JP2015197053A5 - Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer - Google Patents
Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer Download PDFInfo
- Publication number
- JP2015197053A5 JP2015197053A5 JP2014074071A JP2014074071A JP2015197053A5 JP 2015197053 A5 JP2015197053 A5 JP 2015197053A5 JP 2014074071 A JP2014074071 A JP 2014074071A JP 2014074071 A JP2014074071 A JP 2014074071A JP 2015197053 A5 JP2015197053 A5 JP 2015197053A5
- Authority
- JP
- Japan
- Prior art keywords
- centrifugal compressor
- scroll
- flange portion
- scroll casing
- fastening
- 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
- 230000003584 silencer Effects 0.000 title claims description 12
- 238000004519 manufacturing process Methods 0.000 title description 4
- 238000005192 partition Methods 0.000 claims description 10
- 239000012530 fluid Substances 0.000 claims 14
- 230000002093 peripheral Effects 0.000 claims 9
- 238000011144 upstream manufacturing Methods 0.000 claims 3
- 229910000831 Steel Inorganic materials 0.000 claims 2
- 239000010959 steel Substances 0.000 claims 2
- 238000002485 combustion reaction Methods 0.000 claims 1
- 239000000463 material Substances 0.000 claims 1
- 230000001629 suppression Effects 0.000 description 3
Description
本発明は、遠心圧縮機、過給機、および遠心圧縮機の製造方法、並びにサイレンサに関する。 The present invention relates to a centrifugal compressor, a supercharger, a method for manufacturing a centrifugal compressor, and a silencer .
本発明は、このような事情を鑑みてなされたものであり、羽根車の全部または一部が破断あるいは脱落するのに伴って案内筒の全部または一部が飛散する場合に、羽根車の全部または一部が外部に飛散する不具合を抑制することが可能な遠心圧縮機を提供することを目的とする。
また、本発明は、前述した遠心圧縮機を備えた過給機、および前述した遠心圧縮機の製造方法、並びに前述した遠心圧縮機に取り付けられるサイレンサを提供することを目的とする。
The present invention has been made in view of such circumstances. When all or a part of the guide tube is scattered as the whole or a part of the impeller is broken or dropped, the entire impeller is provided. Another object of the present invention is to provide a centrifugal compressor capable of suppressing a problem that a part of the air is scattered outside.
Another object of the present invention is to provide a turbocharger including the above-described centrifugal compressor, a method for manufacturing the above-described centrifugal compressor, and a silencer attached to the above-described centrifugal compressor .
本発明によれば、羽根車の全部または一部が破断あるいは脱落するのに伴って案内筒の全部または一部が飛散する場合に、羽根車の全部または一部が外部に飛散する不具合を抑制することが可能な遠心圧縮機を提供することができる。
また、本発明によれば、前述した遠心圧縮機を備えた過給機、および前述した遠心圧縮機の製造方法、並びに前述した遠心圧縮機に取り付けられるサイレンサを提供することができる。
According to the present invention, when all or a part of the impeller is scattered as a whole or a part of the impeller is broken or dropped, it is possible to suppress a problem that all or a part of the impeller is scattered to the outside. It is possible to provide a centrifugal compressor that can be used.
Moreover, according to this invention, the turbocharger provided with the centrifugal compressor mentioned above, the manufacturing method of the centrifugal compressor mentioned above, and the silencer attached to the centrifugal compressor mentioned above can be provided.
前述したように空気案内筒12が取付位置から脱落すると、空気案内筒12が仕切板14に衝突する。この衝突によってスクロールケーシング13bが軸受台20から離間する方向の衝撃力が加わる。この衝撃力は、締結ボルト41とフランジ部13fとフランジ部20aの締結位置に作用する。 As described above, when the air guide tube 12 is dropped from the mounting position, the air guide tube 12 collides with the partition plate 14. Due to this collision, an impact force is applied in a direction in which the scroll casing 13b is separated from the bearing base 20. This impact force acts on the fastening position of the fastening bolt 41, the flange portion 13f, and the flange portion 20a.
本実施形態の遠心圧縮機10によれば、スクロール部13から離れる方向に飛散する空気案内筒12の全部または一部が仕切板14を収容するサイレンサケーシング15aに衝突すると、スクロールケーシング13bを軸受台20のフランジ部20aから引き離す方向の衝撃が加わる。この衝撃は、締結ボルト41の頭部41aとスクロールケーシング13bとの間に配置されるスペーサ51が収縮することにより吸収される。このように、締結ボルト41に挿入した状態で締結されるスペーサ51を用いて、軸線X方向の衝撃を吸収することにより締結ボルト41が破断する不具合が抑制される。よって、空気案内筒12の全部または一部の飛散によって遠心圧縮機10の一部に隙間が生じ、その隙間から羽根車11の全部または一部が外部に飛散する不具合を抑制することができる。 According to the centrifugal compressor 10 of the present embodiment, when all or a part of the air guide cylinder 12 scattered in a direction away from the scroll portion 13 collides with the silencer casing 15a accommodating the partition plate 14, the scroll casing 13b is moved to the bearing stand. The impact of the direction pulled away from 20 flange parts 20a is added. This impact, the spacers 51 disposed between the head 41a and the scroll casing 1 3 b of the fastening bolt 41 is absorbed by contracting. Thus, the failure | damage which the fastening bolt 41 fractures | ruptures by absorbing the impact of an axis X direction using the spacer 51 fastened in the state inserted in the fastening bolt 41 is suppressed. Therefore, it is possible to suppress a problem that a gap is generated in a part of the centrifugal compressor 10 due to scattering of all or part of the air guide cylinder 12, and all or part of the impeller 11 is scattered outside from the gap.
本実施形態において、フランジ部20aは、クランプ部材60と締結ボルト43によって締結されており、スクロールケーシング13bの軸線X方向の端面13iと、凹所60aの軸線X方向の端面60eとの間に所定の隙間60cが設けられている。そして、フランジ部20aは、スクロールケーシング13bと接触する接触面20eと、圧縮空気が流通する流路13hを形成するとともに接触面20eよりも流路13h側に配置されるフランジ部20aの端面20fとを接続する段部20gを有する。 In the present embodiment, the flange portion 20a is fastened by the clamp member 60 and the fastening bolt 43, and is predetermined between the end surface 13i in the axis X direction of the scroll casing 13b and the end surface 60e in the axis X direction of the recess 60a. The gap 60c is provided. The flange portion 20a forms a contact surface 20e that comes into contact with the scroll casing 13b, a flow passage 13h through which compressed air flows, and an end surface 20f of the flange portion 20a that is disposed closer to the flow passage 13h than the contact surface 20e. Has a step portion 20 g for connecting the two.
このようにすることで、複数の締結ボルト41が破断して軸受台20のフランジ部20aとスクロールケーシング13bとが離間してスクロールケーシング13bの軸線X方向の端面13iが凹所60aの軸線X方向の端面60eが接触する場合に、段部20gの存在によってフランジ部20aとスクロールケーシング13bとの間の口開きが抑制される。更に、段部20gの軸線X方向の幅d6が所定の隙間60dの幅d5よりも広いので、連通する隙間が発生せず、口開きをより確実に抑制することができる。 By doing so, the axis X of the axis X direction of the end face 13i is a recess 60 a of the flange portion 20a and the scroll casing 13b and is scroll casing 13b spaced apart of bearing stand 20 with a plurality of fastening bolts 41 is broken When the direction end surface 60e contacts, the presence of the step portion 20g suppresses the opening between the flange portion 20a and the scroll casing 13b. Furthermore, since the width d6 of the step portion 20g in the axis X direction is wider than the width d5 of the predetermined gap 60d, no communicating gap is generated, and the mouth opening can be more reliably suppressed.
以上の説明において、クランプ部材60は、軸受台20のフランジ部20aに締結するものとしたが、他の態様であってもよい。例えば、クランプ部材60をスクロールケーシング13bのフランジ部13fに締結するようにしてもよい。この場合、スクロールケーシング13bのフランジ部13fが軸線X方向に延びる締結穴を軸線X回りの周方向に複数有するものとなる。そして、この複数の締結穴に締結ボルト43を締結することにより、クランプ部材60がスクロールケーシング13bのフランジ部13fに締結される。また、この場合、前述した隙間60cは、軸受台20のフランジ部20aの軸線X方向の端面とクランプ部材60の凹所の軸線X方向の端面との間に設けられることとなる。 In the above description, the clamp member 60 is fastened to the flange portion 20a of the bearing stand 20, but may be in another form. For example, it may be concluded clamp member 60 to the flange portion 13 f of the scroll casing 13b. In this case, the flange portion 13 f of the scroll casing 13 b has a plurality of fastening holes extending in the axis X direction in the circumferential direction around the axis X. Then, by fastening the fastening bolt 43 to the plurality of fastening holes, the clamping member 60 is fastened to the flange portion 13 f of the scroll casing 13b. In this case, the gap 60 c described above is provided between the end surface in the axis X direction of the flange portion 20 a of the bearing base 20 and the end surface in the axis X direction of the recess of the clamp member 60.
Claims (11)
該羽根車を収容する案内筒と、
該案内筒よりも外周側に配置されるとともに前記吐出口から吐出された圧縮流体が流入するスクロール部と、
前記取込口よりも流体の流通方向の上流側に設けられるとともに前記ロータ軸の軸線方向に所定の長さを有する複数の仕切板と、
前記複数の仕切板を収容するサイレンサケーシングを有するサイレンサとを備え、
前記複数の仕切板は、前記軸線を中心として放射状に配置されるとともに該仕切板の板厚が4mm以上かつ9mm以下の圧延鋼材であることを特徴とする遠心圧縮機。 An impeller that is attached to the rotor shaft and compresses the fluid flowing from the intake port and discharges it from the discharge port;
A guide tube that houses the impeller;
A scroll portion that is arranged on the outer peripheral side of the guide tube and into which the compressed fluid discharged from the discharge port flows;
A plurality of partition plates provided upstream of the intake port in the fluid flow direction and having a predetermined length in the axial direction of the rotor shaft;
A silencer having a silencer casing for accommodating the plurality of partition plates;
The plurality of partition plates are radially arranged around the axis, and are a rolled steel material having a plate thickness of 4 mm or more and 9 mm or less.
該スクロールケーシングと前記サイレンサケーシングとが、前記軸線回りの周方向の複数の第1締結位置において前記軸線方向に延びる複数の第1締結ボルトによって締結されており、
前記スクロールケーシングと前記サイレンサケーシングとは、前記第1締結ボルトの頭部の直径よりも内径の小さい円筒状の第1スペーサ部材を、前記第1締結ボルトの軸部に挿入した状態で締結されることを特徴とする請求項1に記載の遠心圧縮機。 The scroll portion has a scroll casing forming a spiral chamber into which the compressed fluid discharged from the discharge port flows;
The scroll casing and the silencer casing are fastened by a plurality of first fastening bolts extending in the axial direction at a plurality of first fastening positions in a circumferential direction around the axis,
The scroll casing and the silencer casing are fastened in a state where a cylindrical first spacer member having an inner diameter smaller than the diameter of the head of the first fastening bolt is inserted into the shaft portion of the first fastening bolt. The centrifugal compressor according to claim 1.
該フランジ部と前記スクロールケーシングとが、前記軸線回りの複数の第2締結位置において前記軸線方向に延びる複数の第2締結ボルトによって締結されており、
前記フランジ部と前記スクロールケーシングとは、前記第2締結ボルトの頭部の直径よりも内径の小さい円筒状の第2スペーサ部材を、前記第2締結ボルトの軸部に挿入した状態で締結されることを特徴とする請求項2または請求項3に記載の遠心圧縮機。 A bearing stand having a bearing portion for supporting the rotor shaft and a flange portion for supporting the scroll portion;
The flange portion and the scroll casing are fastened by a plurality of second fastening bolts extending in the axial direction at a plurality of second fastening positions around the axis,
The flange portion and the scroll casing are fastened in a state where a cylindrical second spacer member having an inner diameter smaller than the diameter of the head of the second fastening bolt is inserted into the shaft portion of the second fastening bolt. The centrifugal compressor according to claim 2 or 3, characterized in that.
該羽根車を収容する案内筒と、
該案内筒よりも外周側に配置されるとともに前記吐出口から吐出された圧縮流体が流入する渦形室を形成するスクロールケーシングを有するスクロール部と、
前記ロータ軸を支持する軸受部および前記スクロール部を支持するフランジ部を有する軸受台と、
前記フランジ部と前記スクロールケーシングとを、前記ロータ軸の軸線回りの複数の締結位置において前記軸線方向に延びる複数のフランジ部締結ボルトと、
前記フランジ部の外周縁部と前記スクロールケーシングの外周縁部とを外周側から取り囲む凹所と、該凹所に開口するとともに前記軸線方向に沿って延びる貫通穴とを有するクランプ部材を複数備え、
前記フランジ部または前記スクロールケーシングのいずれか一方が、前記軸線方向に延びる締結穴を前記軸線回りの周方向に複数有しており、
前記フランジ部または前記スクロールケーシングのいずれか一方と前記クランプ部材とが、前記貫通穴および前記締結穴に挿入されるクランプ部材締結ボルトによって締結されており、
前記フランジ部または前記スクロールケーシングのいずれか他方の前記軸線方向の端面と、前記凹所の前記軸線方向の端面との間に所定の隙間が設けられていることを特徴とする遠心圧縮機。 An impeller that is attached to the rotor shaft and compresses the fluid flowing from the intake port and discharges it from the discharge port;
A guide tube that houses the impeller;
A scroll portion having a scroll casing that is disposed on the outer peripheral side of the guide tube and forms a spiral chamber into which the compressed fluid discharged from the discharge port flows;
A bearing base having a bearing portion for supporting the rotor shaft and a flange portion for supporting the scroll portion;
A plurality of flange portion fastening bolts extending in the axial direction at a plurality of fastening positions around the axis of the rotor shaft, the flange portion and the scroll casing;
A plurality of clamp members having a recess surrounding the outer peripheral edge of the flange portion and the outer peripheral edge of the scroll casing from the outer peripheral side, and a through-hole that opens in the recess and extends along the axial direction;
Either one of the flange portion or the scroll casing has a plurality of fastening holes extending in the axial direction in the circumferential direction around the axis,
Either the flange portion or the scroll casing and the clamp member are fastened by a clamp member fastening bolt inserted into the through hole and the fastening hole,
A centrifugal compressor, wherein a predetermined gap is provided between the axial end surface of either the flange portion or the scroll casing and the axial end surface of the recess.
前記スクロールケーシングの前記軸線方向の端面と、前記凹所の前記軸線方向の端面との間に所定の隙間が設けられており、
前記フランジ部は、前記スクロールケーシングと接触する接触面と、前記圧縮流体が流通する第2流路を形成するとともに前記接触面よりも前記第2流路側に配置される前記フランジ部の端面とを接続する段部を有することを特徴とする請求項6に記載の遠心圧縮機。 The flange portion has the fastening hole and is fastened by the clamp member and the clamp member fastening bolt,
A predetermined gap is provided between the axial end surface of the scroll casing and the axial end surface of the recess;
The flange portion includes a contact surface that contacts the scroll casing, and an end surface of the flange portion that forms a second flow path through which the compressed fluid flows and is disposed on the second flow path side with respect to the contact surface. The centrifugal compressor according to claim 6, further comprising a connecting step.
内燃機関から排出された排気ガスにより前記軸線回りに回転するとともに前記ロータ軸に連結されるタービンと、を備えることを特徴とする過給機。 The centrifugal compressor according to any one of claims 1 to 8,
A turbocharger comprising: a turbine that rotates around the axis by exhaust gas discharged from an internal combustion engine and is coupled to the rotor shaft.
前記羽根車を収容するように案内筒を取り付けて前記取込口から流入する流体を前記吐出口へ導く流路を形成する工程と、
前記吐出口から吐出された圧縮流体が流入するスクロール部を、前記案内筒よりも前記軸線方向に直交する径方向の外周側に配置する工程と、
板厚が4mm以上かつ9mm以下の複数の仕切板を、前記取込口よりも流体の流通方向の上流側に設けるとともに前記軸線方向に所定の長さを有するように前記軸線を中心として放射状に配置する工程と、を備えることを特徴とする遠心圧縮機の製造方法。 Attaching the impeller that compresses the fluid flowing in from the intake port and discharges it from the discharge port to the rotor shaft;
Attaching a guide tube so as to accommodate the impeller and forming a flow path for guiding fluid flowing in from the intake port to the discharge port;
A step of arranging a scroll portion into which the compressed fluid discharged from the discharge port flows, on the outer peripheral side in the radial direction perpendicular to the axial direction from the guide tube;
A plurality of partition plates having a thickness of 4 mm or more and 9 mm or less are provided on the upstream side in the fluid flow direction from the intake port, and are radially centered on the axis so as to have a predetermined length in the axial direction. And a step of arranging the centrifugal compressor.
前記取込口よりも流体の流通方向の上流側に設けられるとともに前記ロータ軸の軸線方向に所定の長さを有する複数の仕切板と、A plurality of partition plates provided upstream of the intake port in the fluid flow direction and having a predetermined length in the axial direction of the rotor shaft;
前記複数の仕切板を収容するサイレンサケーシングを備え、A silencer casing for accommodating the plurality of partition plates;
前記複数の仕切板は、前記軸線を中心として放射状に配置されるとともに該仕切板の板厚が4mm以上かつ9mm以下の圧延鋼材であることを特徴とするサイレンサ。The silencer, wherein the plurality of partition plates are arranged in a radial pattern about the axis, and are made of rolled steel having a partition plate thickness of 4 mm or more and 9 mm or less.
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014074071A JP6391970B2 (en) | 2014-03-31 | 2014-03-31 | Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer |
EP18185764.0A EP3412916B1 (en) | 2014-03-31 | 2015-02-24 | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor |
CN201580013773.6A CN106104006B (en) | 2014-03-31 | 2015-02-24 | Centrifugal compressor, booster, the manufacturing method of centrifugal compressor and muffler |
KR1020167026159A KR101918377B1 (en) | 2014-03-31 | 2015-02-24 | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor |
EP15774147.1A EP3128184B1 (en) | 2014-03-31 | 2015-02-24 | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor |
CN201810697793.5A CN108799204B (en) | 2014-03-31 | 2015-02-24 | Centrifugal compressor and supercharger |
PCT/JP2015/055240 WO2015151653A1 (en) | 2014-03-31 | 2015-02-24 | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014074071A JP6391970B2 (en) | 2014-03-31 | 2014-03-31 | Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2018023039A Division JP6517386B2 (en) | 2018-02-13 | 2018-02-13 | Centrifugal compressor and supercharger |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2015197053A JP2015197053A (en) | 2015-11-09 |
JP2015197053A5 true JP2015197053A5 (en) | 2017-04-13 |
JP6391970B2 JP6391970B2 (en) | 2018-09-19 |
Family
ID=54239989
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2014074071A Active JP6391970B2 (en) | 2014-03-31 | 2014-03-31 | Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer |
Country Status (5)
Country | Link |
---|---|
EP (2) | EP3128184B1 (en) |
JP (1) | JP6391970B2 (en) |
KR (1) | KR101918377B1 (en) |
CN (2) | CN106104006B (en) |
WO (1) | WO2015151653A1 (en) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015014550A1 (en) * | 2015-11-11 | 2017-05-11 | Man Diesel & Turbo Se | Intake system for an exhaust gas turbocharger and turbocharger |
JP6240251B2 (en) * | 2016-03-30 | 2017-11-29 | 三菱重工業株式会社 | Compressor and supercharger |
DE102016111081A1 (en) * | 2016-06-17 | 2017-12-21 | Man Diesel & Turbo Se | flow machine |
JP6847683B2 (en) * | 2017-01-31 | 2021-03-24 | 三菱重工業株式会社 | Centrifugal compressor and turbocharger |
WO2019087869A1 (en) | 2017-11-01 | 2019-05-09 | 株式会社Ihi | Centrifugal compressor |
CN111279084B (en) * | 2017-11-01 | 2021-04-30 | 株式会社Ihi | Centrifugal compressor |
WO2019087868A1 (en) | 2017-11-01 | 2019-05-09 | 株式会社Ihi | Centrifugal compressor |
US11067098B2 (en) | 2018-02-02 | 2021-07-20 | Carrier Corporation | Silencer for a centrifugal compressor assembly |
JP6879432B2 (en) | 2018-03-30 | 2021-06-02 | 株式会社村田製作所 | CPAP device |
JP2019203446A (en) * | 2018-05-23 | 2019-11-28 | 株式会社オティックス | Compressor housing for turbo charger and manufacturing method of the same |
JP7393095B2 (en) * | 2018-06-07 | 2023-12-06 | トヨタ自動車株式会社 | gas compression equipment |
JP7164346B2 (en) * | 2018-07-24 | 2022-11-01 | 三菱重工マリンマシナリ株式会社 | Rotating machines and turbochargers |
CN112204263A (en) * | 2019-03-06 | 2021-01-08 | 氟技 | Pump case reaches magnetic drive pump including it |
GB201910815D0 (en) * | 2019-07-29 | 2019-09-11 | Cummins Ltd | Bearing housing and method of manufacture |
US11859641B2 (en) * | 2019-11-27 | 2024-01-02 | James E. Petersen, Jr. | Noise abatement for air blowers |
CN115698480A (en) * | 2020-06-04 | 2023-02-03 | 三菱重工船用机械株式会社 | Turbine housing and supercharger |
US11519423B1 (en) * | 2021-11-11 | 2022-12-06 | Progress Rail Locomotive Inc. | Compressor joint |
CN117823463A (en) * | 2023-12-08 | 2024-04-05 | 南京磁谷科技股份有限公司 | High-speed centrifugal compressor air inlet chamber structure, centrifugal compressor and air inlet method |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3635580A (en) * | 1970-02-26 | 1972-01-18 | Westinghouse Electric Corp | Centrifugal refrigerant gas compressor capacity control |
US4181466A (en) * | 1977-03-17 | 1980-01-01 | Wallace Murray Corp. | Centrifugal compressor and cover |
JPS6413299U (en) * | 1987-07-15 | 1989-01-24 | ||
JP4359798B2 (en) | 1999-11-05 | 2009-11-04 | 株式会社Ihi | Exhaust turbine turbocharger |
DE10002581C2 (en) * | 2000-01-21 | 2002-01-17 | Man B & W Diesel Ag | turbocharger |
DE10050931C5 (en) * | 2000-10-13 | 2007-03-29 | Man Diesel Se | Turbomachine with radial impeller |
DE10107807C1 (en) * | 2001-02-20 | 2002-07-25 | Man B & W Diesel Ag | Flow machine with radial compressor wheel, used as a turbosupercharger, has cavity between inner cylinder of spiral casing and casing insertion piece |
CN100395487C (en) * | 2003-07-31 | 2008-06-18 | 松下电器产业株式会社 | Air conditioner |
EP1860284A1 (en) * | 2006-05-23 | 2007-11-28 | ABB Turbo Systems AG | Casings assembling |
CN101506531B (en) * | 2006-08-24 | 2012-07-18 | Abb涡轮系统有限公司 | Fixing mechanism of filter muffler |
JP4648347B2 (en) * | 2007-02-23 | 2011-03-09 | 三菱重工業株式会社 | Hybrid exhaust turbine turbocharger |
WO2010007834A1 (en) * | 2008-07-17 | 2010-01-21 | トヨタ自動車株式会社 | Impact and sound absorbing material and sound absorbing structure |
JP2010127240A (en) * | 2008-11-28 | 2010-06-10 | Mitsubishi Heavy Ind Ltd | Fitting structure of impeller |
JP5230590B2 (en) * | 2009-12-07 | 2013-07-10 | 三菱重工業株式会社 | Exhaust inlet casing of exhaust turbine supercharger |
US20110305554A1 (en) * | 2010-06-14 | 2011-12-15 | Honeywell International Inc. | Light weight vaneless compressor containment design |
DE102010038631B4 (en) * | 2010-07-29 | 2017-07-06 | Man Diesel & Turbo Se | Turbo compressor for an internal combustion engine |
JP6008495B2 (en) * | 2011-12-16 | 2016-10-19 | 三菱重工業株式会社 | Exhaust turbine turbocharger |
CN202483956U (en) * | 2012-01-05 | 2012-10-10 | 黄晓东 | Centrifugal cooling water pump |
-
2014
- 2014-03-31 JP JP2014074071A patent/JP6391970B2/en active Active
-
2015
- 2015-02-24 CN CN201580013773.6A patent/CN106104006B/en active Active
- 2015-02-24 KR KR1020167026159A patent/KR101918377B1/en active IP Right Grant
- 2015-02-24 EP EP15774147.1A patent/EP3128184B1/en active Active
- 2015-02-24 CN CN201810697793.5A patent/CN108799204B/en active Active
- 2015-02-24 EP EP18185764.0A patent/EP3412916B1/en active Active
- 2015-02-24 WO PCT/JP2015/055240 patent/WO2015151653A1/en active Application Filing
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP2015197053A5 (en) | Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer | |
JP6391970B2 (en) | Centrifugal compressor, supercharger, centrifugal compressor manufacturing method, and silencer | |
CN105715308B (en) | Compressor assembly for the explosion of anti-turbocharger | |
EP3324053B1 (en) | Compression device and supercharger | |
US10330102B2 (en) | Centrifugal compressor and turbocharger | |
JP2017180283A5 (en) | ||
WO2015199153A1 (en) | Labyrinth seal device for axial-flow turbine and exhaust gas turbocharger equipped with same | |
CN107002709B (en) | Compressor, supercharger provided with same, and method for adjusting width of discharge port passage of compressor | |
JP2019094899A (en) | Turbine and turbocharger | |
WO2015151844A1 (en) | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor | |
KR101799707B1 (en) | Compressor and supercharger | |
JP6133439B2 (en) | Compressor and turbocharger | |
JP6847683B2 (en) | Centrifugal compressor and turbocharger | |
JP2016145534A (en) | Centrifugal compressor and supercharger with the same | |
JP2016084784A (en) | Centrifugal compressor and supercharger including the same | |
JP6545156B2 (en) | Rotor disc with fluid removal passage to extend spindle bolt life | |
JP6456596B2 (en) | Centrifugal compressor, supercharger, and method of manufacturing centrifugal compressor | |
KR101804742B1 (en) | Intake-air-straightening device and compressor provided with same | |
KR101904679B1 (en) | Centrifugal compressor and supercharger with same | |
JP2017044164A (en) | Centrifugal compressor and turbocharger | |
JP2015197052A5 (en) | ||
JP6541956B2 (en) | Centrifugal compressor and turbocharger equipped with the same | |
JP2018084241A (en) | Centrifugal compressor and supercharger | |
JP2016084785A5 (en) |