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公开(公告)号：KR1020110068080A
公开(公告)日：2011-06-22
申请号：KR1020090124915
申请日：2009-12-15
Applicant: 한국항공우주연구원
Abstract: PURPOSE: An overflow prevention valve and a hydro-pneumatic system including the same are provided to prevent water hammering without a bypass system. CONSTITUTION: An overflow prevention valve(120) comprises a body(121), a spring supporter(122), a spring(123), and an orifice(124). The body has a flow path(129) which fluid flows through and raised protrusions(121a,121b). The spring supporter is coupled to the middle of the body flow path. The spring is coupled to one side of the spring supporter and extended or compressed according to the differential pressure of the flow path. The orifice contacts the raised protrusions to block the flow path when the differential pressure of the flow path exceeds the designated differential pressure.
Abstract translation: 目的：提供防溢流阀和包括该溢流防止阀的液压气动系统，以防止没有旁路系统的水击。 构成：溢流防止阀（120）包括主体（121），弹簧支撑件（122），弹簧（123）和孔口（124）。 主体具有流体流过并突出的突起（121a，121b）的流动路径（129）。 弹簧支撑件联接到身体流动路径的中间。 弹簧联接到弹簧支撑件的一侧，并且根据流动路径的压差被延伸或压缩。 当流路的压差超过指定的压差时，孔与凸起突起接触以阻塞流路。
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公开(公告)号：KR1020060072883A
公开(公告)日：2006-06-28
申请号：KR1020040111648
申请日：2004-12-24
Applicant: 한국항공우주연구원
Abstract: 본 발명은 두 개의 배관을 연결해 주는 배관연결장치에 관한 것으로서, 보다 상세하게는 주름관을 갖는 주름관형 배관연결장치에 관한 것이다. 본 발명에 의한 이중 주름관형 진공단열 배관연결장치는 양단으로 각각 배관이 연결되며 유체의 통로가 되는 내부 주름관; 소정 간격을 두고 내부 주름관을 감싸는 외부 주름관; 외부 주름관에 형성되는 진공펌핑용 포트; 이 포트에 연결되는, 펌핑된 공기에 대한 역류방지수단; 내부 주름관 및 외부 주름관의 일단을 상호간에 밀봉하고 그 타단을 상호간에 밀봉하여 폐공간을 형성하는 제1 및 제2밀봉수단; 및 진공펌핑에 의한 내부 및 외부 주름관의 길이방향 수축을 억제하는 수축억제수단을 포함한다. 본 발명은 진공단열 기능을 수행하면서도 필요시 굴절이 가능하다.
김발, 발사체, 벨로우즈, 단열, 배관-
公开(公告)号：KR1020030052124A
公开(公告)日：2003-06-26
申请号：KR1020010082016
申请日：2001-12-20
Applicant: 한국항공우주연구원
IPC: B64G5/00
Abstract: PURPOSE: A mechanical separating valve is provided to prevent the leakage of an injection and a discharge of a propellant. CONSTITUTION: A body(2) for a ground has a groove(8) in the front side. A spring(6) is adjusted with a separating load in the back of the body for the ground. A spring guide(5) is installed in the outside of the spring, formed with a screw portion(5') therein and installed with a ball(4) in the front side. A separating load adjusting portion(7) adjusts the separating load of the spring by forming a screw portion(7') to be combined with the screw portion of the spring guide. After separating a valve, the spring is reusable by inserting the ball.
Abstract translation: 目的：提供机械分离阀，以防止喷射剂的泄漏和推进剂的排放。 构成：用于地面的主体（2）在前侧具有凹槽（8）。 弹簧（6）用在地面后部的分离载荷进行调节。 弹簧导向件（5）安装在弹簧的外侧，在其中形成有螺纹部分（5'），并在前侧安装有球（4）。 分离负载调整部（7）通过形成与弹簧引导件的螺纹部组合的螺纹部（7'）来调节弹簧的分离载荷。 分离阀后，弹簧可以通过插入球来重复使用。
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公开(公告)号：KR1020030052123A
公开(公告)日：2003-06-26
申请号：KR1020010082015
申请日：2001-12-20
Applicant: 한국항공우주연구원
IPC: B64D7/08
Abstract: PURPOSE: A mechanical separating valve is provided to prevent the leakage by completely composing an internal sealing structure. CONSTITUTION: A body(1) for a launching member has a combining groove. A body(2) for a ground is combined with the body for the launching member and installed with a fixing member(15) by a packing bolt(12). A connecting member(3) is combined with the body for the ground by a lock nut(9) and has a combining protrusion by protruding a protruded portion. The body for the ground are installed in a double structure by a seal(4) for maintaining an interval and a packing(5) in the fixing member. The connecting member is combined and separated by forming a cut portion in the protruded portion. Thereby, the leakage of fluid of very low temperature is prevented by tightening the bolt of a valve at the generation of the leakage.
Abstract translation: 目的：提供机械分离阀，通过完全组成内部密封结构来防止泄漏。 构成：用于发射构件的主体（1）具有组合凹槽。 用于地面的主体（2）与用于发射构件的主体组合并且通过密封螺栓（12）安装有固定构件（15）。 连接构件（3）通过锁定螺母（9）与用于地面的主体组合，并且通过突出突出部分具有组合突起。 用于地面的主体通过用于保持间隔的密封件（4）和密封件（5）安装在双重结构中。 连接构件通过在突出部分中形成切口部分而组合和分离。 因此，通过在产生泄漏时拧紧阀的螺栓来防止非常低温度的流体的泄漏。
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公开(公告)号：KR100868075B1
公开(公告)日：2008-11-11
申请号：KR1020070107298
申请日：2007-10-24
Applicant: 한국항공우주연구원
Abstract: A diffuser for pressurizing and a liquid propellant rocket using the same are provided to prevent the drop of the pressurized gas by passing through the diffuser and spray the pressurized gas uniformly in the whole area of the outlet of the diffuser. An inflow pipe is arranged in one side of a storage tank and the pressurized gas is inputted to the inflow pipe. A diffuser body is equipped in the bottom of the inflow pipe and sprays the pressurized gas into the inside of the storage tank. A conical pitching plate(110) is equipped inside the diffuser and includes a plurality of flow holes in a plate with a conical shape. The conical pitching plate is separated from the diffuser body with a predetermined interval and is installed adjacently to the inflow pipe. A support stand(120) is arranged in the bottom of the conical pitching plate and is installed in the diffuser body. The support stand supports the conical pitching plate.
Abstract translation: 提供用于加压的扩散器和使用其的液体推进剂火箭，以防止加压气体通过扩散器而下降，并将加压气体均匀地喷射在扩散器的出口的整个区域中。 流入管布置在储罐的一侧，加压气体输入到流入管中。 在流入管的底部装有扩散器主体，并将加压气体喷射到储罐的内部。 在扩散器内部装有锥形俯仰板（110），并且在圆板形状的板中包括多个流动孔。 锥形俯仰板以预定间隔与扩散体本体分离，并与流入管相邻地安装。 支撑架（120）布置在锥形俯仰板的底部，并安装在扩散器主体中。 支撑台支撑锥形投影板。
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Patent Agency Ranking
公开(公告)号：KR1020040009407A
公开(公告)日：2004-01-31
申请号：KR1020020043345
申请日：2002-07-23
Applicant: 한국항공우주연구원
IPC: F02K9/96
Abstract: PURPOSE: A fixing structure is provided to achieve improved accuracy of data, while allowing the test environment to be similar to the actual environment. CONSTITUTION: A fixing structure comprises an upper fixed member(12) and a lower fixed member(14) coupled to the top and lower portion of a pressure tank; and a connection shaft(20) penetrating through a coupling bracket(16) mounted on the upper and lower fixed members, wherein the connection shaft has an end coupled to a coupling bracket mounted on a fuel tank through a pair of adjustment nuts. The end of the shaft is coupled with a fixing nut(24) for restraining the movement of the upper and lower fixed members.
Abstract translation: 目的：提供固定结构，以提高数据的准确性，同时允许测试环境与实际环境相似。 构成：固定结构包括联接到压力罐的顶部和下部的上部固定构件（12）和下部固定构件（14）; 以及穿过安装在所述上下固定构件上的联接支架（16）的连接轴（20），其中所述连接轴具有通过一对调节螺母联接到安装在燃料箱上的联接支架的一端。 轴的端部与用于限制上固定构件和下固定构件的运动的固定螺母（24）联接。
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公开(公告)号：KR100446017B1
公开(公告)日：2004-08-30
申请号：KR1020010082016
申请日：2001-12-20
Applicant: 한국항공우주연구원
IPC: B64G5/00
Abstract: PURPOSE: A mechanical separating valve is provided to prevent the leakage of an injection and a discharge of a propellant. CONSTITUTION: A body(2) for a ground has a groove(8) in the front side. A spring(6) is adjusted with a separating load in the back of the body for the ground. A spring guide(5) is installed in the outside of the spring, formed with a screw portion(5') therein and installed with a ball(4) in the front side. A separating load adjusting portion(7) adjusts the separating load of the spring by forming a screw portion(7') to be combined with the screw portion of the spring guide. After separating a valve, the spring is reusable by inserting the ball.
Abstract translation: 目的：提供机械分离阀以防止喷射剂和喷射剂的泄漏。 组成：用于地面的本体（2）在前侧具有凹槽（8）。 弹簧（6）通过身体后部的分离载荷调整地面。 弹簧导向件（5）安装在弹簧的外侧，在其中形成有螺纹部分（5'）并且在前侧安装有球（4）。 分离载荷调节部分（7）通过形成与弹簧导向件的螺纹部分结合的螺纹部分（7'）来调节弹簧的分离载荷。 分离阀门后，通过插入球体可重复使用弹簧。
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公开(公告)号：KR100445681B1
公开(公告)日：2004-08-21
申请号：KR1020010082015
申请日：2001-12-20
Applicant: 한국항공우주연구원
IPC: B64D7/08
Abstract: PURPOSE: A mechanical separating valve is provided to prevent the leakage by completely composing an internal sealing structure. CONSTITUTION: A body(1) for a launching member has a combining groove. A body(2) for a ground is combined with the body for the launching member and installed with a fixing member(15) by a packing bolt(12). A connecting member(3) is combined with the body for the ground by a lock nut(9) and has a combining protrusion by protruding a protruded portion. The body for the ground are installed in a double structure by a seal(4) for maintaining an interval and a packing(5) in the fixing member. The connecting member is combined and separated by forming a cut portion in the protruded portion. Thereby, the leakage of fluid of very low temperature is prevented by tightening the bolt of a valve at the generation of the leakage.
Abstract translation: 目的：提供机械分离阀，以通过完全构成内部密封结构来防止泄漏。 构成：用于发射构件的主体（1）具有结合凹槽。 用于地面的主体（2）与用于发射构件的主体结合并且通过密封螺栓（12）安装有固定构件（15）。 连接构件（3）通过锁定螺母（9）与地面主体结合，并且通过突出突出部分而具有结合突起。 通过用于在固定构件中保持间隔和密封件（5）的密封件（4）将地面主体安装成双层结构。 连接构件通过在突出部分中形成切口部分而结合并分离。 由此，通过在发生泄漏时拧紧阀门的螺栓来防止极低温度的流体泄漏。
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公开(公告)号：KR101576752B1
公开(公告)日：2015-12-10
申请号：KR1020140167343
申请日：2014-11-27
Applicant: 한국항공우주연구원
Inventor： 권오성
IPC: F16K1/34 , F16K17/04 , F16K27/02 , F16K31/122
Abstract: 본발명은벤트기능과릴리프기능을갖는밸브장치및 그작동방법에관한것으로서, 더욱상세하게는벤트기능을갖는벤트밸브와릴리프기능을갖는릴리프밸브를겸용으로사용할수 있도록하는한편, 벤트모드와릴리프모드의상태에따라배출구의유로면적이다르게조절될수 있도록하기위한벤트기능과릴리프기능을갖는밸브장치및 그작동방법에관한것이다.
Abstract translation: 本发明涉及一种具有通气功能和释放功能的阀装置及其操作方法，更具体地涉及一种具有排气功能和排泄功能的阀装置及其操作方法，其能够使排气口 具有排气功能的阀和具有能够一起使用的释放功能的安全阀，并且还能够根据排气模式和排气模式的状态使排出口的流路面积被不同地控制。
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公开(公告)号：KR101376384B1
公开(公告)日：2014-03-20
申请号：KR1020120114132
申请日：2012-10-15
Applicant: 한국항공우주연구원
Inventor： 권오성
Abstract: Disclosed are a device and a method for decelerating an object falling along the chamber of a drop tower. The device for decelerating a falling object of a drop tower, according to an embodiment, incudes: a hollow pipe-shaped catch tube formed with an accommodating portion where the falling object is accommodated; a reception portion provided inside the catch tube, to receive the falling object; and a gas supplying unit which jets gas from the bottom to the top of the catch tube, in order to decelerate the falling object, using the pressure of the gas.
Abstract translation: 公开了一种用于使沿着落下塔的室落下的物体减速的装置和方法。 根据一个实施例，用于使滴塔的落下物体减速的装置包括：形成有容纳部分的中空管状捕获管，其中容纳坠落物体; 接收部，设置在所述卡止管内部，以接收所述下落物体; 以及从吸管的底部到顶部喷射气体的气体供给单元，以便使用气体的压力来减速坠落物体。
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