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1. 发明公开

KR1020170106276A 날개와 원통이 일체화된 추진 장치 및 이를 이용한 추진방법 无效
标题翻译：集成了机翼和气缸的推进装置以及使用该装置的推进方法
公开(公告)号：KR1020170106276A
公开(公告)日：2017-09-20
申请号：KR1020170116410
申请日：2017-09-12
申请人： 고신대학교 산학협력단
发明人： 김용기 , 손현근
IPC分类号： F01D15/02 , F01D15/04 , F01D1/20 , B63H11/02 , B64D27/02
CPC分类号： F01D15/02 , B63H11/02 , B64D27/02 , F01D1/20 , F01D15/04
摘要： 본발명은, 날개의회전을통해유체속도를증가시키고추진체의후방으로유체를배출하는과정에서발생하는주변유체와의반발력을이용해추진(推進)하는, 선박이나비행체등을포함한, 모든추진체에쓰일수 있는새로운형태의날개와원통이일체화된추진장치및 이를이용한추진방법에대한것으로, 본장치는로더(rotor)와유도장치및 하우징, 로더지지골조를포함하며, 특히로더(rotor)는원통(圓筒)과, 원통의내면상에서원통내면과 90도각도를이루며고정설치되는 1개이상의고정날개들과, 동력전달용림(rim) 기어및 스프로킷(sprocket)과샤프트를포함한동력전달장치와, 원통의자중을지지하는원통지지장치, 원통의진동을제어하는원통의진동제어장치, 원통의변위를제어하는원통의변위제어장치, 누수방지장치를포함하며, 유체의밀도와추진체의조건에따라, 원통의구경과길이를조정함과함께원통의내면상에설치하는고정날개들의개수와높이및 이동각도, 설치길이를조정하는방법으로날개와원통이일체화된추진장치의추진효율을높일수 있는날개와원통이일체화되어회전하는추진장치및 이를이용한추진방법을개시한다.
摘要翻译：本发明中，通过叶片的旋转增加流体速度，并使用环境流体之间的排斥力从推进剂排放流体的后部的推（推进），包括船只和飞机，在所有的推进剂被使用的过程作为使用的新型叶片和缸的推进方法被集成推进单元，这一点，本发明的装置装载器（转子）wayu还包括装置和壳体，装载机支撑框架，特别是装载器（转子），该圆筒形（圆筒）和汽缸和至少一个牢固地固定的所述内表面上的圆柱形内表面形成90 dogak更加固定刀片和一个动力传递yongrim（RIM）齿轮和链轮（链轮）和动力传递包括一个轴装置和一个圆柱形座圆柱形支撑装置，其控制所述缸单元的振动，对用于控制所述缸的位移用于支撑一个，防漏包括设备和，这取决于流体的密度和推进剂条件，气缸的气缸排量控制装置的气缸的振动控制经过的时间此调整也固定刀片数目和高度，和移动角度，用于调节所述翼的安装长度和反过来气缸的方法，它有利于推进单元的推进效率的叶片和圆筒一体的气缸的与内表面上的安装的一体旋转以及使用其的推进方法。

2. 发明公开

KR1020160122108A 날개와 원통이 일체화된 추진 장치 및 이를 이용한 추진방법 无效
标题翻译：叶片与气缸一体化的推进系统和使用其的推进方法
公开(公告)号：KR1020160122108A
公开(公告)日：2016-10-21
申请号：KR1020160132600
申请日：2016-10-13
申请人： 고신대학교 산학협력단
发明人： 김용기
IPC分类号： F01D15/02 , F01D15/04 , F01D1/20 , B63H11/02 , B64D27/02
CPC分类号： F01D15/02 , B63H11/02 , B64D27/02 , F01D1/20 , F01D15/04
摘要： 본발명은, 날개의회전을통해유체속도를증가시키고추진체의후방으로유체를배출하는과정에서발생하는주변유체와의반발력을이용해추진(推進)하는, 선박이나비행체등을포함한, 모든추진체에쓰일수 있는새로운형태의날개와원통이일체화된추진장치및 이를이용한추진방법에대한것으로, 본장치는로더(rotor)와유도장치및 하우징, 로더지지골조를포함하며, 특히로더(rotor)는원통(圓筒)과, 원통의내면상에서원통내면과 90도각도를이루며고정설치되는 1개이상의고정날개들과, 동력전달용림(rim) 기어및 스프로킷(sprocket)과샤프트를포함한동력전달장치와, 원통의자중을지지하는원통지지장치, 원통의진동을제어하는원통의진동제어장치, 원통의변위를제어하는원통의변위제어장치, 누수방지장치를포함하며, 유체의밀도와추진체의조건에따라, 원통의구경과길이를조정함과함께원통의내면상에설치하는고정날개들의개수와높이및 이동각도, 설치길이를조정하는방법으로날개와원통이일체화된추진장치의추진효율을높일수 있는날개와원통이일체화되어회전하는추진장치및 이를이용한추진방법을개시한다.

3. 发明公开

KR1020150029666A 날개와 케이싱이 일체화된 추진 장치 및 이를 이용한 추진방법 无效
标题翻译：推进装置集成刀片和套管，采用推进方法
公开(公告)号：KR1020150029666A
公开(公告)日：2015-03-18
申请号：KR1020150027696
申请日：2015-02-27
申请人： 김용기
发明人： 김용기
IPC分类号： F01D15/02 , F01D15/04 , F01D1/20 , B63H11/02 , B64D27/02
CPC分类号： F01D15/02 , B63H11/02 , B64D27/02 , F01D1/20 , F01D15/04
摘要： 본 발명은, 날개의 회전을 통해 유체속도를 증가시키고 추진체 후방으로 유체를 배출하는 과정에서 발생하는 주변유체와의 반발력을 이용해 추진(推進)하는, 선박이나 비행체 등을 포함한, 모든 추진체에 쓰일 수 있는 새로운 형태의 추진 장치 및 이를 이용한 추진방법에 대한 것으로, 본 장치는 로터(rotor)와 유도장치 및 하우징, 로터 지지 골조를 포함하며, 특히 로터(rotor)는 원통(圓筒)과, 원통 내면에서 원통 내면과 90도 각도를 이루며 고정 설치되는 1개 이상의 고정날개, 동력전달용 림(rim) 기어 및 스프로켓(sprocket)과 샤프트를 포함한 동력전달 장치, 원통의 자중을 지지하는 지지 장치, 원통의 진동을 제어하는 진동제어장치, 원통의 변위를 제어하는 변위제어장치, 누수방지장치를 포함하며, 유체 밀도와 추진체의 조건에 따라, 원통 구경과 길이를 조정함과 함께 원통 내부에 설치하는 날개 개수와 높이 및 이동각도, 설치길이를 조정하는 방법으로 추진효율을 높일 수 있는 날개와 원통이 일체화되어 회전하는 추진 장치 및 이를 이용한 추진방법을 개시한다.
摘要翻译：本发明涉及一种新型的推进系统，其可以通过叶片的旋转来增加流体速度，并且可以用于所有推进剂，包括使用排斥力推进的船舶和飞机，以及在排放过程中产生的周围流体推进剂后部的流体，以及使用其的推进方法。本发明的推进系统包括：转子; 指导系统; 房屋; 和转子支撑框架，其中所述转子包括：气缸; 一个或多个固定刀片相对于气缸的内表面以90度的角度安装在气缸的内表面上; 动力传递装置，包括动力传递轮辋齿轮，链轮和轴; 支撑装置，用于支撑气缸的重量; 控制气缸振动的振动控制装置; 位移控制装置，用于控制气缸的位移; 和防漏装置。其中叶片和气缸一体化并旋转的推进系统可以通过调节安装在气缸内的叶片的数量，高度，移动角度和安装长度来调节气缸的直径和长度来提高推进效率，对流体的密度和推进剂的状态。

4. 发明公开

KR1020130126192A 반작용식 터빈 无效
标题翻译：反应型涡轮机
公开(公告)号：KR1020130126192A
公开(公告)日：2013-11-20
申请号：KR1020120050078
申请日：2012-05-11
申请人： 주식회사 에이치케이터빈
发明人： 장영일 , 하용식 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D25/24
CPC分类号： F01D1/32 , F01D1/04 , F01D1/20 , F01D1/34 , F01D25/24 , F05D2220/30
摘要： A reaction type turbine according to the present invention includes a rotary shaft enlarging member joined to a rotary shaft between a housing inlet and a rotor. As the pressing area on which working fluid applies pressure to the rotary shaft in a direction opposite to a flowing direction, the power to the direction opposite to the flowing direction is increase so that thrust applied to the flowing direction of the working fluid can be reduced. Therefore, the installation of a separate thrust bearing for supporting the thrust in the flowing direction is not necessary. Furthermore, the rotary shaft enlarging member is separately formed to have the diameter larger than the diameter of the rotary shaft and joined to the rotary shaft so that time and expenses for enlarging the diameter of the rotary shaft are reduced.
摘要翻译：根据本发明的反应型涡轮机包括在壳体入口和转子之间接合到旋转轴的旋转轴扩大构件。作为工作流体沿与流动方向相反的方向对旋转轴施加压力的按压区域，与流动方向相反的方向的动力增加，从而能够减少施加到工作流体的流动方向的推力。因此，不需要安装用于在流动方向上支撑推力的单独的止推轴承。此外，旋转轴扩大构件分开形成为具有大于旋转轴的直径的直径并且接合到旋转轴，从而减小了用于扩大旋转轴的直径的时间和费用。

5. 发明公开

KR1020130126115A 반작용식 터빈 审中-实审
标题翻译：反应型涡轮机
公开(公告)号：KR1020130126115A
公开(公告)日：2013-11-20
申请号：KR1020120049940
申请日：2012-05-10
申请人： 주식회사 에이치케이터빈
发明人： 하용식 , 장영일 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D25/16 , F01D11/00
CPC分类号： F01D1/32 , F01D1/04 , F01D1/20 , F01D11/02 , F05D2220/30 , F05D2240/55 , F16J15/447
摘要： A reaction type turbine according to the present invention includes two first and second sealing members between a bearing and both sides of a turbine housing unit, thereby prevent a leakage of working fluid inside the turbine housing unit. Furthermore, the dilution of bearing lubricating oil and the contamination of cooling water might be generated when the bearing lubricating oil and the cooling water are mixed. Additionally, the fluid between the second sealing members is discharged to the outside via a guide unit as the present invention includes the guide unit for guiding the fluid so that the circulation of the diluted bearing lubricating oil and the contaminated cooling water is minimized.
摘要翻译：根据本发明的反应式涡轮机包括在轴承和涡轮机壳体单元的两侧之间的两个第一和第二密封构件，从而防止工作流体在涡轮机壳体单元内泄漏。此外，当轴承润滑油和冷却水混合时，可能会产生轴承润滑油的稀释和冷却水的污染。此外，第二密封构件之间的流体通过引导单元排出到外部，因为本发明包括用于引导流体的引导单元，使得稀释的轴承润滑油和受污染的冷却水的循环最小化。

6. 发明公开

KR1020130125960A 반작용식 터빈 有权
标题翻译：反应型涡轮机
公开(公告)号：KR1020130125960A
公开(公告)日：2013-11-20
申请号：KR1020120049631
申请日：2012-05-10
申请人： 주식회사 에이치케이터빈
发明人： 장영일 , 하용식 , 김정훈 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D25/24
CPC分类号： F01D1/20 , F01D1/32 , F01D1/34 , F01D5/02 , F01D11/02
摘要： The manufacture of a reaction type turbine according to the present invention into a shape desired by a designer is facilitated as first and second rotor plates of a rotor are formed to be integrated and an inner flow passage is formed by forming first and second flow passages, which are formed on facing surfaces of the first and second rotor plates, to be integrated. Furthermore, the inner flow passages, which is composed of the first and second flow passages, can be manufactured into a circular shape by manufacturing each cross section of the first and second flow passages into a semicircular shape so that the performance of the turbine is improved by minimizing a pressure loss of working fluid passing through the inner flow passage.
摘要翻译：将转子的第一和第二转子板形成为一体并且通过形成第一和第二流动通道形成内部流动通道，从而促进了根据本发明的反应型涡轮机制造成设计者期望的形状，其形成在第一和第二转子板的相对表面上，以被集成。此外，由第一和第二流动通道组成的内部流动通道可以通过将第一和第二流动通道的每个横截面制成半圆形形状来制造成圆形，使得涡轮机的性能得到改善通过最小化通过内部流动通道的工作流体的压力损失。

7. 发明公开

KR1020130125193A 반작용식 터빈 有权
标题翻译：反应型涡轮机
公开(公告)号：KR1020130125193A
公开(公告)日：2013-11-18
申请号：KR1020120048746
申请日：2012-05-08
申请人： 주식회사 에이치케이터빈
发明人： 장영일 , 정훈 , 김정훈 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D25/24
CPC分类号： F01D1/32 , F01D1/04 , F01D1/20 , F01D1/34 , F01D9/02 , F01D25/24 , F05D2220/30
摘要： As a rotor of which an inner flow passage is formed into an involute curve shape, a flow passage change of working fluid, which is guided from the center of the rotor to the outer periphery of the rotor and sprayed to a circumferential direction, is gradual so that a pressure loss caused by the flow passage change is minimized and the performance of a turbine can be increased. Furthermore, the turbine prevents a rapid flow passage change between a rotor inlet and the inner flow passage by forming at least one among the outer periphery of the rotor inlet, which sends the working fluid from the center of the rotor to an axial direction, and the outer circumference of the inner flow passages into a circle shape.
摘要翻译：作为内流道形成为渐开线曲线形状的转子，从转子的中心向转子的外周引导到周向喷射的工作流体的流路变化是逐渐的使得由流路变化引起的压力损失最小化，并且能够提高涡轮机的性能。此外，涡轮机通过在转子入口的外周中形成至少一个，转子入口和内流道之间的至少一个将工作流体从转子的中心向轴向方向传递，从而防止转子入口和内部流动通道之间的快速流动通道变化，以及内流道的外周为圆形。

8. 发明授权

KR101589260B1 반작용식 터빈 有权
标题翻译：反应型涡轮机
公开(公告)号：KR101589260B1
公开(公告)日：2016-01-28
申请号：KR1020120049631
申请日：2012-05-10
申请人： 주식회사 에이치케이터빈
发明人： 장영일 , 하용식 , 김정훈 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D25/24
CPC分类号： F01D1/20 , F01D1/32 , F01D1/34 , F01D5/02 , F01D11/02
摘要： 본발명에따른반작용식터빈은, 로터가 2개의제 1,2로터플레이트가서로결합되어일체가되고, 내부유로는상기제 1,2로터플레이트에서각각서로마주보는면에형성된제 1,2유로가합해져이루어지기때문에, 상기내부유로의단면형상에대한제약이해소되어설계자가원하는형상으로의제작이용이해질수 있다. 또한, 상기제 1,2유로의각 단면이반원형상으로제작이가능하여, 상기제 1,2유로가합해진내부유로의형상이원형이될 수있으므로, 상기내부유로를통과하는작동유체의압력손실이최소화되어터빈의성능이향상될수 있는효과가있다.

9. 发明公开

KR1020140000381A 반작용식 터빈 审中-实审
标题翻译：反应型涡轮机
公开(公告)号：KR1020140000381A
公开(公告)日：2014-01-03
申请号：KR1020120067169
申请日：2012-06-22
申请人： 주식회사 에이치케이터빈
发明人： 김정훈 , 장영일 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D25/00
CPC分类号： F01D1/32 , F01D1/04 , F01D1/20 , F01D25/24 , F05D2220/30
摘要： A reaction turbine according to the present invention can improve efficiency by raising the degree of reaction as well as reducing time and cost for production as a reaction rotor is substituted for a high-priced blade at the final stage. And the torque variance of the whole turbine can be reduced because the reaction rotor has the effect of a flywheel. Also the working fluid being sprayed from the reaction rotor is discharged backward in an inclined direction and collides with the inner rear surface of a housing to generate a reaction force in a forward direction, wherein the reaction force reduces load in an axial direction which is generated in the flowing direction of the working fluid.
摘要翻译：根据本发明的反应涡轮机可以通过提高反应程度来提高效率，并且由于反应转子在最后阶段代替高价格的叶片，因此可以缩短生产时间和成本。并且由于反应转子具有飞轮的作用，整个涡轮机的扭矩变化可以减小。另外，从反应转子喷出的工作流体向倾斜方向后退，与壳体的内后表面碰撞，产生向前方向的反作用力，其中反作用力减小轴向产生的载荷在工作流体的流动方向。

10. 发明公开

KR1020130125461A 반작용식 터빈 审中-实审
标题翻译：反应型涡轮机
公开(公告)号：KR1020130125461A
公开(公告)日：2013-11-19
申请号：KR1020120048979
申请日：2012-05-09
申请人： 주식회사 에이치케이터빈
发明人： 장영일 , 하용식 , 김철규 , 김기태
IPC分类号： F01D1/32 , F01D1/34 , F01D11/02 , F01D25/24
CPC分类号： F01D1/32 , F01D1/20 , F01D1/34 , F01D11/02 , F01D25/24 , F05D2220/30 , F05D2240/55
摘要： A reaction type turbine according to the present invention includes a labyrinth sealing portion which is axially joined to one among the outer peripheries of a separation plate and a rotor inlet and enables the inflow of steam only to the rotor inlet without a steam leakage via a gap between the outer peripheries of the separation plate and the rotor inlet, thereby improving the performance of the turbine by preventing a pressure loss caused by the steam leakage. The manufacture of the labyrinth sealing portion is facilitated by only lathe turning as the labyrinth sealing portion is formed into a ring shape so that costs for manufacturing the labyrinth sealing portion can be reduced. Furthermore, the labyrinth sealing portion is axially joined so that the assembly of the labyrinth sealing portion is facilitated. Additionally, the labyrinth sealing portion includes a plurality of toothed uneven portions which is axially formed and effectively performs a sealing function without obstructing the rotation of a rotor.
摘要翻译：根据本发明的反应型涡轮机包括迷宫式密封部分，该迷宫式密封部分轴向地连接到分离板的外周和转子入口中的一个，并且仅使蒸汽仅流到转子入口而没有通过间隙的蒸汽泄漏在分离板的外周和转子入口之间，通过防止由蒸汽泄漏引起的压力损失来提高涡轮机的性能。迷宫式密封部的制造由于迷宫式密封部形成为环状而仅通过车床转动来实现，从而能够降低制造迷宫式密封部的成本。此外，迷宫式密封部分被轴向连接，使得迷宫式密封部分的组件变得容易。此外，迷宫式密封部分包括多个齿形不平坦部分，其轴向形成并且有效地执行密封功能而不阻碍转子的旋转。

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