JP2015140748A - turbine housing - Google Patents

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JP2015140748A
JP2015140748A JP2014014745A JP2014014745A JP2015140748A JP 2015140748 A JP2015140748 A JP 2015140748A JP 2014014745 A JP2014014745 A JP 2014014745A JP 2014014745 A JP2014014745 A JP 2014014745A JP 2015140748 A JP2015140748 A JP 2015140748A
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housing
turbine
inner housing
inner shell
fluid
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克己 八木
Katsumi Yagi
克己 八木
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Sango Co Ltd
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Sango Co Ltd
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Abstract

PROBLEM TO BE SOLVED: To provide a turbine housing that can reduce heat stress due to a temperature difference between an inner housing and an outer housing in a turbine housing that includes the inner housing and the outer housing where a space is defined between the inner housing and the outer housing.SOLUTION: The turbine housing 1 includes the inner housing 3 and the outer housing 2 where the space 10 is defined between the inner housing 3 and the outer housing 2. In the turbine housing 1, the inner housing 3 is constituted of two inner shell members 3a, 3b and a partition member 3c provided between both inner shell members 3a, 3b, and a periphery 3d of the inner housing 3 is not coupled to the outer housing 2.

Description

本発明は、ターボ過給機等のタービンハウジングに関する。   The present invention relates to a turbine housing such as a turbocharger.

ターボ過給機のタービンハウジングとして、鋳造製のものが一般的に使用されている。しかし、鋳造時の湯流れを考慮する必要があるため、肉厚を一定以下とすることができないため、軽量化や、熱容量の点において限界がある。   As a turbine housing for a turbocharger, a cast housing is generally used. However, since it is necessary to consider the hot water flow at the time of casting, the thickness cannot be reduced below a certain level, so there is a limit in terms of weight reduction and heat capacity.

そのため、近年、鋼板のプレス成形品を用いてタービンハウジングを製作することが提案されている(例えば、特許文献1参照)。   Therefore, in recent years, it has been proposed to manufacture a turbine housing using a press-formed product of a steel plate (see, for example, Patent Document 1).

特許第4512058号Japanese Patent No. 4512058

前記特許文献1記載のタービンハウジングは、内側ハウジングと外側ハウジングを有し、内側ハウジングと外側ハウジングとの間に隙間を形成し、内側ハウジングは2枚の内殻部材を有し、外側ハウジングは2枚の外殻部材を有し、2枚の外殻部材の外周部間を、連結部材の端部を介して接合するとともに、2枚の外殻部材の外周部間を、前記連結部材を介して接合したものである。すなわち、内側ハウジングと外側ハウジングの外周部は連結部材により連結されている。   The turbine housing described in Patent Document 1 has an inner housing and an outer housing, a gap is formed between the inner housing and the outer housing, the inner housing has two inner shell members, and the outer housing has 2 The outer peripheral members of the two outer shell members are joined via the end portions of the connecting members, and the outer peripheral portions of the two outer shell members are joined via the connecting members. Are joined together. That is, the outer peripheral part of the inner housing and the outer housing is connected by the connecting member.

内側ハウジングには排気ガスが流通するために高温となるが、外側ハウジングは内側ハウジングと隙間を設けて配設されているために、内側ハウジングとの間に温度差が生じる。その温度差による熱応力が連結部材に作用し耐久性が損なわれる虞がある。   Since the exhaust gas flows through the inner housing, the temperature becomes high. However, since the outer housing is disposed with a gap from the inner housing, a temperature difference is generated between the inner housing and the inner housing. There is a risk that the thermal stress due to the temperature difference acts on the connecting member and the durability is impaired.

そこで、本発明は、上記問題点を解決したタービンハウジングを提供することを目的とするものである。   Accordingly, an object of the present invention is to provide a turbine housing that solves the above problems.

前記の課題を解決するために、請求項1記載の発明は、内側ハウジングと外側ハウジングを有し、前記内側ハウジングと外側ハウジングとの間に空間を設けたタービンハウジングにおいて、
前記内側ハウジングは、2枚の内殻部材と、両内殻部材間に設けた1枚の仕切部材で構成され、
前記内側ハウジングの外周部と、外側ハウジングとは連結しないことを特徴とするものである。
In order to solve the above-mentioned problem, the invention according to claim 1 is a turbine housing having an inner housing and an outer housing, and a space is provided between the inner housing and the outer housing.
The inner housing is composed of two inner shell members and one partition member provided between the inner shell members,
The outer peripheral portion of the inner housing and the outer housing are not connected.

請求項2記載の発明は、請求項1記載の発明において、内側ハウジング内に流体を導入する入口部と、前記流体が排出される出口部を有し、前記内殻部材の内周面の一部と仕切部材の一部を当接することにより舌部を形成し、該舌部により、内側ハウジング内で旋回した流体と入口部付近の流体とが合流することを抑制するようにしたことを特徴とするものである。   According to a second aspect of the present invention, in the first aspect of the present invention, the inner shell member has an inlet portion for introducing a fluid into the inner housing and an outlet portion for discharging the fluid. A tongue is formed by abutting a part of the partition and the partition member, and the tongue prevents the fluid swirling in the inner housing and the fluid in the vicinity of the inlet from being merged. It is what.

本発明によれば、内側ハウジングを、2枚の内殻部材と、両内殻部材間に設けた1枚の仕切部材で構成し、内側ハウジングと外側ハウジングとの間に空間を設け、かつ、内殻部材の外周部と外側ハウジングとは連結しないことにより、内側ハウジングと外側ハウジングの温度差による熱応力を軽減でき、従来技術のものよりも耐久性を高めることができる。   According to the present invention, the inner housing is constituted by two inner shell members and one partition member provided between the inner shell members, a space is provided between the inner housing and the outer housing, and By not connecting the outer peripheral portion of the inner shell member and the outer housing, the thermal stress due to the temperature difference between the inner housing and the outer housing can be reduced, and the durability can be improved as compared with the conventional one.

本発明の実施例に用いるタービンハウジングの正面図。The front view of the turbine housing used for the Example of this invention. 図1の左側面図。The left view of FIG. 図1の右側面図。The right view of FIG. 図1の上面図。The top view of FIG. 図1の下面図。The bottom view of FIG. 図1の縦端面図。FIG. 2 is a vertical end view of FIG. 1. 図4の横端面図。FIG. 5 is a lateral end view of FIG. 4. 本発明の実施例に用いる内側ハウジングの斜視図。The perspective view of the inner side housing used for the Example of this invention. 本発明の実施例に用いる内側ハウジングの分解斜視図。The disassembled perspective view of the inner side housing used for the Example of this invention. 本発明の実施例のタービンハウジングの分解斜視図。The disassembled perspective view of the turbine housing of the Example of this invention.

本発明を実施するための形態を図に示す実施例に基づいて説明する。
図1は、本実施例のタービンハウジング1の正面図、図2は図1の左側面図、図3は図1の右側面図である。なお、図面の一部においては、曲面形状がわかるように、稜線を記載した。
A mode for carrying out the present invention will be described based on an embodiment shown in the drawings.
1 is a front view of the turbine housing 1 of the present embodiment, FIG. 2 is a left side view of FIG. 1, and FIG. 3 is a right side view of FIG. In some of the drawings, ridge lines are shown so that the curved surface shape can be seen.

タービンハウジング1は、車両用ターボ過給機に用いられるタービンハウジングであり、図示しないエンジンから流入した流体である排気ガスが、入口11からタービンハウジング1内に導入され、タービンハウジング1内を通り、出口12から排出されるとともに、この排気ガスの流れにより、タービンハウジング1の中心部に設けられた貫通孔20,21内のタービンホイール(図示せず)が回転駆動されるようになっている。また、このタービンホイールの回転によりコンプレッサホイールが回転駆動され、エンジンへ空気が過給されるようになっている。   The turbine housing 1 is a turbine housing used in a turbocharger for a vehicle. Exhaust gas, which is a fluid flowing from an engine (not shown), is introduced into the turbine housing 1 from an inlet 11 and passes through the turbine housing 1. While being discharged from the outlet 12, a turbine wheel (not shown) in the through holes 20 and 21 provided in the central portion of the turbine housing 1 is rotationally driven by the flow of the exhaust gas. In addition, the compressor wheel is driven to rotate by the rotation of the turbine wheel, and air is supercharged to the engine.

タービンハウジング1は、外側ハウジング2と内側ハウジング3と入口部材4と出口部材5を有している。   The turbine housing 1 includes an outer housing 2, an inner housing 3, an inlet member 4, and an outlet member 5.

外側ハウジング2は、第1外殻部材2aと第2外殻部材2bの2枚の部材で構成されている。第1外殻部材2aと第2外殻部材2bは、金属製の板材を、プレス成形することにより作製される。用いられる板材としては、耐食性、耐熱性に優れたものが好ましい。外側ハウジング2の中心部には、貫通孔20が形成されている。   The outer housing 2 is composed of two members, a first outer shell member 2a and a second outer shell member 2b. The first outer shell member 2a and the second outer shell member 2b are produced by press-molding a metal plate material. As a board | plate material used, the thing excellent in corrosion resistance and heat resistance is preferable. A through hole 20 is formed at the center of the outer housing 2.

第1外殻部材2aと第2外殻部材2bは、夫々外側方向に膨出し、内側に内側ハウジング3が配設できるようになっている。第1外殻部材2aと第2外殻部材2bは、外周部において、入口11以外の全周に亘って溶接等により接合されている。   The first outer shell member 2a and the second outer shell member 2b bulge outward, and the inner housing 3 can be disposed on the inner side. The first outer shell member 2 a and the second outer shell member 2 b are joined by welding or the like over the entire circumference except for the inlet 11 at the outer peripheral portion.

外側ハウジング2内には、内側ハウジング3が配設され、外側ハウジング2と内側ハウジング3間には空間10が形成されている。   An inner housing 3 is disposed in the outer housing 2, and a space 10 is formed between the outer housing 2 and the inner housing 3.

内側ハウジング3は、第1内殻部材3aと第2内殻部材3bと仕切部材3cの3枚の部材で構成されている。第1内殻部材3aと第2内殻部材3bと仕切部材3cは、金属製の板材を、プレス成形することにより作製される。用いられる板材としては、耐食性、耐熱性に優れたものが好ましい。仕切部材3cの板厚は、内殻部材3a,3bの板厚と同一かそれよりも薄くすることが好ましい。   The inner housing 3 is composed of three members: a first inner shell member 3a, a second inner shell member 3b, and a partition member 3c. The 1st inner shell member 3a, the 2nd inner shell member 3b, and the partition member 3c are produced by press-molding a metal plate material. As a board | plate material used, the thing excellent in corrosion resistance and heat resistance is preferable. The plate thickness of the partition member 3c is preferably equal to or thinner than the plate thickness of the inner shell members 3a and 3b.

仕切部材3cは、図6〜8に示すように、入口11以外の外周部において周方向全体に亘って、第1内殻部材3aと第2内殻部材3bにより挟持されている。その挟持部において、内殻部材3a,3bと仕切部材3cは、溶接等により接合されている。   As shown in FIGS. 6 to 8, the partition member 3 c is sandwiched between the first inner shell member 3 a and the second inner shell member 3 b over the entire circumferential direction in the outer peripheral portion other than the inlet 11. In the clamping portion, the inner shell members 3a and 3b and the partition member 3c are joined by welding or the like.

内側ハウジング3の外周部3d、すなわち、内殻部材3a,3b及び仕切部材3cの外周部3dと、外側ハウジング2とは接合等により連結されず、空間10が介在している。内側ハウジング3の中心部には、表裏方向(図2の左右方向)を貫通する貫通孔21が形成されている。   The outer peripheral portion 3d of the inner housing 3, that is, the outer peripheral portions 3d of the inner shell members 3a and 3b and the partition member 3c, and the outer housing 2 are not connected by bonding or the like, and the space 10 is interposed. A through hole 21 is formed in the central portion of the inner housing 3 so as to penetrate the front and back direction (left and right direction in FIG. 2).

第1内殻部材3aの内周面と仕切部材3cの一方の面により第1流路13が形成され、第2内殻部材3bの内周面と仕切部材3cの他方の面により第2流路14が形成されている。2つの流路13,14は、「の」字状に形成され、周方向の一部が開口して入口11と連通し、また、内周部の貫通孔21側が開口して出口12と連通している。   The first flow path 13 is formed by the inner peripheral surface of the first inner shell member 3a and one surface of the partition member 3c, and the second flow is formed by the inner peripheral surface of the second inner shell member 3b and the other surface of the partition member 3c. A path 14 is formed. The two flow paths 13, 14 are formed in a “-” shape, a part in the circumferential direction is opened and communicated with the inlet 11, and the through hole 21 side of the inner circumferential part is opened and communicated with the outlet 12. doing.

入口11から流路13,14内に流入した流体は周方向に旋回した後に、内周側の開口から出口12に排出されるようになっている。また、2つの流路13,14は、タービンホイール近傍で合流するようになっている。   The fluid that has flowed into the flow paths 13 and 14 from the inlet 11 is swung in the circumferential direction, and then discharged from the opening on the inner peripheral side to the outlet 12. Moreover, the two flow paths 13 and 14 are merged in the vicinity of the turbine wheel.

流路13,14は、内周側の開口部近傍、すなわち、タービンホイール近傍の断面積が狭くなるように形成されて流体の流速が増加するようになっている。   The flow paths 13 and 14 are formed so that the cross-sectional area in the vicinity of the opening on the inner peripheral side, that is, in the vicinity of the turbine wheel is narrowed, and the flow velocity of the fluid is increased.

入口11部の内周側には、第1内殻部材3aの内周面の一部と仕切部材3cの一方の面の一部、及び、第2内殻部材3bの内周面の一部と仕切部材3cの他方の面の一部が夫々当接するとともに、溶接等で接合されて舌部16が形成されている。この舌部16は入口11から流入したばかりの流体と、流路13,14内を旋回した流体とが合流することを抑制し、流体が出口12からスムーズに排出されるようにしている。   On the inner peripheral side of the inlet 11 portion, a part of the inner peripheral surface of the first inner shell member 3a, a part of one surface of the partition member 3c, and a part of the inner peripheral surface of the second inner shell member 3b And part of the other surface of the partition member 3c are in contact with each other and joined by welding or the like to form the tongue portion 16. The tongue portion 16 prevents the fluid just flowing in from the inlet 11 and the fluid swirled in the flow paths 13 and 14 from joining together, so that the fluid is smoothly discharged from the outlet 12.

内側ハウジング3の入口11側開口部には、フランジ状に形成された入口部材4が固設されている。この入口部材4には、図2に示すように、2つの開口部4aが上下に形成され、この開口部4aが入口11を構成している。   An inlet member 4 formed in a flange shape is fixed to the opening portion on the inlet 11 side of the inner housing 3. As shown in FIG. 2, the inlet member 4 has two openings 4 a formed vertically, and the opening 4 a constitutes the inlet 11.

出口部材5は、環状部材5aと出口フランジ5bで構成され、第2外殻部材2bの中心部の貫通孔20の開口部には環状部材5aが挿通され、この環状部材5aは第2外殻部材2bに対して溶接等により接合されている。また、環状部材5aの内側端部は、第2内殻部材3bの内周側に形成された凸部22に対して摺動可能に嵌合している。また、環状部材5aの外側端部には出口フランジ5bが固設され、出口12を形成している。   The outlet member 5 includes an annular member 5a and an outlet flange 5b, and the annular member 5a is inserted into the opening of the through hole 20 at the center of the second outer shell member 2b. The annular member 5a is the second outer shell. It is joined to the member 2b by welding or the like. The inner end of the annular member 5a is slidably fitted to a convex portion 22 formed on the inner peripheral side of the second inner shell member 3b. An outlet flange 5b is fixed to the outer end of the annular member 5a to form an outlet 12.

第1内殻部材3aの貫通穴21には取付フランジ25が固設され、取付フランジ25内にはタービンホイール等が収納されている。   A mounting flange 25 is fixed in the through hole 21 of the first inner shell member 3a, and a turbine wheel or the like is accommodated in the mounting flange 25.

このように、タービンハウジング1は、内部に2つの流路13,14が形成されたツインスクロール型のタービンハウジングである。   As described above, the turbine housing 1 is a twin scroll type turbine housing in which the two flow paths 13 and 14 are formed.

以上の構成により、外側ハウジング2は、内側ハウジング3を保護し、タービンハウジング1の剛性を高めている。   With the above configuration, the outer housing 2 protects the inner housing 3 and increases the rigidity of the turbine housing 1.

外側ハウジング2と内側ハウジング3との間に形成した空間10を設け、かつ、内側ハウジング3の外周部を外側ハウジング2と連結しないようにしたことにより、内側ハウジング3の熱が外側ハウジング2に伝わりにくくなり、断熱効果を有し、排気ガスのエネルギーを効率よく、タービンホイールの回転運動に変換することができ、過給機の効率を高めることができる。また、内側ハウジング3と外側ハウジング2の温度差による膨張差・熱応力を従来技術のものよりも軽減できるため、タービンハウジング1の耐久性を従来技術のものよりも高くすることができる。   By providing the space 10 formed between the outer housing 2 and the inner housing 3 and not connecting the outer peripheral portion of the inner housing 3 to the outer housing 2, the heat of the inner housing 3 is transmitted to the outer housing 2. It becomes difficult, has a heat insulation effect, can efficiently convert the energy of the exhaust gas into the rotational motion of the turbine wheel, and can increase the efficiency of the supercharger. Further, since the difference in expansion and thermal stress due to the temperature difference between the inner housing 3 and the outer housing 2 can be reduced as compared with the prior art, the durability of the turbine housing 1 can be made higher than that of the prior art.

また、外側ハウジング2を、プレス成形で作製した外殻部材2a,2bで構成し、内側ハウジング3を、プレス成形で作製した内殻部材3a,3bと仕切部材3cで構成したことにより、タービンハウジング1の熱容量を低くすることができ、冷間始動時の排気ガス温度の上昇を早め、排気ガス浄化性能を向上させ、排気ガス浄化触媒の量を減らすことが出来る。   Further, the outer housing 2 is constituted by outer shell members 2a and 2b produced by press molding, and the inner housing 3 is constituted by inner shell members 3a and 3b and partition members 3c produced by press molding, whereby a turbine housing is obtained. 1 can be reduced, the temperature of the exhaust gas during the cold start can be increased, the exhaust gas purification performance can be improved, and the amount of the exhaust gas purification catalyst can be reduced.

なお、外側ハウジング2を、プレス成形で作製した外殻部材2a,2bで構成し、内側ハウジング3を、プレス成形で作製した内殻部材3a,3bと仕切部材3cで構成するとともに、内側ハウジング2と外側ハウジング3との間に空間10を設け、内側ハウジング2の外周部3dと外側ハウジング3とを連結しなければ、外殻部材2a,2b、内殻部材3a,3b、仕切部材3cは、図に示した形状に限定されること無く任意の形状とすることができる。   The outer housing 2 is constituted by outer shell members 2a and 2b produced by press molding, and the inner housing 3 is constituted by inner shell members 3a and 3b and a partition member 3c produced by press molding. If the space 10 is provided between the outer housing 3 and the outer peripheral portion 3d of the inner housing 2 and the outer housing 3 are not connected, the outer shell members 2a and 2b, the inner shell members 3a and 3b, and the partition member 3c are Any shape can be used without being limited to the shape shown in the figure.

1 タービンハウジング
2 外側ハウジング
3 内側ハウジング
3a,3b 内殻部材
3c 仕切部材
10 空間
16 舌部
DESCRIPTION OF SYMBOLS 1 Turbine housing 2 Outer housing 3 Inner housing 3a, 3b Inner shell member 3c Partition member 10 Space 16 Tongue

Claims (2)

内側ハウジングと外側ハウジングを有し、前記内側ハウジングと外側ハウジングとの間に空間を設けたタービンハウジングにおいて、
前記内側ハウジングは、2枚の内殻部材と、両内殻部材間に設けた1枚の仕切部材で構成され、
前記内側ハウジングの外周部と、外側ハウジングとは連結しないことを特徴とするタービンハウジング。
In a turbine housing having an inner housing and an outer housing, and providing a space between the inner housing and the outer housing,
The inner housing is composed of two inner shell members and one partition member provided between the inner shell members,
A turbine housing characterized in that the outer peripheral portion of the inner housing is not connected to the outer housing.
内側ハウジング内に流体を導入する入口部と、前記流体が排出される出口部を有し、前記内殻部材の内周面の一部と仕切部材の一部を当接することにより舌部を形成し、該舌部により、内側ハウジング内で旋回した流体と入口部付近の流体とが合流することを抑制するようにしたことを特徴とする請求項1記載のタービンハウジング。
It has an inlet for introducing fluid into the inner housing and an outlet for discharging the fluid, and a tongue is formed by contacting a part of the inner peripheral surface of the inner shell member and a part of the partition member. The turbine housing according to claim 1, wherein the tongue portion prevents the fluid swirled in the inner housing from confluence with the fluid in the vicinity of the inlet portion.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020159221A (en) * 2019-03-25 2020-10-01 株式会社豊田自動織機 Turbocharger

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1357278A2 (en) * 2002-04-25 2003-10-29 Benteler Automobiltechnik GmbH & Co. KG Exhaust gas turbine for a turbocharger
JP2006161574A (en) * 2004-12-02 2006-06-22 Toyota Motor Corp Turbine housing for turbocharger
JP2007002791A (en) * 2005-06-24 2007-01-11 Toyota Motor Corp Turbine housing
JP4512058B2 (en) * 2006-04-04 2010-07-28 トヨタ自動車株式会社 Turbine housing
WO2012105004A1 (en) * 2011-02-02 2012-08-09 三菱重工業株式会社 Sheet metal turbine housing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1357278A2 (en) * 2002-04-25 2003-10-29 Benteler Automobiltechnik GmbH & Co. KG Exhaust gas turbine for a turbocharger
JP2006161574A (en) * 2004-12-02 2006-06-22 Toyota Motor Corp Turbine housing for turbocharger
JP2007002791A (en) * 2005-06-24 2007-01-11 Toyota Motor Corp Turbine housing
JP4512058B2 (en) * 2006-04-04 2010-07-28 トヨタ自動車株式会社 Turbine housing
WO2012105004A1 (en) * 2011-02-02 2012-08-09 三菱重工業株式会社 Sheet metal turbine housing

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020159221A (en) * 2019-03-25 2020-10-01 株式会社豊田自動織機 Turbocharger
JP7103286B2 (en) 2019-03-25 2022-07-20 株式会社豊田自動織機 Turbocharger
DE102020107894B4 (en) 2019-03-25 2023-05-25 Kabushiki Kaisha Toyota Jidoshokki turbocharger

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