CN107701298A - Compressor and booster - Google Patents
Compressor and booster Download PDFInfo
- Publication number
- CN107701298A CN107701298A CN201710818678.4A CN201710818678A CN107701298A CN 107701298 A CN107701298 A CN 107701298A CN 201710818678 A CN201710818678 A CN 201710818678A CN 107701298 A CN107701298 A CN 107701298A
- Authority
- CN
- China
- Prior art keywords
- frame
- impeller
- vortex chamber
- bearing frame
- bolt
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/16—Other safety measures for, or other control of, pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/422—Discharge tongues
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
- F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/52—Outlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/39—Retaining components in desired mutual position by a V-shaped ring to join the flanges of two cylindrical sections, e.g. casing sections of a turbocharger
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Abstract
本发明以提供一种压缩机及增压器为目的,能够有效抑制紧固与涡旋室框架相邻的框架和涡旋室框架的螺栓的断裂,使这些框架稳定地结合,压缩机(10)具备:叶轮(14),该叶轮(14)用于压缩空气;空气引导筒(16),该空气引导筒(16)用于收容叶轮(14)且引导空气;涡旋室框架(20),该涡旋室框架(20)设置成与空气引导筒(16)相邻,形成用于将通过空气引导筒的空气向外部引导的涡旋室(18);框架(22,40),该框架(22,40)设置成与涡旋室框架(20)相邻;螺栓(25,48),该螺栓(25,48)紧固涡旋室框架(20)与框架(22,40);以及衬套(28),该衬套(28)设置于螺栓(25,48)的头部(26,52)与涡旋室框架(20)之间。
The purpose of the present invention is to provide a compressor and a supercharger, which can effectively suppress the fracture of the bolts fastening the frame adjacent to the scroll chamber frame and the scroll chamber frame, so that these frames can be stably combined, and the compressor (10 ) has: an impeller (14), the impeller (14) is used to compress air; an air guide cylinder (16), the air guide cylinder (16) is used to accommodate the impeller (14) and guide air; the vortex chamber frame (20) , the vortex chamber frame (20) is arranged adjacent to the air guide cylinder (16), forming a vortex chamber (18) for guiding the air passing through the air guide cylinder to the outside; the frame (22, 40), the The frame (22, 40) is arranged adjacent to the vortex chamber frame (20); bolts (25, 48), the bolts (25, 48) fasten the vortex chamber frame (20) and the frame (22, 40); And a bush (28) disposed between the head (26, 52) of the bolt (25, 48) and the scroll chamber frame (20).
Description
本申请为下述申请的分案申请:This application is a divisional application of the following application:
原申请的申请日:2014年06月30日Filing date of the original application: June 30, 2014
原申请的申请号:201480041368.0Application number of the original application: 201480041368.0
原申请的发明名称:压缩机及增压器Invention title of the original application: compressor and supercharger
技术领域technical field
本发明涉及用于内燃机的压缩机及增压器。The invention relates to compressors and superchargers for internal combustion engines.
背景技术Background technique
以往,作为用于压缩供给至内燃机的空气的增压器,使用一种包含如下压缩机的增压器,该压缩机包含:叶轮,该叶轮用于压缩空气;空气引导筒,该空气引导筒用于收容叶轮并引导空气;以及涡旋室框架,该涡旋室框架与空气引导筒相邻而设置,形成用于将通过空气引导筒的空气向外部引导的涡旋室。Conventionally, as a supercharger for compressing air supplied to an internal combustion engine, a supercharger including a compressor including: an impeller for compressing air; an air guide cylinder for accommodating the impeller and guiding air; and a swirl chamber frame which is provided adjacent to the air guide cylinder and forms a swirl chamber for guiding the air passing through the air guide cylinder to the outside.
在专利文献1所述增压器中,在叶轮的一部分爆裂而向外飞散时,为了不使用于润滑径向滑动轴承的润滑油的压力罐破损而发生油泄漏,在压缩器的扩散室与压力罐之间设置有冲击吸收隔壁。In the turbocharger described in Patent Document 1, when a part of the impeller bursts and is scattered outward, in order to prevent oil leakage from being damaged in the pressure tank for lubricating the lubricating oil for lubricating the radial sliding bearing, the diffusion chamber of the compressor and the Shock-absorbing partitions are provided between the pressure tanks.
现有技术文献prior art literature
专利文献patent documents
专利文献1:日本特开2001-132465号公报Patent Document 1: Japanese Patent Laid-Open No. 2001-132465
然而,在构成增压器的一部分的压缩机中,叶轮断裂的话,有叶轮碎片向叶轮的半径方向外侧飞散,与空气引导筒、其周围的框架等碰撞的可能性。叶轮碎片与空气引导筒、其周围的框架等碰撞的话,有在用于紧固相邻于空气引导筒的涡旋室框架与相邻于涡旋室框架的框架的螺栓产生拉伸应力,该螺栓断裂的可能性。However, if the impeller of the compressor constituting a part of the supercharger is broken, the impeller fragments may scatter outward in the radial direction of the impeller and may collide with the air guide tube, the frame around it, and the like. If the impeller fragments collide with the air guide cylinder, its surrounding frame, etc., there will be tensile stress on the bolts for fastening the frame of the scroll chamber adjacent to the air guide cylinder and the frame adjacent to the scroll chamber frame, and the Possibility of bolt breakage.
关于这点,虽然在专利文献1中记载了如上所述在叶轮的一部分飞散时,不使润滑油压力罐破损的结构,但没有公开任何关于由于叶轮的飞散而导致上述螺栓断裂的问题及其解决方案。Regarding this point, although Patent Document 1 describes a structure that does not damage the lubricating oil pressure tank when a part of the impeller is scattered as described above, it does not disclose any problems related to the breakage of the above-mentioned bolts due to the scattering of the impeller and its solution.
发明内容Contents of the invention
本发明的几个实施方式的目的在于提供一种压缩机及增压器,能够有效抑制紧固相邻于涡旋室框架的框架和涡旋室框架的螺栓的断裂,实现这些框架的稳定的结合状态。The purpose of several embodiments of the present invention is to provide a compressor and a supercharger, which can effectively suppress the fracture of the bolts fastening the frame adjacent to the scroll chamber frame and the scroll chamber frame, and realize the stability of these frames. combined state.
用于解决课题的手段means to solve the problem
本发明的几个实施方式的压缩机,Compressors according to several embodiments of the present invention,
(1)具备:叶轮,该叶轮用于压缩空气;(1) Equipped with: an impeller, which is used for compressing air;
空气引导筒,该空气引导筒用于收容所述叶轮并引导所述空气;an air guiding cylinder for housing the impeller and guiding the air;
涡旋室框架,该涡旋室框架设置成与所述空气引导筒相邻且形成涡旋室,该涡旋室用于将通过所述空气引导筒的空气向外部引导;a swirl chamber frame disposed adjacent to the air guide cylinder and forming a swirl chamber for guiding air passing through the air guide cylinder to the outside;
第1框架,该第1框架设置成与所述涡旋室框架相邻;a first frame, the first frame is arranged adjacent to the vortex chamber frame;
第1螺栓,该第1螺栓紧固所述涡旋室框架与所述第1框架;以及a first bolt fastening the scroll chamber frame and the first frame; and
衬套,该衬套设置于所述第1螺栓的头部与所述涡旋室框架之间。A bush, the bush is arranged between the head of the first bolt and the frame of the scroll chamber.
压缩机中若叶轮断裂的话,有叶轮碎片向叶轮的半径方向外侧飞散,与空气引导筒、其周围的框架等碰撞的可能性。叶轮碎片与空气引导筒、其周围的框架等碰撞的话,有在用于紧固相邻于空气引导筒的涡旋室框架与相邻于涡旋室框架的第1框架的第1螺栓产生拉伸应力,第1螺栓断裂的可能性。If the impeller is broken in the compressor, the impeller fragments may scatter outward in the radial direction of the impeller and may collide with the air guide tube, the frame around it, and the like. If the impeller debris collides with the air guide cylinder and its surrounding frame, tension will be generated on the first bolts for fastening the scroll chamber frame adjacent to the air guide cylinder and the first frame adjacent to the scroll chamber frame. Tensile stress, the possibility of breaking the first bolt.
对此,根据上述(1)所述的压缩机,由于在第1螺栓的头部与涡旋室框架之间设置有衬套,因此与不设置衬套的情况相比,能够使用轴部的长度(颈部的长度)较长的第1螺栓来紧固涡旋室框架与第1框架。因此,与不设置衬套的情况相比,能够在对第1螺栓施加了轴向的拉伸负荷时不使第1螺栓断裂而使能够伸长的伸长量变大。由此,即使在紧固涡旋室框架与第1框架的第1螺栓产生如上所述的因叶轮的断裂而导致的拉伸应力,也能够有效抑制第1螺栓的断裂。即,能够实现涡旋室框架与第1框架的稳定的结合状态。In contrast, according to the compressor described in (1) above, since a bush is provided between the head portion of the first bolt and the scroll chamber frame, compared with the case where no bush is provided, it is possible to use the Fasten the scroll chamber frame and the first frame with the first bolt with a long length (the length of the neck). Therefore, when a tensile load in the axial direction is applied to the first bolt, the amount of elongation that can be extended can be increased without breaking the first bolt, compared to the case where the bush is not provided. Thereby, even if the above-mentioned tensile stress due to fracture of the impeller occurs in the first bolts fastening the scroll chamber frame and the first frame, the fracture of the first bolts can be effectively suppressed. That is, a stable coupling state between the scroll chamber frame and the first frame can be realized.
另外,为了制造上述(1)所述的压缩机,无须重新采购所有的结构,对已有的压缩机进行衬套的追加与第1螺栓的交换即可。即,上述(1)所述的压缩机还有生产容易性的观点上的优势。In addition, in order to manufacture the compressor described in (1) above, it is not necessary to repurchase all the structures, and it is only necessary to add the bushing and replace the first bolts to the existing compressor. That is, the compressor described in (1) above is also advantageous in terms of ease of production.
另外,(1)所述的压缩机中的“第1框架”至少包含用于实施发明的方式所述的消音器框架与轴承框架的意思。另外,在上述(1)所述的压缩机中,在第1螺栓为双头螺栓的情况下,第1螺栓的头部是指双头螺栓所用的螺帽。In addition, the "first frame" in the compressor described in (1) includes at least the muffler frame and the bearing frame described in the embodiment of the invention. Moreover, in the compressor as described in said (1), when a 1st bolt is a stud bolt, the head part of a 1st bolt means the nut used for a stud bolt.
在几个实施方式中,在上述(1)所述的压缩机中,In several embodiments, in the compressor described in (1) above,
(2)所述衬套形成为套筒状且以包围所述第1螺栓的轴部的方式设置,(2) The bush is formed in a sleeve shape and provided so as to surround the shaft portion of the first bolt,
所述衬套的内径比所述第1螺栓的头部的直径小。The inner diameter of the bush is smaller than the diameter of the head of the first bolt.
根据上述(2)所述的压缩机,通过以包围第1螺栓的轴部的方式设置的套筒状的衬套而能够均匀地支承第1螺栓的头部,因此即使在第1螺栓产生如上所述的因叶轮的断裂而导致的拉伸应力,也能够有效抑制第1螺栓的断裂。因此,能够实现涡旋室框架与相邻于涡旋室的第1框架的稳定的结合状态。According to the compressor described in (2) above, the head of the first bolt can be evenly supported by the sleeve-shaped bush provided so as to surround the shaft portion of the first bolt. The tensile stress caused by the fracture of the impeller can also effectively suppress the fracture of the first bolt. Therefore, a stable coupling state between the swirl chamber frame and the first frame adjacent to the swirl chamber can be realized.
在几个实施方式中,在上述(1)或(2)所述的压缩机中,In several embodiments, in the compressor described in (1) or (2) above,
(3)所述第1螺栓的轴向上的所述衬套的尺寸比所述第1螺栓的径向上的所述衬套的尺寸大。(3) A dimension of the bush in the axial direction of the first bolt is larger than a dimension of the bush in the radial direction of the first bolt.
如上述(3)所述的压缩机那样,通过使用适合使第1螺栓的轴部的长度变长的衬套,从而能够在对第1螺栓施加了轴向的拉伸负荷时不使第1螺栓断裂而容易地使能够伸长的伸长量变大。As in the compressor described in (3) above, by using a bush suitable for increasing the length of the shaft portion of the first bolt, it is possible to prevent the first bolt from being distorted when an axial tensile load is applied to the first bolt. When the bolt breaks, the amount of elongation that can be elongated is easily increased.
由此,即使在紧固涡旋室框架与第1框架的第1螺栓产生如上所述的因叶轮的断裂而导致的拉伸应力,也能够有效抑制第1螺栓的断裂。因此,能够实现涡旋室框架与相邻于涡旋室框架的第1框架的稳定的结合状态。Thereby, even if the above-mentioned tensile stress due to fracture of the impeller occurs in the first bolts fastening the scroll chamber frame and the first frame, the fracture of the first bolts can be effectively suppressed. Therefore, a stable coupling state between the swirl chamber frame and the first frame adjacent to the swirl chamber frame can be realized.
在几个实施方式中,在上述(1)~(3)中任一项所述的压缩机中,In several embodiments, in the compressor described in any one of the above (1) to (3),
(4)进一步具备:消音器,该消音器用于降低所述压缩机所产生的声音,(4) further comprising: a muffler for reducing the sound generated by the compressor,
所述第1框架是所述消音器的框架。The first frame is a frame of the muffler.
根据上述(4)所述的压缩机,即使在紧固消音器的框架与涡旋室框架的第1螺栓产生如上所述的因叶轮的断裂而导致的拉伸应力,也能够有效抑制第1螺栓的断裂。因此,能够有效抑制消音器从压缩机脱落。According to the compressor described in (4) above, even if the above-mentioned tensile stress caused by fracture of the impeller occurs in the first bolts fastening the frame of the muffler and the frame of the scroll chamber, the first bolt can be effectively suppressed. Breakage of bolts. Therefore, it is possible to effectively suppress the detachment of the muffler from the compressor.
在几个实施方式中,在上述(1)~(4)中任一项所述的压缩机中,In several embodiments, in the compressor described in any one of the above (1) to (4),
(5)具备:第2框架,该第2框架配置成与所述涡旋室框架相邻;(5) equipped with: a second frame, the second frame is disposed adjacent to the vortex chamber frame;
第2螺栓,该第2螺栓紧固所述涡旋室框架与所述第2框架;以及a second bolt fastening the scroll chamber frame and the second frame; and
夹具,该夹具构成为对所述涡旋室框架与所述第2框架进行夹持。A clamp configured to clamp the scroll chamber frame and the second frame.
压缩机中若叶轮断裂的话,有叶轮碎片向叶轮的半径方向外侧飞散,与空气引导筒、涡旋室框架等碰撞的情况。叶轮碎片与空气引导筒、涡旋室框架等碰撞的话,有在用于紧固相邻于涡旋室框架而配置的第2框架和涡旋室框架的第2螺栓产生拉伸应力,第2螺栓断裂的可能性。If the impeller breaks in the compressor, the impeller fragments may fly outward in the radial direction of the impeller and collide with the air guide tube, the scroll chamber frame, and the like. If the impeller fragments collide with the air guide cylinder, the swirl chamber frame, etc., tensile stress will be generated on the second bolts for fastening the second frame and the swirl chamber frame arranged adjacent to the swirl chamber frame, and the second Possibility of bolt breakage.
对此,根据上述(5)所述的压缩机,通过构成为对涡旋室框架与第2框架进行夹持的夹具,能够抑制在第2螺栓产生拉伸应力,有效抑制第2螺栓的断裂。因此,能够实现涡旋室框架与相邻于涡旋室框架的第2框架的稳定的结合状态。On the other hand, according to the compressor described in (5) above, by the clamp configured to sandwich the scroll chamber frame and the second frame, it is possible to suppress the generation of tensile stress on the second bolt and effectively suppress the breakage of the second bolt. . Therefore, a stable coupling state between the swirl chamber frame and the second frame adjacent to the swirl chamber frame can be realized.
另外,上述(5)所述的压缩机中的“第2框架”至少包含用于实施发明的方式所述的消音器框架与轴承框架的意思。In addition, the "second frame" in the compressor described in the above (5) includes at least the muffler frame and the bearing frame described in the embodiment of the invention.
在几个实施方式中,在上述(5)所述的压缩机中,In several embodiments, in the compressor described in (5) above,
(6)所述第2框架是设置有轴承部的轴承框架,所述轴承部轴支承所述叶轮的旋转轴。(6) The second frame is a bearing frame provided with a bearing portion that pivotally supports the rotating shaft of the impeller.
根据上述(6)所述的压缩机,即使在紧固涡旋室框架与轴承框架的第2螺栓产生如上述的因叶轮的断裂而导致的拉伸应力,也能够有效抑制第2螺栓的断裂。因此,能够实现涡旋室框架与轴承框架的稳定的结合状态。According to the compressor described in (6) above, even if the tensile stress caused by the breakage of the impeller as described above occurs in the second bolts fastening the scroll chamber frame and the bearing frame, the breakage of the second bolts can be effectively suppressed. . Therefore, a stable coupling state of the scroll chamber frame and the bearing frame can be realized.
在几个实施方式中,在上述(6)所述的压缩机中,In several embodiments, in the compressor described in (6) above,
(7)所述涡旋室框架具备:(7) The frame of the vortex chamber has:
涡旋室形成部,该涡旋室形成部形成所述涡旋室;以及a swirl chamber forming portion forming the swirl chamber; and
凸缘部,该凸缘部为了使所述涡旋室框架与所述轴承框架结合而从所述涡旋室形成部向所述叶轮的半径方向外侧延伸设置,a flange portion extending radially outward of the impeller from the swirl chamber forming portion for coupling the swirl chamber frame to the bearing frame,
所述第2螺栓紧固所述凸缘部与所述轴承框架,the second bolt fastens the flange portion and the bearing frame,
所述夹具构成为对所述凸缘部与所述轴承框架进行夹持。The clamp is configured to clamp the flange portion and the bearing frame.
在使从涡旋室形成部向叶轮的半径方向外侧延伸设置的凸缘部与轴承框架结合的结构中,难以确保凸缘部与涡旋室形成部之间的空间,有为了防止第2螺栓的断裂而难以在第2螺栓的头部与涡旋室框架之间设置衬套的情况。In the structure where the flange portion extending from the swirl chamber forming portion to the radially outer side of the impeller is combined with the bearing frame, it is difficult to secure a space between the flange portion and the swirl chamber forming portion. In case of fracture, it is difficult to install a bushing between the head of the second bolt and the frame of the scroll chamber.
即使在这样的情况下,根据上述(7)所述的压缩机,能够通过构成为对涡旋室框架与轴承框架进行夹持的夹具抑制在第2螺栓产生拉伸应力,有效抑制第2螺栓的断裂。因此,能够实现涡旋室框架与轴承框架的稳定的结合状态。Even in such a case, according to the compressor described in (7) above, the occurrence of tensile stress on the second bolt can be suppressed by the clamp configured to clamp the scroll chamber frame and the bearing frame, and the tension of the second bolt can be effectively suppressed. of the break. Therefore, a stable coupling state of the scroll chamber frame and the bearing frame can be realized.
在几个实施方式中,在上述(7)所述的压缩机中,In several embodiments, in the compressor described in (7) above,
(8)所述夹具具有按压螺栓,该按压螺栓对所述轴承框架从与所述涡旋室框架的所述凸缘部相反的一侧施加按压。(8) The jig has a pressing bolt for pressing the bearing frame from a side opposite to the flange portion of the scroll chamber frame.
在使从涡旋室形成部向叶轮的半径方向外侧延伸设置的凸缘部与轴承框架结合的结构中,难以确保凸缘部与涡旋室形成部之间的空间,有为了防止第2螺栓的断裂而难以在第2螺栓的头部与涡旋室框架之间设置衬套的情况。In the structure where the flange portion extending from the swirl chamber forming portion to the radially outer side of the impeller is combined with the bearing frame, it is difficult to secure a space between the flange portion and the swirl chamber forming portion. In case of fracture, it is difficult to install a bushing between the head of the second bolt and the frame of the scroll chamber.
即使在这样的情况下,根据上述(8)所述的压缩机,设置对轴承框架从与涡旋室框架的凸缘部相反的一侧施加按压的按压螺栓的话,能够以简单的结构抑制在第2螺栓产生拉伸应力,有效抑制第2螺栓的断裂。因此,能够以简单的结构实现涡旋室框架与轴承框架的稳定的结合状态。Even in such a case, according to the compressor described in (8) above, if the pressing bolt that presses the bearing frame from the side opposite to the flange portion of the scroll chamber frame is provided, it can be suppressed with a simple structure. Tensile stress is generated in the second bolt, effectively suppressing the breakage of the second bolt. Therefore, a stable coupling state of the scroll chamber frame and the bearing frame can be realized with a simple structure.
(9)本发明的几个实施方式的增压器具备上述(1)乃至(8)任一项所述的压缩机。(9) A supercharger according to some embodiments of the present invention includes the compressor described in any one of (1) to (8).
在本发明的几个实施方式的增压器中,即使因叶轮的断裂而产生拉伸应力,也能够有效抑制第1螺栓的断裂。即,能够实现涡旋室框架与第1框架的稳定的结合状态。In the supercharger according to some embodiments of the present invention, even if tensile stress occurs due to fracture of the impeller, fracture of the first bolt can be effectively suppressed. That is, a stable coupling state between the scroll chamber frame and the first frame can be realized.
发明的效果The effect of the invention
根据本发明的几个实施方式,能够有效抑制紧固相邻于涡旋室框架的框架和涡旋室框架的螺栓的断裂,实现这些框架的稳定的结合状态。According to several embodiments of the present invention, it is possible to effectively suppress breakage of the bolts fastening the frame adjacent to the scroll chamber frame and the scroll chamber frame, and achieve a stable combined state of these frames.
附图说明Description of drawings
图1是表示几个实施方式的内燃机系统的整体结构的概要图。FIG. 1 is a schematic diagram showing the overall configuration of an internal combustion engine system according to some embodiments.
图2是几个实施方式的增压器的一部分的概要剖视图。Fig. 2 is a schematic sectional view of a part of a supercharger according to some embodiments.
图3是紧固涡旋室框架与消音器框架的螺栓的周边的概要剖视图。Fig. 3 is a schematic cross-sectional view around bolts fastening a scroll chamber frame and a muffler frame.
图4是表示涡旋室框架变形而在紧固涡旋室框架与轴承框架的螺栓产生拉伸应力的状态的图。4 is a view showing a state in which a scroll chamber frame is deformed and tensile stress is generated in bolts fastening the scroll chamber frame and the bearing frame.
图5是从图2的P方向观察到的涡旋室框架的凸缘部与轴承框架的凸缘部的图。Fig. 5 is a view of a flange portion of a scroll chamber frame and a flange portion of a bearing frame viewed from the direction P in Fig. 2 .
图6是用于对几个实施方式的夹具的结构进行说明的概要剖视图。Fig. 6 is a schematic cross-sectional view for explaining the structure of the jig of some embodiments.
符号说明Symbol Description
2 内燃机2 internal combustion engine
4 增压器4 superchargers
6 涡轮6 turbo
8 发电机8 generators
10 压缩器10 compressors
12 旋转轴12 axis of rotation
13 消音器13 silencer
14 叶轮14 impeller
16 空气引导筒16 Air guide barrel
17 翼17 wings
18 涡旋室18 Vortex chamber
19 涡旋室形成部19 Vortex chamber forming part
20 涡旋室框架20 Vortex chamber frame
22 消音器框架22 muffler frame
23,24,29,46 凸缘部23, 24, 29, 46 Flange
25,48 螺栓25, 48 bolts
26,52 头部26, 52 head
28 衬套28 Bushing
30 倾斜部30 Inclined part
31 轴部31 Shaft
32 入口部32 entrance
40 轴承框架40 bearing frame
43 出口部43 Export Department
44 轴承部44 Bearing
50 扩散部50 Diffusion Department
54 夹具54 Fixtures
56 按压螺栓56 Press bolt
100 内燃机系统100 Internal combustion engine systems
d1 内径d 1 inner diameter
d2 直径d 2 diameter
d3,d4 尺寸d 3 , d 4 size
具体实施方式detailed description
以下,按照附图对本发明的实施方式进行说明。但是,该实施方式所记载的结构零件的尺寸、材质、形状及其相对的配置等若无特定的记载则不是将本发明的范围限定于此的主旨,只不过是说明例而已。Embodiments of the present invention will be described below with reference to the drawings. However, the dimensions, materials, shapes, relative arrangements, and the like of the components described in this embodiment are not intended to limit the scope of the present invention thereto, and are merely illustrative examples.
图1是表示几个实施方式的内燃机系统100的整体结构的概要图。FIG. 1 is a schematic diagram showing the overall configuration of an internal combustion engine system 100 according to some embodiments.
图1所示的内燃机系统100具备:内燃机2、对向内燃机2的进气进行加压的增压器4及由增压器4所具有的涡轮6驱动的发电机8。An internal combustion engine system 100 shown in FIG. 1 includes an internal combustion engine 2 , a supercharger 4 that pressurizes intake air to the internal combustion engine 2 , and a generator 8 driven by a turbine 6 included in the supercharger 4 .
图1所示的增压器4具备:对向内燃机2的进气进行加压的离心式的压缩器(压缩机)10、经由旋转轴12与压缩器10连结且通过内燃机2的排气而被驱动的涡轮6及用于使压缩器10产生的声音降低的消音器13。Supercharger 4 shown in FIG. The driven turbine 6 and the muffler 13 for reducing the sound generated by the compressor 10 .
在图1所示的增压器4中,像这样,使用通过由内燃机2的排气所驱动的涡轮6来驱动压缩器10的排气涡轮式的增压器(所谓涡轮增压器)。在其他实施方式的增压器4中,也可以使用通过从内燃机2的输出轴经由带等传递的动力来驱动压缩器10的机械式的增压器(所谓机械增压器)。另外,作为内燃机2,例如能够适当选择柴油机、汽油发动机等。In the supercharger 4 shown in FIG. 1 , an exhaust turbine type supercharger (so-called turbocharger) in which the compressor 10 is driven by the turbine 6 driven by the exhaust gas of the internal combustion engine 2 is used. As the supercharger 4 in another embodiment, a mechanical supercharger (so-called supercharger) that drives the compressor 10 by power transmitted from the output shaft of the internal combustion engine 2 via a belt or the like may be used. In addition, as the internal combustion engine 2, for example, a diesel engine, a gasoline engine, or the like can be appropriately selected.
接着,根据图2对增压器4的具体的结构例进行如下说明。Next, a specific configuration example of the supercharger 4 will be described below with reference to FIG. 2 .
图2是几个实施方式的增压器4的一部分的概要剖视图。FIG. 2 is a schematic cross-sectional view of a part of the turbocharger 4 according to some embodiments.
图2所示的压缩器10包含:用于压缩空气的叶轮14、用于收容叶轮14且引导空气的空气引导筒16、涡旋室框架20及轴承框架40。叶轮14包含轮毂15及设置于轮毂15周围的多个翼17。涡旋室框架20与空气引导筒16相邻而设置,涡旋室框架20具有形成用于将通过空气引导筒16的空气向外部引导的涡旋室18的涡旋室形成部19。在轴承框架40设置有轴承部44,轴承部44轴支承叶轮14的旋转轴12。The compressor 10 shown in FIG. 2 includes: an impeller 14 for compressing air, an air guide cylinder 16 for accommodating the impeller 14 and guiding air, a scroll chamber frame 20 and a bearing frame 40 . The impeller 14 includes a hub 15 and a plurality of wings 17 arranged around the hub 15 . The swirl chamber frame 20 is provided adjacent to the air guide cylinder 16 , and has a swirl chamber forming portion 19 forming the swirl chamber 18 for guiding the air passing through the air guide cylinder 16 to the outside. The bearing frame 40 is provided with a bearing portion 44 that pivotally supports the rotating shaft 12 of the impeller 14 .
消音器13包含与涡旋室框架20相邻而设置的消音器框架22。涡旋室框架20与消音器框架22是通过螺栓25紧固涡旋室框架20的凸缘部23与消音器框架22的凸缘部24。在螺栓25的头部26与涡旋室框架20之间设置衬套28(参照图3)。The muffler 13 includes a muffler frame 22 provided adjacent to the swirl chamber frame 20 . The swirl chamber frame 20 and the muffler frame 22 are fastened by bolts 25 to the flange portion 23 of the swirl chamber frame 20 and the flange portion 24 of the muffler frame 22 . A bush 28 is provided between the head 26 of the bolt 25 and the scroll chamber frame 20 (see FIG. 3 ).
轴承框架40与涡旋室框架20是通过螺栓48紧固轴承框架40的凸缘部46与涡旋室框架20的凸缘部29。The bearing frame 40 and the scroll chamber frame 20 are fastened to the flange portion 46 of the bearing frame 40 and the flange portion 29 of the scroll chamber frame 20 by bolts 48 .
在图2所示的构成增压器4的一部分的压缩器10中,若叶轮14断裂的话,有叶轮碎片向叶轮14的半径方向外侧飞散,而与空气引导筒16、涡旋室框架20等碰撞的情况。In the compressor 10 constituting a part of the supercharger 4 shown in FIG. 2 , if the impeller 14 breaks, the impeller fragments will fly outward in the radial direction of the impeller 14, and will interfere with the air guide cylinder 16, the scroll chamber frame 20, etc. Collision situation.
例如,叶轮碎片与空气引导筒16的倾斜部30碰撞的话,由于该碰撞的影响,空气引导筒16的入口部32沿箭头S方向(参照图3)向消音器13侧移动而与消音器框架22的出口部43碰撞。由此,消音器框架22的凸缘部24会向远离涡旋室框架20的凸缘部23的方向移动,因此在螺栓25产生拉伸应力。For example, if the impeller debris collides with the inclined portion 30 of the air guide cylinder 16, the inlet portion 32 of the air guide cylinder 16 moves toward the muffler 13 in the direction of arrow S (see FIG. The exit portion 43 of 22 collides. As a result, the flange portion 24 of the muffler frame 22 moves away from the flange portion 23 of the scroll chamber frame 20 , so tensile stress is generated in the bolt 25 .
即使像这样在螺栓25产生拉伸应力的情况下,根据压缩器10及增压器4,由于在螺栓25的头部26与涡旋室框架20之间设置有衬套28,因此与不设置衬套28的情况相比,能够使用轴部31(图3参照)的长度(颈部的长度)较长的螺栓25来紧固涡旋室框架20与消音器框架22。因此,与不设置衬套28的情况相比,在对螺栓25施加了轴向的拉伸负荷时,能够不使螺栓25断裂而增大能够伸长的伸长量。由此,即使对紧固涡旋室框架20与消音器框架22的螺栓25产生因如上所述的叶轮14的断裂而导致的拉伸应力,也能够有效抑制螺栓25的断裂。因此,能够使涡旋室框架20与消音器框架22稳定地结合,有效抑制消音器13从增压器4、压缩器10脱落。Even when tensile stress is generated in the bolt 25 like this, according to the compressor 10 and the supercharger 4, since the bushing 28 is provided between the head 26 of the bolt 25 and the scroll chamber frame 20, it is different from not installing the bushing 28 . Compared with the case of the bushing 28, the swirl chamber frame 20 and the muffler frame 22 can be fastened using the bolt 25 having a longer length (neck length) of the shaft portion 31 (see FIG. 3 ). Therefore, when a tensile load in the axial direction is applied to the bolt 25, the amount of elongation that can be extended can be increased without breaking the bolt 25, compared to the case where the bush 28 is not provided. Thus, even if tensile stress due to breakage of the impeller 14 as described above occurs on the bolts 25 fastening the scroll chamber frame 20 and the muffler frame 22 , breakage of the bolts 25 can be effectively suppressed. Therefore, the scroll chamber frame 20 and the muffler frame 22 can be stably coupled, and the muffler 13 can be effectively suppressed from coming off from the supercharger 4 and the compressor 10 .
图3所示的衬套28形成为套筒状且以包围螺栓25的轴部31的方式设置,衬套28的内径d1比螺栓25的头部26的直径d2小。因此,由于能够通过衬套28均匀地支承螺栓25的头部26,因此即使如上所述在螺栓25产生因叶轮14的断裂导致的拉伸应力,也能够有效抑制螺栓25的断裂。 Bushing 28 shown in FIG. Therefore, since the heads 26 of the bolts 25 can be uniformly supported by the bushes 28 , even if tensile stress due to fracture of the impeller 14 occurs in the bolts 25 as described above, fracture of the bolts 25 can be effectively suppressed.
另外,图3所示的螺栓25的轴向上的衬套28的尺寸d3比螺栓25的径方向上的衬套28的尺寸d4大。这样一来,通过使用适合使螺栓25的轴部31的长度变长的衬套28,从而能够在对螺栓25施加了轴向的拉伸负荷时不使螺栓25断裂而容易地使能够伸长的伸长量变大。由此,即使对紧固涡旋室框架20与消音器框架22的螺栓25产生因如上所述的叶轮14的断裂而导致的拉伸应力,也能够有效抑制螺栓25的断裂。In addition, the dimension d3 of the bushing 28 in the axial direction of the bolt 25 shown in FIG. 3 is larger than the dimension d4 of the bushing 28 in the radial direction of the bolt 25 . In this way, by using the bush 28 suitable for increasing the length of the shaft portion 31 of the bolt 25 , when an axial tensile load is applied to the bolt 25 , the bolt 25 can be easily extended without breaking the bolt 25 . The elongation becomes larger. Thus, even if tensile stress due to breakage of the impeller 14 as described above occurs on the bolts 25 fastening the scroll chamber frame 20 and the muffler frame 22 , breakage of the bolts 25 can be effectively suppressed.
在图3中,说明了因叶轮14的断裂而在紧固涡旋室框架20与消音器框架22的螺栓25产生拉伸应力的例子,但有因叶轮14的断裂而在紧固涡旋室框架20与轴承框架40的螺栓48产生拉伸应力的情况。In FIG. 3 , an example in which tensile stress occurs in the bolts 25 fastening the vortex chamber frame 20 and the muffler frame 22 due to the fracture of the impeller 14 is illustrated, but there is a case where the fracture of the impeller 14 causes tension in the bolt 25 fastening the vortex chamber. The frame 20 and the bolts 48 of the bearing frame 40 produce tensile stress.
例如,在叶轮碎片侵入图2的扩散部50而堵塞扩散部50的情况下,该叶轮碎片导致扩散部50在叶轮14的轴向上扩张。由此,涡旋室框架20与轴承框架受到相互离开的方向的力,因此如图4所示,涡旋室框架20变形而在螺栓48产生拉伸应力。For example, when impeller fragments intrude into the diffuser 50 of FIG. 2 to clog the diffuser 50 , the impeller fragments cause the diffuser 50 to expand in the axial direction of the impeller 14 . As a result, the scroll chamber frame 20 and the bearing frame receive a force in a direction away from each other. As shown in FIG. 4 , the scroll chamber frame 20 is deformed and tensile stress is generated in the bolt 48 .
为了不因该拉伸应力而导致螺栓48断裂,在几个实施方式中,也可以通过将根据图3进行了说明的衬套28设置在螺栓48的头部52与涡旋室框架20之间,从而使螺栓48的轴部53比图4所示的结构长。然而,如图2所示,涡旋室框架20的凸缘部29从涡旋室形成部19向叶轮14的半径方向外侧延伸设置,因此有难以确保凸缘部29与涡旋室形成部19之间的空间,而难以为了防止螺栓48的断裂而在螺栓48的头部52与涡旋室框架20之间设置衬套的情况。In order not to cause the bolt 48 to break due to the tensile stress, in several embodiments, it is also possible to arrange the bushing 28 described with reference to FIG. , so that the shaft portion 53 of the bolt 48 is longer than the structure shown in FIG. 4 . However, as shown in FIG. 2 , the flange portion 29 of the swirl chamber frame 20 is extended from the swirl chamber forming portion 19 to the radial direction outside of the impeller 14, so it is difficult to ensure that the flange portion 29 and the swirl chamber forming portion 19 Therefore, it is difficult to provide a bushing between the head 52 of the bolt 48 and the scroll chamber frame 20 in order to prevent the bolt 48 from breaking.
因此,图2所示的增压器4及压缩器10具有如图5及图6所示的夹具54,夹具54构成为对涡旋室框架20与轴承框架40进行夹持。图5是从图2的P方向观察到的涡旋室框架20的凸缘部29与轴承框架40的凸缘部46的图,表示螺栓48及夹具54的配置。图6是用于对夹具54的结构进行说明的概要剖视图。Therefore, the supercharger 4 and the compressor 10 shown in FIG. 2 have the clamp 54 shown in FIGS. 5 and 6 , and the clamp 54 is configured to clamp the scroll chamber frame 20 and the bearing frame 40 . 5 is a view of the flange portion 29 of the scroll chamber frame 20 and the flange portion 46 of the bearing frame 40 as viewed from the direction P in FIG. 2 , showing the arrangement of the bolts 48 and the clamps 54 . FIG. 6 is a schematic cross-sectional view for explaining the structure of the jig 54 .
这样一来,通过使用构成为对涡旋室框架20的凸缘部29与轴承框架40的凸缘部46进行夹持的夹具54,从而即使在难以确保充足的用于在凸缘部29与涡旋室形成部19之间设置上述衬套的空间的结构中,也能够抑制在螺栓48产生拉伸应力,能够有效地抑制螺栓48的断裂。因此,能够稳定地结合涡旋室框架20与轴承框架40。In this way, by using the jig 54 configured to clamp the flange portion 29 of the scroll chamber frame 20 and the flange portion 46 of the bearing frame 40, even when it is difficult to secure a sufficient gap between the flange portion 29 and the flange portion 46, Also in the structure in which the space for the above-mentioned bush is provided between the scroll chamber forming portions 19, generation of tensile stress on the bolt 48 can be suppressed, and breakage of the bolt 48 can be effectively suppressed. Therefore, it is possible to stably couple the scroll chamber frame 20 and the bearing frame 40 .
图5及图6所示的夹具54具有按压螺栓56,该按压螺栓56对轴承框架40从与涡旋室框架20的凸缘部29相反的一侧施加按压。由此,即使在以防止螺栓48的断裂为目的而难以如上所述在螺栓48的头部52与涡旋室框架20之间设置衬套的情况下,也能够以简单的结构抑制在螺栓48产生拉伸应力,能够有效抑制螺栓48的断裂。因此,能够以简单的结构而稳定地结合涡旋室框架20与轴承框架40。另外,在其他实施方式中,也可以使用对涡旋室框架20的凸缘部29从与轴承框架40相反的一侧施加按压的按压螺栓。The jig 54 shown in FIGS. 5 and 6 has a pressing bolt 56 that presses the bearing frame 40 from the side opposite to the flange portion 29 of the scroll chamber frame 20 . Thus, even if it is difficult to provide a bushing between the head portion 52 of the bolt 48 and the scroll chamber frame 20 as described above for the purpose of preventing the bolt 48 from breaking, it is possible to suppress the breakage of the bolt 48 with a simple structure. The generation of tensile stress can effectively suppress the breakage of the bolt 48 . Therefore, the scroll chamber frame 20 and the bearing frame 40 can be stably coupled with a simple structure. In addition, in other embodiments, a pressing bolt that presses the flange portion 29 of the scroll chamber frame 20 from the side opposite to the bearing frame 40 may be used.
在根据图6进行了说明的实施方式中,例示了构成为对涡旋室框架20与轴承框架40进行夹持的夹具54,但在其他实施方式中,也可以使用构成为对涡旋室框架20与消音器框架22进行夹持的夹具。由此,能够使涡旋室框架20与消音器框架22稳定地结合。In the embodiment described with reference to FIG. 6 , the clamp 54 configured to clamp the scroll chamber frame 20 and the bearing frame 40 is illustrated, but in other embodiments, a clamp configured to clamp the scroll chamber frame 20 and the bearing frame 40 may also be used. 20 and the muffler frame 22 for clamping. Thereby, the swirl chamber frame 20 and the muffler frame 22 can be stably coupled.
Claims (10)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2013-198638 | 2013-09-25 | ||
| JP2013198638A JP6097188B2 (en) | 2013-09-25 | 2013-09-25 | Turbocharger |
| CN201480041368.0A CN105531460B (en) | 2013-09-25 | 2014-06-30 | Compressor and Supercharger |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201480041368.0A Division CN105531460B (en) | 2013-09-25 | 2014-06-30 | Compressor and Supercharger |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107701298A true CN107701298A (en) | 2018-02-16 |
| CN107701298B CN107701298B (en) | 2020-03-27 |
Family
ID=52742699
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710818678.4A Active CN107701298B (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
Country Status (5)
| Country | Link |
|---|---|
| EP (2) | EP3173630B1 (en) |
| JP (1) | JP6097188B2 (en) |
| KR (1) | KR101799707B1 (en) |
| CN (1) | CN107701298B (en) |
| WO (1) | WO2015045541A1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3053384B1 (en) * | 2016-06-30 | 2018-07-27 | Safran Aircraft Engines | FIXING ASSEMBLY OF A DISTRIBUTOR TO A STRUCTURAL ELEMENT OF A TURBOMACHINE |
| JP6517386B2 (en) * | 2018-02-13 | 2019-05-22 | 三菱重工業株式会社 | Centrifugal compressor and supercharger |
| JP7562357B2 (en) * | 2020-09-30 | 2024-10-07 | 三菱重工マリンマシナリ株式会社 | Rotating Machinery |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1920312A (en) * | 2005-08-22 | 2007-02-28 | 曼·B及W柴油机公开股份有限公司 | External housing safety device for turbocharger with axial flow fluid compressor |
| US20080080966A1 (en) * | 2006-09-29 | 2008-04-03 | Jtket Corporation | Turbocharger |
| CN202614598U (en) * | 2012-05-21 | 2012-12-19 | 上海大学 | High-intensity steel plate stretching auxiliary clamping device |
| CN103069128A (en) * | 2010-09-03 | 2013-04-24 | 博格华纳公司 | Turbocharger housing seal |
Family Cites Families (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2948398A1 (en) * | 1979-12-01 | 1981-06-04 | Skf Kugellagerfabriken Gmbh, 8720 Schweinfurt | EXHAUST TURBOCHARGER |
| JPS5939930A (en) * | 1982-08-27 | 1984-03-05 | Nissan Motor Co Ltd | Turbocharger |
| JPH0195536U (en) * | 1987-12-18 | 1989-06-23 | ||
| JPH03129731U (en) * | 1990-04-09 | 1991-12-26 | ||
| WO1992016725A1 (en) * | 1991-03-18 | 1992-10-01 | Moody Ralph A Jr | Apparatus regulating exhaust flow to increase back pressure in an internal combustion engine |
| EP0574605B1 (en) * | 1992-06-17 | 1996-11-20 | Asea Brown Boveri Ag | Filter-silencer |
| US5295785A (en) * | 1992-12-23 | 1994-03-22 | Caterpillar Inc. | Turbocharger having reduced noise emissions |
| DE59308448D1 (en) * | 1993-09-03 | 1998-05-28 | Asea Brown Boveri | Method for adapting the radial turbine of a turbocharger to an internal combustion engine |
| JPH1122568A (en) * | 1997-07-08 | 1999-01-26 | Aisan Ind Co Ltd | Intake device for internal combustion engine |
| DE19745659C1 (en) * | 1997-10-17 | 1999-05-06 | Man B & W Diesel Ag | Turbo-supercharger for internal combustion engine |
| DE19818873C2 (en) * | 1998-04-28 | 2001-07-05 | Man B & W Diesel Ag | Reciprocating internal combustion engine |
| JP4359798B2 (en) | 1999-11-05 | 2009-11-04 | 株式会社Ihi | Exhaust turbine turbocharger |
| EP1186781B2 (en) * | 2000-09-08 | 2012-05-30 | ABB Turbo Systems AG | Filter silencer mounting device for turbo charger inlet |
| DE102004028133C5 (en) * | 2004-06-09 | 2017-10-26 | Man Diesel & Turbo Se | Turbomachine, in particular exhaust gas turbocharger |
| DE102004055429B3 (en) * | 2004-11-17 | 2006-08-10 | Man B & W Diesel Ag | Sealing device for a particularly lubricated at standstill bearing a rotor shaft |
| KR200422136Y1 (en) * | 2006-05-04 | 2006-07-24 | 남순선 | Connection clamp of gas inlet pipe |
| EP1860284A1 (en) * | 2006-05-23 | 2007-11-28 | ABB Turbo Systems AG | Casings assembling |
| WO2008023033A1 (en) * | 2006-08-24 | 2008-02-28 | Abb Turbo Systems Ag | Attaching a filter muffler |
| JP5526999B2 (en) * | 2010-05-10 | 2014-06-18 | 株式会社Ihi | Silencers and turbochargers |
| DE102010028975A1 (en) * | 2010-05-14 | 2012-03-29 | Abb Turbo Systems Ag | Additional compressor housing |
| DE102011010673A1 (en) * | 2011-02-08 | 2012-08-09 | Voith Patent Gmbh | Housing for an exhaust gas turbocharger or a turbocompound system |
| JP2011174477A (en) * | 2011-06-17 | 2011-09-08 | Jtekt Corp | Supercharger |
| US8857178B2 (en) * | 2011-06-28 | 2014-10-14 | Caterpillar Inc. | Nozzled turbocharger turbine and associated engine and method |
| KR101990880B1 (en) * | 2012-02-17 | 2019-06-19 | 보르그워너 인코퍼레이티드 | Multi-segment turbocharger bearing housing and methods therefor |
| CN102650296A (en) * | 2012-06-11 | 2012-08-29 | 重庆江增船舶重工有限公司 | High-speed and small-flow centrifugal type compressor set |
-
2013
- 2013-09-25 JP JP2013198638A patent/JP6097188B2/en active Active
-
2014
- 2014-06-30 EP EP16205770.7A patent/EP3173630B1/en active Active
- 2014-06-30 CN CN201710818678.4A patent/CN107701298B/en active Active
- 2014-06-30 EP EP14849505.4A patent/EP3009633B1/en active Active
- 2014-06-30 KR KR1020167002207A patent/KR101799707B1/en active Active
- 2014-06-30 WO PCT/JP2014/067415 patent/WO2015045541A1/en not_active Ceased
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1920312A (en) * | 2005-08-22 | 2007-02-28 | 曼·B及W柴油机公开股份有限公司 | External housing safety device for turbocharger with axial flow fluid compressor |
| US20080080966A1 (en) * | 2006-09-29 | 2008-04-03 | Jtket Corporation | Turbocharger |
| CN103069128A (en) * | 2010-09-03 | 2013-04-24 | 博格华纳公司 | Turbocharger housing seal |
| CN202614598U (en) * | 2012-05-21 | 2012-12-19 | 上海大学 | High-intensity steel plate stretching auxiliary clamping device |
Also Published As
| Publication number | Publication date |
|---|---|
| KR20160023893A (en) | 2016-03-03 |
| WO2015045541A1 (en) | 2015-04-02 |
| EP3173630B1 (en) | 2018-08-15 |
| JP6097188B2 (en) | 2017-03-15 |
| KR101799707B1 (en) | 2017-11-20 |
| JP2015063956A (en) | 2015-04-09 |
| CN107701298B (en) | 2020-03-27 |
| EP3009633A4 (en) | 2016-09-14 |
| EP3173630A1 (en) | 2017-05-31 |
| CN105531460A (en) | 2016-04-27 |
| EP3009633B1 (en) | 2020-02-05 |
| EP3009633A1 (en) | 2016-04-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11396889B2 (en) | Supercharger and motor cooling method | |
| US9995158B2 (en) | Split nozzle ring to control EGR and exhaust flow | |
| JP5894203B2 (en) | Supercharger manufacturing method | |
| JP6240251B2 (en) | Compressor and supercharger | |
| WO2015151653A1 (en) | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor | |
| KR100818839B1 (en) | Exhaust gas turbine supercharger | |
| CN107701298A (en) | Compressor and booster | |
| US20120186247A1 (en) | Turbocharger with Reversed Compressor Volute Optionally Integrated into the Center Housing | |
| KR101547092B1 (en) | Silencer for supercharger | |
| CN105814319B (en) | Compressor and booster | |
| CN101506531B (en) | Fixing mechanism for filter muffler | |
| US10077785B2 (en) | Impeller assembly, turbocharger, and method of assembling impeller assembly | |
| CN105531460B (en) | Compressor and Supercharger | |
| US20190063445A1 (en) | Motor, turbocharger and assembly method turbocharger | |
| EP2693018A1 (en) | Turbocharger | |
| CN104619972A (en) | Gas turbine device | |
| KR102646973B1 (en) | Bearing structure, supercharger equipped with the same, and method of assembling the supercharger | |
| US20180142699A1 (en) | Compressor Assembly for a Turbocharger | |
| JP2019044776A (en) | Turbocharger |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20250610 Address after: No.1, 1-1, shiozhimachi, Nagasaki, Nagasaki, Japan Patentee after: Mitsubishi Heavy Industries Marine Machinery Co.,Ltd. Country or region after: Japan Address before: Japan's Tokyo port harbor two chome 16 No. 5 Patentee before: MITSUBISHI HEAVY INDUSTRIES, Ltd. Country or region before: Japan |
|
| TR01 | Transfer of patent right |