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1. 发明申请

US20120148391A1 CENTRIFUGAL COMPRESSOR 审中-公开
标题翻译：离心式压缩机
公开(公告)号：US20120148391A1
公开(公告)日：2012-06-14
申请号：US13380649
申请日：2010-03-17
申请人： Seiichi Ibaraki , Isao Tomita , Yasuaki Jinnai , Takashi Mikogami , Masaki Tojo , Akio Kitada
发明人： Seiichi Ibaraki , Isao Tomita , Yasuaki Jinnai , Takashi Mikogami , Masaki Tojo , Akio Kitada
IPC分类号： F01D1/02
CPC分类号： F04D29/023 , F04D29/162 , F04D29/4206 , F04D29/4213 , F04D29/441 , F04D29/685 , F05D2220/40 , F05D2250/52 , F05D2300/43 , F05D2300/502
摘要： A centrifugal compressor is equipped with a resin housing, that is made in a manner such that compression efficiency is not lost and merits such as weight and cost reduction are not cancelled out. The turbo charger housing comprises a volute section, a channel formation section, and an impeller that is fixed in the center of the channel formation section to a rotating shaft. An annular shroud is disposed in a recess formed on the inner wall of the channel formation section. The annular shroud forms the outer walls of a channel and a diffuser for compressed gas. The edge of the annular shroud spaced from a partition wall, which forms a portion of a bearing housing. If the resin housing undergoes thermal deformation, the dimensions of a gap between the annular shroud and the curved profile of a blade is maintained.
摘要翻译：离心压缩机配备有树脂壳体，其以不会损失压缩效率的方式制造，并且不能抵消诸如重量和成本降低的优点。涡轮增压器壳体包括蜗壳部分，通道形成部分和叶轮，其被固定在通道形成部分的中心到旋转轴。环形护罩设置在形成在通道形成部分的内壁上的凹部中。环形护罩形成通道的外壁和用于压缩气体的扩散器。环形护罩的边缘与形成轴承壳体的一部分的分隔壁间隔开。如果树脂壳体发生热变形，则保持环形护罩与叶片的弯曲轮廓之间的间隙的尺寸。

2. 发明申请

US20120121400A1 COMPRESSOR OF EXHAUST GAS TURBOCHARGER 有权
标题翻译：排气机压缩机
公开(公告)号：US20120121400A1
公开(公告)日：2012-05-17
申请号：US13383951
申请日：2010-08-10
申请人： Isao Tomita , Seiichi Ibaraki , Yasuaki Jinnai , Masaki Tojo
发明人： Isao Tomita , Seiichi Ibaraki , Yasuaki Jinnai , Masaki Tojo
IPC分类号： F04D29/42
CPC分类号： F04D29/4213 , F04D27/023 , F04D27/0238 , F04D29/624 , F04D29/681 , F04D29/682 , F04D29/684 , F04D29/685 , F05D2220/40 , Y10S415/914
摘要： A compressor of an exhaust gas turbocharger has an inlet slit, an outlet slit and the recirculation passage can formed at the same time when the compressor housing assembled. Ease of assembly and the reduction of the production cost is achieved. The structure of the inlet slit, the outlet slit and the recirculation passage can be compact and can be easily adjusted. Noises generated in the compressor impeller can be reduced without providing a noise insulation cover.
摘要翻译：排气涡轮增压器的压缩机具有入口狭缝，出口狭缝，并且在压缩机壳体组装的同时形成再循环通道。实现了组装的轻松和生产成本的降低。入口狭缝，出口狭缝和再循环通道的结构可以是紧凑的并且可以容易地调节。压缩机叶轮产生的噪音可以减小而不提供隔音罩。

3. 发明授权

US08888440B2 Compressor of exhaust gas turbocharger 有权
标题翻译：废气涡轮增压器压缩机
公开(公告)号：US08888440B2
公开(公告)日：2014-11-18
申请号：US13383951
申请日：2010-08-10
申请人： Isao Tomita , Seiichi Ibaraki , Yasuaki Jinnai , Masaki Tojo
发明人： Isao Tomita , Seiichi Ibaraki , Yasuaki Jinnai , Masaki Tojo
IPC分类号： F04D29/66 , F04D29/42 , F04D29/68 , F04D27/02
CPC分类号： F04D29/4213 , F04D27/023 , F04D27/0238 , F04D29/624 , F04D29/681 , F04D29/682 , F04D29/684 , F04D29/685 , F05D2220/40 , Y10S415/914
摘要： A compressor of an exhaust gas turbocharger has a compressor housing of a divided type that forms an inlet slit, an outlet slit and a recirculation passage at the same time when the compressor housing is assembled. In the compressor of the exhaust gas turbocharger, mating surfaces of compressor housing members 9a and 9b are formed in the neighborhood of the inlet part of the impeller 5 in the compressor housing 9 that is divided into the compressor housing members 9a and 9b in the direction of the rotation axis of the impeller; and, a space forming the recirculation passage 29, an inlet slit 25 and an outlet slit 27 are formed between the mating compressor housing members 9a and 9b.
摘要翻译：排气涡轮增压器的压缩机具有分体式的压缩机壳体，其在组装压缩机壳体的同时形成入口狭缝，出口狭缝和再循环通道。在排气涡轮增压器的压缩机中，压缩机壳体部件9a和9b的配合面形成在压缩机壳体9的叶轮5的入口部附近，压缩机壳体部件9a和9b沿方向的叶轮的旋转轴线; 并且在配合压缩机壳体部件9a和9b之间形成形成再循环通道29的空间，入口狭缝25和出口狭缝27。

4. 发明授权

US08251650B2 Compressor housing 有权
标题翻译：压缩机外壳
公开(公告)号：US08251650B2
公开(公告)日：2012-08-28
申请号：US12360522
申请日：2009-01-27
申请人： Seiichi Ibaraki , Yasuaki Jinnai , Masaki Tojo
发明人： Seiichi Ibaraki , Yasuaki Jinnai , Masaki Tojo
IPC分类号： F04D29/42
CPC分类号： F04D29/023 , F04D29/4206 , F05D2300/43
摘要： The present invention provides a compressor housing capable of reducing the weight of a compressor without leading to an increase in the size and a reduction in the efficiency of the compressor. The compressor housing includes: an inner cylinder made of a plastic material and extending in an axial direction and in a circumferential direction to surround blade tips of the blades; and an outer cylinder made of a plastic material and extending in the axial direction and in the circumferential direction to surround the inner cylinder. The inner cylinder and the outer cylinder are bonded or jointed at the first end, opposite the second end where the volute is formed.
摘要翻译：本发明提供一种压缩机壳体，其能够减小压缩机的重量，而不会导致压缩机的尺寸增加和效率降低。压缩机壳体包括：由塑料材料制成并沿轴向方向和沿圆周方向延伸以围绕叶片的叶片尖端的内筒; 以及由塑料材料制成并在轴向和周向上延伸以围绕内筒的外筒。内筒和外筒在形成蜗壳的第二端的第一端处接合或接合。

5. 发明授权

US08147186B2 Centrifugal compressor 有权
标题翻译：离心式压缩机
公开(公告)号：US08147186B2
公开(公告)日：2012-04-03
申请号：US12308246
申请日：2008-04-10
申请人： Seiichi Ibaraki , Isao Tomita , Yasuaki Jinnai , Takashi Shiraishi , Koichi Sugimoto
发明人： Seiichi Ibaraki , Isao Tomita , Yasuaki Jinnai , Takashi Shiraishi , Koichi Sugimoto
IPC分类号： F01D9/04
CPC分类号： F04D29/4206 , F04D29/422 , F04D29/441 , F04D29/462 , F04D29/464 , F05D2250/52
摘要： A centrifugal compressor having a wide operating range, being economically efficient and high reliability in terms of a stable operation is provided. A centrifugal compressor including a partition wall for dividing a flow channel in the diffuser section and the volute section into a plurality of channels in the direction of circulation of the fluid so as to define a hub-side flow channel and a shroud-side flow channel; and a flow rate adjusting valve for lowering the flow rate of the fluid flowing in the shroud-side flow channel to increase the flow rate in the hub-side flow channel when the flow rate of the fluid compressed by an impeller is low and not lowering the flow rate of the fluid flowing the shroud-side flow channel to allow the fluid to flow both in the shroud-side flow channel and the hub-side flow channel when the flow rate of the fluid compressed by the impeller is high is employed.
摘要翻译：提供了一种操作范围广，离心压缩机经济高效，稳定操作的高可靠性。一种离心压缩机，包括用于将扩散器部分中的流动通道和所述涡旋部分分隔成流体的流动方向上的多个通道的分隔壁，以便限定毂侧流动通道和护罩侧流动通道 ; 以及流量调节阀，用于降低在所述护罩侧流路中流动的流体的流量，以在由叶轮压缩的流体的流量低且不降低时增加所述毂侧流路中的流量采用流体流动侧流动通道的流体，以便当由叶轮压缩的流体的流量高时，流体在护罩侧流路和毂侧流路中流动。

6. 发明申请

US20100166539A1 Centrifugal compressor 有权
标题翻译：离心式压缩机
公开(公告)号：US20100166539A1
公开(公告)日：2010-07-01
申请号：US12308246
申请日：2008-04-10
申请人： Seiichi Ibaraki , Isao Tomita , Yasuaki Jinnai , Takashi Shiraishi , Koichi Sugimoto
发明人： Seiichi Ibaraki , Isao Tomita , Yasuaki Jinnai , Takashi Shiraishi , Koichi Sugimoto
IPC分类号： F04D29/46
CPC分类号： F04D29/4206 , F04D29/422 , F04D29/441 , F04D29/462 , F04D29/464 , F05D2250/52
摘要： A centrifugal compressor having a wide operating range, being economically efficient and high reliability in terms of a stable operation is provided. A centrifugal compressor including a partition wall 37 for dividing a flow channel in the diffuser section 15 and the volute section 16 into a plurality of channels in the direction of circulation of the fluid so as to define a hub-side flow channel A and a shroud-side flow channel B; and a flow rate adjusting valve 36 for lowering the flow rate of the fluid flowing in the shroud-side flow channel B to increase the flow rate in the hub-side flow channel A when the flow rate of the fluid compressed by an impeller 13 is low and not lowering the flow rate of the fluid flowing the shroud-side flow channel B to allow the fluid to flow both in the shroud-side flow channel B and the hub-side flow channel A when the flow rate of the fluid compressed by the impeller 13 is high is employed.
摘要翻译：提供了一种操作范围广，离心压缩机经济高效，稳定操作的高可靠性。一种离心式压缩机，包括分隔壁37，用于将扩散器部分15中的流动通道和蜗壳部分16沿流体的循环方向分成多个通道，以限定轮毂侧流动通道A和护罩侧流道B; 以及流量调节阀36，用于降低在侧翼流路B中流动的流体的流量，从而当由叶轮13压缩的流体的流量为流量时增加毂侧流路A的流量并且不会降低流过护罩侧流路B的流体的流量，以允许流体在护罩侧流路B和毂侧流路A中流动，当流体被压缩的流体流速叶轮13高。

7. 发明申请

US20090151348A1 Exhaust Turbo Supercharger 有权
标题翻译：排气涡轮增压器
公开(公告)号：US20090151348A1
公开(公告)日：2009-06-18
申请号：US11989306
申请日：2007-02-09
申请人： Noriyuki Hayashi , Yasuaki Jinnai , Seiichi Ibaraki , Fumiharu Takahashi , Yoh Akiyama
发明人： Noriyuki Hayashi , Yasuaki Jinnai , Seiichi Ibaraki , Fumiharu Takahashi , Yoh Akiyama
IPC分类号： F02B33/44
CPC分类号： F02C6/12 , F01D25/16 , F01D25/24 , F02B39/00 , F02C7/24 , F05B2260/301 , F05D2220/40 , F05D2300/502
摘要： An exhaust turbo supercharger is provided that is able to effectively prevent exhaust gas that has flowed into between a turbine housing and a bearing housing from leaking to outside of the device, while allowing an excellent level of workability in assembly and disassembly. Included is a turbine housing, into which exhaust gas from an internal combustion engine is introduced; a turbine wheel which is provided within the turbine housing and which is rotation-driven by the exhaust gas; a turbine shaft, one end of which is inserted into the turbine housing, and to which the turbine wheel is attached; a bearing which supports the turbine shaft; and a bearing housing which is connected to the turbine housing and inside of which the bearing is housed. A bolt insert hole is formed in the turbine housing, and an internal thread insert made from a heat insulating material is provided in the bolt insert hole, and the turbine housing and the bearing housing are fixed by a bolt that engages with the internal thread insert.
摘要翻译：提供一种排气涡轮增压器，其能够有效地防止已经流入涡轮壳体和轴承壳体之间的废气泄漏到装置外部，同时允许在组装和拆卸中具有优异的可加工性水平。包括引入来自内燃机的废气的涡轮机壳体; 涡轮机轮，其设置在所述涡轮机壳体内并且由所述排气旋转驱动; 一个涡轮轴，其一端插入涡轮机壳体中，涡轮机叶轮安装在该涡轮轴上; 支撑涡轮轴的轴承; 以及连接到所述涡轮机壳体并且其内部容纳所述轴承的轴承壳体。螺栓插入孔形成在涡轮机壳体中，并且由绝热材料制成的内螺纹插入件设置在螺栓插入孔中，并且涡轮壳体和轴承壳体通过与内螺纹插入件接合的螺栓固定。

8. 发明授权

US07797936B2 Exhaust turbo supercharger 有权
标题翻译：排气涡轮增压器
公开(公告)号：US07797936B2
公开(公告)日：2010-09-21
申请号：US11989306
申请日：2007-02-09
申请人： Noriyuki Hayashi , Yasuaki Jinnai , Seiichi Ibaraki , Fumiharu Takahashi , Yoh Akiyama
发明人： Noriyuki Hayashi , Yasuaki Jinnai , Seiichi Ibaraki , Fumiharu Takahashi , Yoh Akiyama
IPC分类号： F02D23/00 , F02B39/00 , F01D25/24 , F16B35/04 , F16B39/04
CPC分类号： F02C6/12 , F01D25/16 , F01D25/24 , F02B39/00 , F02C7/24 , F05B2260/301 , F05D2220/40 , F05D2300/502
摘要： An exhaust turbo supercharger is provided that is able to effectively prevent exhaust gas that has flowed into between a turbine housing and a bearing housing from leaking to outside of the device, while allowing an excellent level of workability in assembly and disassembly. Included is a turbine housing, into which exhaust gas from an internal combustion engine is introduced; a turbine wheel which is provided within the turbine housing and which is rotation-driven by the exhaust gas; a turbine shaft, one end of which is inserted into the turbine housing, and to which the turbine wheel is attached; a bearing which supports the turbine shaft; and a bearing housing which is connected to the turbine housing and inside of which the bearing is housed. A bolt insert hole is formed in the turbine housing, and an internal thread insert made from a heat insulating material is provided in the bolt insert hole, and the turbine housing and the bearing housing are fixed by a bolt that engages with the internal thread insert.
摘要翻译：提供一种排气涡轮增压器，其能够有效地防止已经流入涡轮壳体和轴承壳体之间的废气泄漏到装置外部，同时允许在组装和拆卸中具有优异的可加工性水平。包括引入来自内燃机的废气的涡轮机壳体; 涡轮机轮，其设置在所述涡轮机壳体内并且由所述排气旋转驱动; 一个涡轮轴，其一端插入涡轮机壳体中，涡轮机叶轮安装在该涡轮轴上; 支撑涡轮轴的轴承; 以及连接到所述涡轮机壳体并且其内部容纳所述轴承的轴承壳体。螺栓插入孔形成在涡轮机壳体中，并且由绝热材料制成的内螺纹插入件设置在螺栓插入孔中，并且涡轮壳体和轴承壳体通过与内螺纹插入件接合的螺栓固定。

9. 发明申请

US20060188368A1 Structure of scroll of variable-throat exhaust turbocharger and method for manufacturing the turbocharger 有权
标题翻译：可变喉排气涡轮增压器的涡旋结构和制造涡轮增压器的方法
公开(公告)号：US20060188368A1
公开(公告)日：2006-08-24
申请号：US11349111
申请日：2006-02-08
申请人： Yasuaki Jinnai , Hiroshi Nakagawa , Takashi Mikogami
发明人： Yasuaki Jinnai , Hiroshi Nakagawa , Takashi Mikogami
IPC分类号： F01D9/00
CPC分类号： F02C6/12 , F01D17/165 , F05D2220/40
摘要： According to the present invention, the A/R, the ratio of cross sectional area A of scroll passage to scroll radius R can be increased without increasing the size of the turbine casing and with very simple construction and exhaust turbine capacity can be increased, so a variable-throat exhaust turbocharger with which engine output can be increased is provided. The turbocharger is equipped with a nozzle throat area varying mechanism of which the nozzle assembly unit is composed such that a plurality of nozzle vanes are supported rotatably by an annular nozzle mount and an annular nozzle plate is connected to the nozzle mount by means of a plurality of nozzle supports to sandwich the nozzle vanes, the nozzle plate is located in the scroll chamber by attaching the nozzle assembly unit to the turbine casing to allow the nozzle plate to form part of the inside sidewall face of the scroll chamber and a wall face of the annular flow passage.
摘要翻译：根据本发明，可以在不增加涡轮机壳体的尺寸的情况下增加涡旋通道的横截面积A与涡旋半径R的比率，并且以非常简单的结构和排气涡轮机容量可以增加，因此提供可增加发动机输出的可变喉排气涡轮增压器。涡轮增压器配备有喷嘴喉部区域变化机构，其喷嘴组件单元组成，使得多个喷嘴叶片由环形喷嘴座可旋转地支撑，并且环形喷嘴板通过多个连接到喷嘴座上的喷嘴支撑件夹住喷嘴叶片，喷嘴板通过将喷嘴组件单元附接到涡轮机壳体而位于涡旋室中，以允许喷嘴板形成涡旋室的内侧壁面的一部分，环形流路。

10. 发明授权

US06669442B2 Method and device for assembling and adjusting variable capacity turbine 有权
标题翻译：组装和调整变量涡轮机的方法和装置
公开(公告)号：US06669442B2
公开(公告)日：2003-12-30
申请号：US10086450
申请日：2002-03-04
申请人： Yasuaki Jinnai , Takashi Mikogami , Koji Matsumoto
发明人： Yasuaki Jinnai , Takashi Mikogami , Koji Matsumoto
IPC分类号： F01D1716
CPC分类号： F01D17/165 , F05D2220/40 , F05D2230/64 , Y10T29/4932
摘要： The invention provides a method and device of assembling and adjusting a variable capacity turbine, which simplifies assembling process resulting in reduction of man-hours and costs of assembling and adjustment, and makes it possible that the nozzle vane setting of the adjustable nozzle mechanism is done with high accuracy without influenced by the accuracy in dimensions of the constituent parts such as nozzle vane and annular link mechanism and that the adjustable nozzle vane mechanism is adjusted whenever necessary even after the turbine is assembled. The invention is characterized in that a plurality of nozzle vanes are temporarily encircled and bound with a binding member capable of binding/releasing such as belt, etc. in a state the vanes are perfectly closed with the vanes contacting to each other, then the nozzle pin fixed to each of the nozzle vanes and supported free of rotation in the nozzle mount is fixed by staking or the like to the lever plate constituting the connection part of the annular link mechanism with the vanes in the temporarily bound state.
摘要翻译：本发明提供一种组装和调节可变容量涡轮机的方法和装置，其简化了组装过程，从而减少了工时和组装和调节的成本，并且使得可调节喷嘴机构的喷嘴叶片设定成为可能高精度，不受喷嘴叶片和环形连杆机构等构成部件的尺寸精度的影响，并且即使在涡轮组装后也可以调节可调喷嘴叶片机构。本发明的特征在于，多个喷嘴叶片在叶片彼此接触的状态下被暂时环绕并且能够与叶片完全闭合的状态下与能够粘合/释放的捆扎件结合在一起，然后喷嘴销固定到每个喷嘴叶片并被支撑在喷嘴座中没有旋转，通过铆钉等固定到构成连接点p的杆板上环形连杆机构的技术，其中叶片处于暂时束缚状态。

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