JPH07189725A - Lagging cover for turbine housing - Google Patents
Lagging cover for turbine housingInfo
- Publication number
- JPH07189725A JPH07189725A JP33312693A JP33312693A JPH07189725A JP H07189725 A JPH07189725 A JP H07189725A JP 33312693 A JP33312693 A JP 33312693A JP 33312693 A JP33312693 A JP 33312693A JP H07189725 A JPH07189725 A JP H07189725A
- Authority
- JP
- Japan
- Prior art keywords
- turbine housing
- cover body
- cover
- present
- shape
- 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
Landscapes
- Supercharger (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、タービンハウジングラ
ギングカバーに関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a turbine housing lagging cover.
【0002】[0002]
【従来の技術】ターボチャージャーでは、特に高温とな
るタービンハウジングを、カバーで覆うことにより断熱
を行わせる場合がある。2. Description of the Related Art In a turbocharger, a turbine housing, which has a particularly high temperature, is sometimes covered with a cover so as to be insulated.
【0003】図12〜図14は、従来のタービンハウジ
ングラギングカバーを示すものであり、タービンハウジ
ングのスクロール部における周面に合わせてほぼ短冊状
に裁断して耐熱布2で包んだ断熱材1と、前記スクロー
ル部における両端面に合う渦巻状に裁断した耐熱布3を
縫い合わせて立体的なカバー本体4を形成し、各耐熱布
3,3の両端部にベルト5及びバックル6をそれぞれ取
付けて、タービンハウジングにカバー本体4を被せ、各
バックル6に対応するベルト5を通して締め付けること
により、タービンハウジングにカバー本体4を固定して
いた。FIGS. 12 to 14 show a conventional turbine housing lagging cover, in which a heat insulating material 1 is cut into strips and wrapped with a heat resistant cloth 2 in accordance with the peripheral surface of the scroll portion of the turbine housing. , A scroll-shaped heat-resistant cloth 3 that fits both end surfaces of the scroll portion is sewn together to form a three-dimensional cover body 4, and a belt 5 and a buckle 6 are attached to both ends of each heat-resistant cloth 3, 3 respectively. The cover main body 4 is fixed to the turbine housing by covering the turbine housing with the cover main body 4 and tightening the belts 5 corresponding to the respective buckles 6 by tightening.
【0004】[0004]
【発明が解決しようとする課題】しかしながら、上記従
来のタービンハウジングラギングカバーには、以下のよ
うな問題があった。However, the above-mentioned conventional turbine housing lagging cover has the following problems.
【0005】即ち、立体的に形成したカバー本体4は、
タービンハウジングに対する密着性が低く、タービンハ
ウジングの振動により位置ずれを起こし易い。That is, the three-dimensionally formed cover body 4 is
It has low adhesion to the turbine housing and is easily displaced due to vibration of the turbine housing.
【0006】又、立体的なカバー本体4は、製作に手間
が掛かる。Further, the three-dimensional cover body 4 takes time to manufacture.
【0007】本発明は、上述の実情に鑑み、簡単に製作
できて、タービンハウジングに対する密着性を向上し得
るようにしたタービンハウジングラギングカバーを提供
することを目的とするものである。SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and an object of the present invention is to provide a turbine housing lagging cover which can be easily manufactured to improve the adhesion to the turbine housing.
【0008】[0008]
【課題を解決するための手段】本発明は、断熱材と形状
保持層を有する断熱部材を、タービンハウジングのスク
ロール部における周面及び両端面を被覆可能なほぼ短冊
状に形成したカバー本体と、該カバー本体の両端部近傍
に取付けられた針金とを備えたことを特徴とするタービ
ンハウジングラギングカバーにかかるものである。According to the present invention, a heat insulating member having a heat insulating material and a shape retaining layer is formed into a substantially strip-shaped cover body capable of covering the peripheral surface and both end surfaces of a scroll portion of a turbine housing, According to another aspect of the present invention, there is provided a turbine housing lagging cover, the wire being attached to both ends of the cover body.
【0009】[0009]
【作用】本発明の作用は以下の通りである。The operation of the present invention is as follows.
【0010】短冊状をした断熱性のカバー本体でタービ
ンハウジングのスクロール部における周面及び両端面を
被覆し、カバー本体の両端部近傍に取付けられた針金を
結べば、形状保持層がカバー本体をタービンハウジング
に沿った形状に保持させ密着させるので、簡単且つ、密
着性良く、タービンハウジングのスクロール部にカバー
本体が装着される。The strip-shaped heat-insulating cover main body covers the peripheral surface and both end surfaces of the scroll portion of the turbine housing, and if wires attached near both ends of the cover main body are connected, the shape-retaining layer forms the cover main body. The cover body is attached to the scroll portion of the turbine housing easily and with good adhesion because the shape is held along the turbine housing and brought into close contact therewith.
【0011】[0011]
【実施例】以下、本発明の実施例を図面に基いて説明す
る。Embodiments of the present invention will be described below with reference to the drawings.
【0012】図1〜図3は、本発明の第一の実施例であ
る。1 to 3 show a first embodiment of the present invention.
【0013】ガラスクロスやガラスクロスにアルミ箔を
コーティングして成る耐熱布製の外面材7と、グラスウ
ールなどの断熱材8と、前記外面材7と同様の内面材9
と、金網などの形状保持層10とを外側から順に一体化
して成る断熱部材製のカバー本体11を設け、該カバー
本体11をタービンハウジング12のスクロール部13
における周面及び両端面を一度に被覆可能な大きさの短
冊状に形成する。An outer surface material 7 made of a heat-resistant cloth made of glass cloth or glass cloth coated with aluminum foil, a heat insulating material 8 such as glass wool, and an inner surface material 9 similar to the outer surface material 7.
And a shape-maintaining layer 10 such as a wire mesh are sequentially integrated from the outside to provide a cover body 11 made of a heat insulating member, and the cover body 11 is provided with a scroll portion 13 of the turbine housing 12.
The peripheral surface and both end surfaces are formed in a strip shape having a size capable of being covered at once.
【0014】該カバー本体11は、タービンハウジング
12のスクロール部13における排ガス吸入口14に対
応する一端側が広幅となる台形状に形成されており、そ
の一端側に、一端部を折返して縫い付けて成る袋状の針
金通部15が形成されると共に、両側部に、他端側から
一端側の手前まで延びる同様の袋状をした針金通部1
6,17が形成され、各針金通部15〜17に別個に針
金18〜20が通されている。The cover body 11 is formed in a trapezoidal shape in which one end side corresponding to the exhaust gas intake port 14 in the scroll portion 13 of the turbine housing 12 has a wide width, and one end portion thereof is folded back and sewn. The bag-shaped wire passing portion 15 is formed, and the same bag-shaped wire passing portion 1 extending from the other end side to the front side of the one end side is formed on both sides.
6 and 17 are formed, and the wires 18 to 20 are separately passed through the wire passing portions 15 to 17, respectively.
【0015】次に、作動について説明する。Next, the operation will be described.
【0016】カバー本体11をタービンハウジング12
に取付ける場合には、形状保持層10を内側にしてカバ
ー本体11をタービンハウジング12の上に被せ、必要
に応じてカバー本体11をタービンハウジング12に沿
うように押え付けて曲げを与えた後、針金18〜20を
それぞれ強く引絞って、図3に示すように、各針金18
〜20の両端部どうしを結び付ける。The cover body 11 is attached to the turbine housing 12
In the case of attaching the cover body 11 to the turbine housing 12 with the shape-retaining layer 10 inside, the cover body 11 is pressed and bent along the turbine housing 12 if necessary, Firmly squeeze each of the wires 18 to 20, and as shown in FIG.
Tie the ends of ~ 20 together.
【0017】すると、カバー本体11は、針金18が引
絞られた時に、タービンハウジング12に沿った形に変
形して密着し、形状保持層10の形状保持性と、針金1
8〜20の引絞力でタービンハウジング12に密着した
状態に保たれる。Then, when the wire 18 is drawn, the cover body 11 is deformed into a shape along the turbine housing 12 and comes into close contact therewith, so that the shape-retaining property of the shape-retaining layer 10 and the wire 1 are retained.
It is kept in close contact with the turbine housing 12 by a drawing force of 8 to 20.
【0018】このように、カバー本体11がタービンハ
ウジング12に密着されることにより、振動などによっ
て、容易に位置ずれを起こしにくい状態となる。As described above, the cover body 11 is brought into close contact with the turbine housing 12 so that the position is less likely to be displaced due to vibration or the like.
【0019】しかも、短冊型のカバー本体11は製作が
容易である。Moreover, the strip-shaped cover body 11 is easy to manufacture.
【0020】尚、金網などの形状保持層10を設けるこ
とによって、内面材9が直接タービンハウジング12に
接触されるのを防止できると共に、内面材9とタービン
ハウジング12との間に断熱性の空気層を形成すること
ができるという効果も得られる。By providing the shape-retaining layer 10 such as a wire mesh, it is possible to prevent the inner surface member 9 from directly contacting the turbine housing 12, and at the same time, to provide heat insulating air between the inner surface member 9 and the turbine housing 12. The effect that a layer can be formed is also obtained.
【0021】図4・図5は、本発明の第二の実施例であ
り、針金通部16,17間に一本の針金21を通すよう
にした以外は、前記実施例と同様の構成を備えており、
同様の作用・効果を得ることができる。FIGS. 4 and 5 show a second embodiment of the present invention, which has the same construction as the above embodiment except that one wire 21 is inserted between the wire passage portions 16 and 17. Is equipped with
Similar actions and effects can be obtained.
【0022】図6・図7は、本発明の第三の実施例であ
り、針金通部16,17に通した針金19,20の一端
を交差させた後、カバー本体11の一端部に形成した針
金通穴22,23から取出すようにした以外は、前記実
施例と同様の構成を備えており、同様の作用・効果を得
ることができる。FIGS. 6 and 7 show a third embodiment of the present invention, which is formed at one end of the cover body 11 after intersecting one ends of the wires 19 and 20 passed through the wire passing portions 16 and 17. The structure is the same as that of the above-described embodiment except that the wire is taken out from the wire passage holes 22 and 23, and the same action and effect can be obtained.
【0023】図8〜図10は、本発明の第四の実施例で
ある。形状保持層24としてアルミ箔やステンレス箔な
どの金属薄板を用い、カバー本体11の両端部に形成し
た針金通穴25,26間を直接針金27,29で結ぶよ
うにした以外は、前記実施例と同様の構成を備えてお
り、同様の作用・効果を得ることができる。8 to 10 show a fourth embodiment of the present invention. A metal thin plate such as an aluminum foil or a stainless steel foil is used as the shape-retaining layer 24, and the wire through holes 25 and 26 formed at both ends of the cover body 11 are directly connected by the wires 27 and 29. It has the same configuration as the above and can obtain the same operation and effect.
【0024】又、本実施例によれば、金網よりも密着性
の良い、アルミ箔やステンレス箔などの金属薄板を用い
たので、カバー本体11の両端部どうしを直接針金2
7,29で結んでも位置ずれを充分防止することが可能
となる。Further, according to the present embodiment, since the metal thin plate such as aluminum foil or stainless steel foil, which has better adhesion than the wire mesh, is used, both ends of the cover body 11 are directly connected to the wire 2.
Even if they are tied with 7, 29, it is possible to sufficiently prevent the displacement.
【0025】図11は、本発明の第五の実施例であり、
外面材7の外側に金網層28を設けて、外面材7に破れ
や損傷が生じた場合でも、破れなどの拡大を防止し得る
ようにした以外は、前記実施例と同様の構成を備えてお
り、同様の作用・効果を得ることができる。FIG. 11 shows the fifth embodiment of the present invention.
A wire mesh layer 28 is provided on the outer side of the outer surface material 7, and even if the outer surface material 7 is torn or damaged, it is possible to prevent expansion such as tearing and the like, and is provided with the same configuration as in the above embodiment. Therefore, the same action and effect can be obtained.
【0026】尚、本発明は、上述の実施例にのみ限定さ
れるものではなく、本発明の要旨を逸脱しない範囲内に
おいて種々変更を加え得ることは勿論である。The present invention is not limited to the above-mentioned embodiments, and it goes without saying that various modifications can be made without departing from the gist of the present invention.
【0027】[0027]
【発明の効果】以上説明したように、本発明のタービン
ハウジングラギングカバーによれば、簡単に製作でき
て、タービンハウジングに対する密着性を向上し、位置
ずれをなくすことができるという優れた効果を奏し得
る。As explained above, according to the turbine housing lagging cover of the present invention, the turbine housing lagging cover can be easily manufactured, the adhesion to the turbine housing can be improved, and the displacement can be eliminated. obtain.
【図1】本発明の第一の実施例の平面図である。FIG. 1 is a plan view of a first embodiment of the present invention.
【図2】図1の断面図である。FIG. 2 is a cross-sectional view of FIG.
【図3】図1の取付図である。3 is a mounting view of FIG. 1. FIG.
【図4】本発明の第二の実施例の平面図である。FIG. 4 is a plan view of the second embodiment of the present invention.
【図5】図4の取付図である。5 is a mounting view of FIG. 4. FIG.
【図6】本発明の第三の実施例の平面図である。FIG. 6 is a plan view of a third embodiment of the present invention.
【図7】図6の取付図である。FIG. 7 is a mounting view of FIG.
【図8】本発明の第四の実施例の平面図である。FIG. 8 is a plan view of the fourth embodiment of the present invention.
【図9】図8の断面図である。9 is a cross-sectional view of FIG.
【図10】図8の取付図である。10 is a mounting view of FIG. 8. FIG.
【図11】本発明の第五の実施例の断面図である。FIG. 11 is a sectional view of a fifth embodiment of the present invention.
【図12】従来例の部品展開図である。FIG. 12 is a component development view of a conventional example.
【図13】図12の組立断面図である。FIG. 13 is an assembled sectional view of FIG.
【図14】図12の組立斜視図である。14 is an assembled perspective view of FIG. 12. FIG.
8 断熱材 10,24 形状保持層 11 カバー本体 12 タービンハウジング 13 スクロール部 18〜21,27 針金 8 Heat Insulating Material 10,24 Shape Retaining Layer 11 Cover Main Body 12 Turbine Housing 13 Scroll Part 18-21,27 Wire
Claims (1)
を、タービンハウジングのスクロール部における周面及
び両端面を被覆可能なほぼ短冊状に形成したカバー本体
と、該カバー本体の両端部近傍に取付けられた針金とを
備えたことを特徴とするタービンハウジングラギングカ
バー。1. A cover main body in which a heat insulating member having a heat insulating material and a shape-retaining layer is formed in a substantially strip shape capable of covering the peripheral surface and both end surfaces of a scroll portion of a turbine housing, and in the vicinity of both end portions of the cover main body. A turbine housing lagging cover, comprising: an attached wire.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP33312693A JP3296061B2 (en) | 1993-12-27 | 1993-12-27 | Turbine housing lagging cover |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP33312693A JP3296061B2 (en) | 1993-12-27 | 1993-12-27 | Turbine housing lagging cover |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH07189725A true JPH07189725A (en) | 1995-07-28 |
JP3296061B2 JP3296061B2 (en) | 2002-06-24 |
Family
ID=18262588
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP33312693A Expired - Lifetime JP3296061B2 (en) | 1993-12-27 | 1993-12-27 | Turbine housing lagging cover |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP3296061B2 (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008202467A (en) * | 2007-02-19 | 2008-09-04 | Ihi Corp | Supercharger |
JP2008248773A (en) * | 2007-03-30 | 2008-10-16 | Ihi Corp | Heat insulation cover of supercharger |
JP2009174326A (en) * | 2008-01-21 | 2009-08-06 | Ihi Corp | Insulation cover of supercharger |
JP2010096114A (en) * | 2008-10-17 | 2010-04-30 | Ihi Corp | Heat insulating cover |
JP2012102743A (en) * | 2012-01-19 | 2012-05-31 | Ihi Corp | Heat insulation cover of supercharger |
JP2012102744A (en) * | 2012-01-19 | 2012-05-31 | Ihi Corp | Heat insulation cover of supercharger |
JP2012211544A (en) * | 2011-03-31 | 2012-11-01 | Mitsubishi Heavy Ind Ltd | Sheet-metal turbine housing |
WO2014186129A1 (en) * | 2013-05-14 | 2014-11-20 | Borgwarner Inc. | Turbine housing of an exhaust-gas turbocharger |
JP2016014353A (en) * | 2014-07-02 | 2016-01-28 | 株式会社Ihi | Turbocharger heat insulation cover |
WO2023026581A1 (en) * | 2021-08-26 | 2023-03-02 | 株式会社Ihi | Supercharger |
-
1993
- 1993-12-27 JP JP33312693A patent/JP3296061B2/en not_active Expired - Lifetime
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008202467A (en) * | 2007-02-19 | 2008-09-04 | Ihi Corp | Supercharger |
JP2008248773A (en) * | 2007-03-30 | 2008-10-16 | Ihi Corp | Heat insulation cover of supercharger |
JP2009174326A (en) * | 2008-01-21 | 2009-08-06 | Ihi Corp | Insulation cover of supercharger |
JP2010096114A (en) * | 2008-10-17 | 2010-04-30 | Ihi Corp | Heat insulating cover |
JP2012211544A (en) * | 2011-03-31 | 2012-11-01 | Mitsubishi Heavy Ind Ltd | Sheet-metal turbine housing |
JP2012102743A (en) * | 2012-01-19 | 2012-05-31 | Ihi Corp | Heat insulation cover of supercharger |
JP2012102744A (en) * | 2012-01-19 | 2012-05-31 | Ihi Corp | Heat insulation cover of supercharger |
WO2014186129A1 (en) * | 2013-05-14 | 2014-11-20 | Borgwarner Inc. | Turbine housing of an exhaust-gas turbocharger |
JP2016518553A (en) * | 2013-05-14 | 2016-06-23 | ボーグワーナー インコーポレーテッド | Turbine housing of exhaust gas turbocharger |
US9841033B2 (en) | 2013-05-14 | 2017-12-12 | Borgwarner Inc. | Exhaust gas turbocharger having an internally insulated turbine volute |
JP2016014353A (en) * | 2014-07-02 | 2016-01-28 | 株式会社Ihi | Turbocharger heat insulation cover |
WO2023026581A1 (en) * | 2021-08-26 | 2023-03-02 | 株式会社Ihi | Supercharger |
Also Published As
Publication number | Publication date |
---|---|
JP3296061B2 (en) | 2002-06-24 |
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