines the change in the rotation angle of the antenna by configuring the rotation velocity of the antenna, for the processing section, with a preset optimized rotation velocity.
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公开(公告)号:US09752644B2
公开(公告)日:2017-09-05
申请号:US15101657
申请日:2014-12-02
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Dae Kwan Kim , Hong-Taek Choi
CPC classification number: F16F15/08 , B64G2001/228 , F16M11/22 , F16M2200/08
Abstract: Provided is a non-adhesive type vibration reduction apparatus comprising: a support; a body; and an elastomer, wherein the elastomer is coupled in a non-adhesive manner in which an adhesive is not used, thereby preventing a separation of and reducing a damage of an elastomer which result from a weakening of an adhesive force.
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公开(公告)号:US11029411B2
公开(公告)日:2021-06-08
申请号:US16009008
申请日:2018-06-14
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Seon Ho Lee , Jae Cheol Yoon , Dae Kwan Kim
Abstract: Disclosed is a method and apparatus for correcting a satellite image acquisition time. The method may include receiving, from a ground-based orbit propagator, an initially predicted imaging time, a correction command execution time, and a desired satellite position for imaging, and calculating a waiting time for imaging, a predicted satellite position, a correction time, and a corrected imaging time to correct a satellite image acquisition time.
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公开(公告)号:US10605305B2
公开(公告)日:2020-03-31
申请号:US16130474
申请日:2018-09-13
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Dae Kwan Kim
IPC: F16C27/06 , F16F15/124 , F16F1/373 , F16F15/12
Abstract: Provided is a vibration reduction device for a bearing, including: a bearing tube (50) which is spaced apart from an outer race of a bearing at a predetermined interval and surrounds the outer race; and a link (100) which is disposed between the outer race and the bearing tube, in which the link includes an outer race connecting portion (120) which is in contact with the outer race, and a tube connecting portion (130) which is in contact with the bearing tube, such that vibration reduction performance is implemented by the bearing tube and the link installed at an outer side of the bearing, and as a result, the vibration reduction device may be applied to various fields in which it is necessary to minimize vibration.
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公开(公告)号:US20180372882A1
公开(公告)日:2018-12-27
申请号:US16009008
申请日:2018-06-14
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Seon Ho Lee , Jae Cheol Yoon , Dae Kwan Kim
Abstract: Disclosed is a method and apparatus for correcting a satellite image acquisition time. The method may include receiving, from a ground-based orbit propagator, an initially predicted imaging time, a correction command execution time, and a desired satellite position for imaging, and calculating a waiting time for imaging, a predicted satellite position, a correction time, and a corrected imaging time to correct a satellite image acquisition time.
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