公开(公告)号：US07521815B2

公开(公告)日：2009-04-21

申请号：US11666052

申请日：2004-11-25

申请人： Yong Bok Lee ,  Seung-Jong Kim ,  Chang Ho Kim ,  Keun Ryu

发明人： Yong Bok Lee ,  Seung-Jong Kim ,  Chang Ho Kim ,  Keun Ryu

IPC分类号： F02C3/00

CPC分类号： H02K7/1823 ,  F01D25/22 ,  F02C3/05 ,  F05D2240/52 ,  F05D2250/82

摘要： There is provided a micro power generating device. A compressor impeller and a turbine wheel are coupled to the ends of a rotating shaft. A cooler is provided for lowering a temperature of the compressed air from the compressor impeller. The compressed air is mixed with the fuel and combusted in a combustion chamber. An air foil thrust bearing for supporting the rotating shaft has a thrust collar coupled to the rotating shaft, as well as a pair of thrust discs located apart from the thrust collar and fixed to the housing. Impeller type seals are formed at both surfaces of the thrust collar and impulse turbine blades are formed at the periphery of the thrust collar. A generator is positioned between the air foil thrust bearing and the compressor impeller. A portion of the cool air is bypassed toward the generator and the impulse turbine blades from the cooler.

摘要翻译： 提供了微型发电装置。 压缩机叶轮和涡轮机叶轮联接到旋转轴的端部。 提供了一种用于降低来自压缩机叶轮的压缩空气的温度的冷却器。 压缩空气与燃料混合并在燃烧室中燃烧。 用于支撑旋转轴的气翼止推轴承具有联接到旋转轴的止推环，以及与止推环相隔离并固定到壳体的一对推力盘。 叶片型密封件形成在推力环的两个表面处，并且冲击式涡轮叶片形成在推力套环的周边。 发电机位于气翼推力轴承和压缩机叶轮之间。 冷空气的一部分从冷却器旁路向发生器和脉冲涡轮机叶片。

公开(公告)号：US20080136190A1

公开(公告)日：2008-06-12

申请号：US11666052

申请日：2004-11-25

申请人： Yong Bok Lee ,  Seung-Jong Kim ,  Chang Ho Kim ,  Keun Ryu

发明人： Yong Bok Lee ,  Seung-Jong Kim ,  Chang Ho Kim ,  Keun Ryu

IPC分类号： F02C3/00 ,  H02K7/18

CPC分类号： H02K7/1823 ,  F01D25/22 ,  F02C3/05 ,  F05D2240/52 ,  F05D2250/82

摘要： There is provided a micro power generating device. A compressor impeller and a turbine wheel are coupled to the ends of a rotating shaft. A cooler is provided for lowering a temperature of the compressed air from the compressor impeller. The compressed air is mixed with the fuel and combusted in a combustion chamber. An air foil thrust bearing for supporting the rotating shaft has a thrust collar coupled to the rotating shaft, as well as a pair of thrust discs located apart from the thrust collar and fixed to the housing. Impeller type seals are formed at both surfaces of the thrust collar and impulse turbine blades are formed at the periphery of the thrust collar. A generator is positioned between the air foil thrust bearing and the compressor impeller. A portion of the cool air is bypassed toward the generator and the impulse turbine blades from the cooler.

摘要翻译： 提供了微型发电装置。 压缩机叶轮和涡轮机叶轮联接到旋转轴的端部。 提供了一种用于降低来自压缩机叶轮的压缩空气的温度的冷却器。 压缩空气与燃料混合并在燃烧室中燃烧。 用于支撑旋转轴的气翼止推轴承具有联接到旋转轴的止推环，以及与止推环相隔离并固定到壳体的一对推力盘。 叶片型密封件形成在推力环的两个表面处，并且冲击式涡轮叶片形成在推力套环的周边。 发电机位于气翼推力轴承和压缩机叶轮之间。 冷空气的一部分从冷却器旁路向发生器和脉冲涡轮机叶片。

公开(公告)号：US20100247010A1

公开(公告)日：2010-09-30

申请号：US12739590

申请日：2007-11-19

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Seung Jong Kim ,  Sang Hwa Lee ,  Hee Soo Kim

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Seung Jong Kim ,  Sang Hwa Lee ,  Hee Soo Kim

IPC分类号： F16C32/06 ,  H02K7/09

CPC分类号： F16C32/0444 ,  F16C17/024 ,  F16C32/0402 ,  F16C32/048

摘要： The present invention relates to an airfoil-magnetic hybrid bearing, which is a combination of a magnetic bearing and airfoil bearing. An airfoil-magnetic hybrid bearing of the present invention comprises: a housing around a rotating shaft of a rotation device; an airfoil bearing positioned between the housing and the rotating shaft for forming dynamic pressure to levitate the rotating shaft during rotation of the rotating shaft; a magnetic bearing including a plurality of cores positioned radially between inner surface of the housing and outer surface of the airfoil bearing, the cores being projected to the center of the rotating shaft, and coils wound to the cores to levitate the rotating shaft using a magnetic attractive force generated by a current application thereto; and a coupling segment for coupling the airfoil bearing to the magnetic bearing directly.

摘要翻译： 本发明涉及一种磁性轴承和翼型轴承的组合的翼型 - 磁性混合轴承。 本发明的翼型磁性混合轴承包括：围绕旋转装置的旋转轴的壳体; 位于所述壳体和所述旋转轴之间的翼型轴承，用于在所述旋转轴的旋转期间形成动态压力以悬浮所述旋转轴; 一种磁性轴承，包括径向位于壳体的内表面和翼型件的外表面之间的多个芯体，芯体突出到旋转轴的中心，线圈缠绕到芯体上以使用磁性悬浮在旋转轴上 由当前应用产生的吸引力; 以及用于将翼型轴承直接连接到磁性轴承的联接段。

公开(公告)号：US08772992B2

公开(公告)日：2014-07-08

申请号：US12739590

申请日：2007-11-19

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Seung Jong Kim ,  Sang Hwa Lee ,  Hee Soo Kim

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Seung Jong Kim ,  Sang Hwa Lee ,  Hee Soo Kim

IPC分类号： H02K7/09

CPC分类号： F16C32/0444 ,  F16C17/024 ,  F16C32/0402 ,  F16C32/048

摘要： An airfoil-magnetic hybrid bearing, which is a combination of a magnetic bearing and airfoil bearing includes a housing, an airfoil bearing, a magnetic bearing, coils, and a coupling segment. The housing is around a rotating shaft of a rotation device. The airfoil bearing is positioned between the housing and the rotating shaft to form dynamic pressure to levitate the rotating shaft during rotation of the rotating shaft. The magnetic bearing includes cores positioned radially between inner surface of the housing and outer surface of the airfoil bearing. The cores are projected to the center of the rotating shaft. The coils wound to the cores to levitate the rotating shaft using a magnetic attractive force generated by a current application thereto. The coupling segment is configured to couple the airfoil bearing to the magnetic bearing directly.

摘要翻译： 作为磁轴承和翼型轴承的组合的翼型 - 磁性混合轴承包括壳体，翼型轴承，磁性轴承，线圈和联接段。 壳体围绕旋转装置的旋转轴。 翼型轴承定位在壳体和旋转轴之间，以在旋转轴旋转期间形成动态压力以使旋转轴悬浮。 磁性轴承包括位于壳体的内表面和翼型件轴承的外表面之间径向的芯。 芯体突出到旋转轴的中心。 线圈缠绕到芯部上以使用由其施加的电流产生的磁吸引力来悬浮旋转轴。 联接段被配置为直接将翼型件轴承连接到磁性轴承。

公开(公告)号：US20080310778A1

公开(公告)日：2008-12-18

申请号：US11665410

申请日：2004-11-26

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Jun Hyeon Jo ,  Keun Ryu

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Jun Hyeon Jo ,  Keun Ryu

IPC分类号： F16C32/06

CPC分类号： F16C17/024 ,  F16C2360/24

摘要： There is provided an air foil bearing. The air foil bearing comprises a bearing house and a first foil, wherein a first end of the first foil is fixed with respect to the bearing housing and a second end of the first foil is extended along a peripheral surface of a rotating shaft while maintaining a predetermined clearance with respect to the rotating shaft to thereby become a free end. The air foil bearing also comprises a second foil fabricated from a porous metallic material and extended along the first foil between the first foil and the bearing housing.

摘要翻译： 提供了一种气翼轴承。 所述气翼轴承包括轴承座和第一箔，其中所述第一箔的第一端相对于所述轴承壳体固定，并且所述第一箔的第二端沿着旋转轴的外周表面延伸，同时保持 相对于旋转轴具有预定的间隙，从而变成自由端。 气翼轴承还包括由多孔金属材料制成并沿着第一箔片延伸在第一箔片和轴承壳体之间的第二箔片。

公开(公告)号：US20110038717A1

公开(公告)日：2011-02-17

申请号：US12988849

申请日：2008-05-19

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Dong Jin Park

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Dong Jin Park

IPC分类号： F04D29/08 ,  F04D29/58

CPC分类号： F01D25/22 ,  F02B39/14 ,  F02C6/12 ,  F05D2220/40 ,  F05D2240/52 ,  F16C17/024 ,  F16C17/042

摘要： The present invention relates to an oil-free turbocharger assembly using an airfoil bearing that may be useful in high speed conditions. The assembly can be cooled easily. A heat-proof coating can also be easily applied to the turbo charger's rotating shaft. In one embodiment, an oil-free turbocharger assembly has a constant distance between a journal portion and a rotating shaft so that the mass of the rotating body can be minimized and the rotating body assembly can have a small moment of inertia. The turbocharger in some embodiments of the invention may be cooled by a refrigerant which improves cooling efficiency. Each part of the rotating body assembly in some embodiments may be individually treated with a heat-proof process so that productivity can be improved.

摘要翻译： 本发明涉及一种使用可在高速条件下使用的翼型轴承的无油涡轮增压器组件。 组件可以轻松冷却。 耐热涂层也可以很容易地应用于涡轮增压器的旋转轴。 在一个实施例中，无油涡轮增压器组件在轴颈部分和旋转轴之间具有恒定的距离，使得旋转体的质量可以最小化并且旋转体组件可以具有小的惯性矩。 本发明的一些实施例中的涡轮增压器可以通过提高冷却效率的制冷剂来冷却。 在一些实施例中，旋转体组件的每个部分可以用耐热处理单独处理，从而可以提高生产率。

公开(公告)号：US20090008881A1

公开(公告)日：2009-01-08

申请号：US12168773

申请日：2008-07-07

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Kyoung Wook Kim

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Kyoung Wook Kim

IPC分类号： F16J15/447

CPC分类号： F16J15/4476 ,  F16J15/445

摘要： The present invention relates to a labyrinth seal used for controlling the axial leakage rate of a working fluid by using the rotating shaft of a turbo-machine such as a compressor or turbine The labyrinth seal includes: a seal disk radially extending from a rotating shaft and being formed on the rotating shaft; a seal ring spaced apart from the seal disk and being opposed to the seal disk; an actuator for moving the seal ring to adjust a gap between the seal disk and the seal ring; and a controller for controlling an operation of the actuator. By actively adjusting the gap between the seal disk and the seal ring, it is possible to effectively prevent the working fluid from leaking.

摘要翻译： 本发明涉及一种用于通过使用诸如压缩机或涡轮机的涡轮机的旋转轴来控制工作流体的轴向泄漏速率的迷宫式密封件。迷宫式密封件包括：从旋转轴径向延伸的密封盘， 形成在旋转轴上; 密封环与密封盘间隔开并与密封盘相对; 用于移动密封环以调节密封盘和密封环之间的间隙的致动器; 以及用于控制致动器的操作的控制器。 通过积极调节密封盘与密封环之间的间隙，可以有效地防止工作液泄漏。

公开(公告)号：US08070873B2

公开(公告)日：2011-12-06

申请号：US11893677

申请日：2007-08-16

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Dong Jin Park ,  Jun Hyeon Jo

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Dong Jin Park ,  Jun Hyeon Jo

IPC分类号： H01L21/316

CPC分类号： C23C4/04 ,  C23C4/02 ,  C23C4/06 ,  C23C4/18 ,  F16C17/024 ,  F16C33/14 ,  F16C33/6677 ,  F16C2204/52 ,  F16C2220/70 ,  F16C2223/06 ,  F16C2223/42 ,  Y02T10/865

摘要： Embodiments of the present invention may provide a coating material having heat resistance, abrasion resistance and low friction characteristics, which is coated on an operating component such as a rotating shaft working at a high speed without oil supply in a medium temperature environment (400° C.˜500° C.). This is so that the operating body can sufficiently withstand friction, heat generation and abrasion caused by contact with a bearing. The coating material of the present invention comprises 15 to 25 wt % antimony trioxide (Sb2O3), 50 to 70 wt % binder, 10 to 20 wt % tungsten disulphide (WS2) and 5 to 15 wt % silver (Ag). The binder comprises 60 to 80 wt % nickel (Ni) and 20 to 40 wt % chromium (Cr).

摘要翻译： 本发明的实施例可以提供具有耐热性，耐磨性和低摩擦特性的涂层材料，其涂覆在诸如在高温下工作的旋转轴等操作部件，而不在中温环境中供油（400℃ 约500℃）。 这样使得操作体能够充分地承受由于与轴承的接触而引起的摩擦，发热和磨损。 本发明的涂料包含15至25重量％的三氧化锑（Sb 2 O 3），50至70重量％的粘合剂，10至20重量％的二硫化钨（WS 2）和5至15重量％的银（Ag）。 粘合剂包含60至80重量％的镍（Ni）和20至40重量％的铬（Cr）。

公开(公告)号：US09322294B2

公开(公告)日：2016-04-26

申请号：US12988849

申请日：2008-05-19

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Dong Jin Park

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Dong Jin Park

IPC分类号： F02C6/12 ,  F01D25/22 ,  F02B39/14

CPC分类号： F01D25/22 ,  F02B39/14 ,  F02C6/12 ,  F05D2220/40 ,  F05D2240/52 ,  F16C17/024 ,  F16C17/042

摘要： The present invention relates to an oil-free turbocharger assembly using an airfoil bearing that may be useful in high speed conditions. The assembly can be cooled easily. A heat-proof coating can also be easily applied to the turbo charger's rotating shaft. In one embodiment, an oil-free turbocharger assembly has a constant distance between a journal portion and a rotating shaft so that the mass of the rotating body can be minimized and the rotating body assembly can have a small moment of inertia. The turbocharger in some embodiments of the invention may be cooled by a refrigerant which improves cooling efficiency. Each part of the rotating body assembly in some embodiments may be individually treated with a heat-proof process so that productivity can be improved.

摘要翻译： 本发明涉及一种使用可在高速条件下使用的翼型轴承的无油涡轮增压器组件。 组件可以轻松冷却。 耐热涂层也可以很容易地应用于涡轮增压器的旋转轴。 在一个实施例中，无油涡轮增压器组件在轴颈部分和旋转轴之间具有恒定的距离，使得旋转体的质量可以最小化并且旋转体组件可以具有小的惯性矩。 本发明的一些实施例中的涡轮增压器可以通过提高冷却效率的制冷剂来冷却。 在一些实施例中，旋转体组件的每个部分可以用耐热处理单独处理，从而可以提高生产率。

公开(公告)号：US07615291B2

公开(公告)日：2009-11-10

申请号：US11299119

申请日：2005-12-08

申请人： Yong Bok Lee ,  Chang Ho Kim ,  Hosung Kong ,  Hung Gu Han ,  Jeon Kook Lee ,  Jun Hyeon Jo ,  Byoung Su Lee

发明人： Yong Bok Lee ,  Chang Ho Kim ,  Hosung Kong ,  Hung Gu Han ,  Jeon Kook Lee ,  Jun Hyeon Jo ,  Byoung Su Lee

IPC分类号： B32B9/00

CPC分类号： F16C33/14 ,  C08K3/08 ,  C08K3/22 ,  C08K3/30 ,  C09D7/61 ,  C09D7/69 ,  C23C4/02 ,  C23C4/06 ,  C23C4/18 ,  C23C30/00 ,  F16C17/024 ,  F16C33/1095 ,  F16C2204/52 ,  F16C2220/70 ,  F16C2223/06 ,  F16C2223/42 ,  F16C2360/00

摘要： There is provided a coating material having heat and abrasion resistance and low friction characteristics, as well as a method of utilizing the same. The coating material comprises 20 to 40 wt % Cr2O3, 40 to 60 wt % binder, 10 to 20 wt % WS2, and 10 to 20 wt % Ag. The binder comprises 60 to 80 wt % Ni and 20 to 40 wt % Cr. The binder may further comprise above 0 to 10 wt % Al. The coating method comprises the steps of pulverizing the coating material, pulverizing a binder, applying the pulverized binder to a surface of a workpiece to form a first layer, applying the pulverized coating material to the first layer to form a second layer, and grinding and polishing the surface of the second layer.

摘要翻译： 提供了具有耐热和耐磨性和低摩擦特性的涂层材料，以及利用该涂层材料的方法。 涂层材料包含20至40重量％的Cr 2 O 3，40至60重量％的粘合剂，10至20重量％的WS 2和10至20重量％的Ag。 粘合剂包含60至80重量％的Ni和20至40重量％的Cr。 粘合剂可以进一步包含0至10重量％的Al。 涂布方法包括以下步骤：粉碎涂料，粉碎粘合剂，将粉碎的粘合剂施加到工件的表面以形成第一层，将粉碎的涂料施加到第一层以形成第二层， 抛光第二层的表面。