JPH06185371A - Variable capacity supercharger - Google Patents

Variable capacity supercharger

Info

Publication number
JPH06185371A
JPH06185371A JP4354881A JP35488192A JPH06185371A JP H06185371 A JPH06185371 A JP H06185371A JP 4354881 A JP4354881 A JP 4354881A JP 35488192 A JP35488192 A JP 35488192A JP H06185371 A JPH06185371 A JP H06185371A
Authority
JP
Japan
Prior art keywords
connecting plate
pin
nozzle vanes
plate
nozzle
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
Application number
JP4354881A
Other languages
Japanese (ja)
Other versions
JP3239499B2 (en
Inventor
Hiroshi Furukawa
弘 古川
Yoshinori Isobe
好則 磯部
Takeshi Mitsubori
健 三堀
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Corp
Original Assignee
IHI Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by IHI Corp filed Critical IHI Corp
Priority to JP35488192A priority Critical patent/JP3239499B2/en
Publication of JPH06185371A publication Critical patent/JPH06185371A/en
Application granted granted Critical
Publication of JP3239499B2 publication Critical patent/JP3239499B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Supercharger (AREA)

Abstract

PURPOSE:To prevent the wear of the connecting parts of a connecting plate for adjusting the throat between nozzle vanes and pins. CONSTITUTION:A plurality of nozzle vanes 12 are arranged on the outer circumference of a turbine disc. One end part of a link plate 14 is connected to each nozzle vane 12. The space between the other end parts of adjacent link plates 14 is connected by a connecting plate 15 by means of pins 16. It is so contrived that the throat S between the nozzle vanes 12 can be regulated by moving the connecting plates 15 in the circumferential direction. The connecting plate 15 is made up of ring-shaped parts 20 at both ends where the pin holes 22 are provided, and an arm part 21 arranged between both the ring-shaped parts 20. The arm part 21 is sloped with regard to the straight line connecting the centers of the pin holes.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は導入されるガスの流量を
調整できるようにした可変容量型過給機に関するもので
ある。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a variable capacity supercharger capable of adjusting the flow rate of introduced gas.

【0002】[0002]

【従来の技術】複数のノズルベーンを組み込んでタービ
ンへ導入されるガス流量を、該ノズルベーン間のスロー
トを変えることにより調整するようにしたタービン車室
を有する可変容量型過給機は、従来より採用されてお
り、その一例を示すと、図6及び図7に示す構成のもの
がある。すなわち、タービン車室1とブロワ車室2とを
軸受車室3を介して一体構造とし、タービン車室1内の
タービン翼車4とブロワ車室2内のブロワ扇車5とを、
軸受車室3内に軸受7で回転自在に支承されたタービン
軸6にて連結し、タービン翼車4をガス流により回転さ
せることによりブロワ扇車5を回転させて空気を吸収し
圧縮して吐出させるようにし、更に、上記タービン翼車
4を回転させるガスを、ガス入口8から導入し、ガスの
通路となるようにタービンシュラウド9の外周に設けた
スクロール10を通してタービン翼車4に導くようにし
てある構成において、上記スクロール10部からタービ
ン翼車4の外周部に至る間のガス流路11部に、円周方
向に複数のノズルベーン12を配列し、該各ノズルベー
ン12を、タービンシュラウド9を貫通させた軸13の
内端に各々固定する。一方、上記各軸13の外端には、
各々リンク14板の一端部を取り付け、上記各隣り合う
リンク板14の他端部間を、タービンシュラウド9の外
側に配置したチェーンリンクの如き連結板15にて周方
向にピン16で連結し、図示しないアクチュエータによ
りレバー19、軸17、アーム18を介して連結板15
を周方向へ移動させることによりリンク板14、軸13
の回転を介し各ノズルベーン12の開閉角度が変えられ
るようにし、各ノズルベーン12の開閉角度をコントロ
ールすることで各ノズルベーン12間のスロートSを広
狭調整することによりガスの流量を大流量から小流量に
変えることができるようにした構成としてある。
2. Description of the Related Art A variable capacity supercharger having a turbine casing, which has a plurality of nozzle vanes incorporated therein and adjusts a gas flow rate introduced into a turbine by changing a throat between the nozzle vanes, has been conventionally adopted. However, there is a configuration shown in FIGS. 6 and 7 as an example. That is, the turbine casing 1 and the blower casing 2 are integrated with each other through the bearing casing 3, and the turbine impeller 4 inside the turbine casing 1 and the blower fan 5 inside the blower casing 2 are
A turbine shaft 6 rotatably supported in a bearing casing 3 by a bearing 7 is connected, and a turbine impeller 4 is rotated by a gas flow to rotate a blower fan 5 to absorb and compress air. The gas for discharging and further for rotating the turbine impeller 4 is introduced from the gas inlet 8 and guided to the turbine impeller 4 through the scroll 10 provided on the outer circumference of the turbine shroud 9 so as to form a gas passage. In the configuration described above, a plurality of nozzle vanes 12 are arranged in the circumferential direction in the gas flow passage 11 portion between the scroll 10 portion and the outer peripheral portion of the turbine impeller 4, and each nozzle vane 12 is connected to the turbine shroud 9 Are fixed to the inner ends of the shafts 13 which are penetrated. On the other hand, at the outer end of each shaft 13,
One end of each of the link 14 plates is attached, and the other end of each of the adjacent link plates 14 is connected by a pin 16 in the circumferential direction by a connecting plate 15 such as a chain link arranged outside the turbine shroud 9, Connecting plate 15 via lever 19, shaft 17, and arm 18 by an actuator (not shown)
By moving the link in the circumferential direction, the link plate 14, the shaft 13
The opening / closing angle of each nozzle vane 12 can be changed by rotating the nozzle vane 12, and the opening / closing angle of each nozzle vane 12 is controlled to adjust the throat S between the nozzle vanes 12 to a wide range or a small flow rate. It is designed so that it can be changed.

【0003】[0003]

【発明が解決しようとする課題】ところが、上記従来の
可変容量型過給機の場合、エンジンからの排気ガスによ
り各ノズルベーン12間に脈動圧が発生し、この脈動圧
がノズルベーン12からリンク板14、ピン16を介し
て連結板15に伝わるため、連結板15とピン16との
間で異常摩耗が発生する問題がある。すなわち、上記連
結板15に伝えられる脈動圧は連結板15を周方向へ振
動させるように作用するため、連結板15のピン孔とピ
ン16との間が一点局部的に衝突を繰り返すことによる
フレッティング摩耗という異常摩耗の原因となる。特
に、上記リンク板14や連結板15は高温無潤滑で動か
されるため、上記問題は顕著である。
However, in the case of the conventional variable displacement supercharger described above, pulsating pressure is generated between the nozzle vanes 12 by the exhaust gas from the engine, and the pulsating pressure is generated from the nozzle vanes 12 to the link plate 14. Since it is transmitted to the connecting plate 15 via the pins 16, there is a problem that abnormal wear occurs between the connecting plate 15 and the pins 16. That is, the pulsating pressure transmitted to the connecting plate 15 acts so as to vibrate the connecting plate 15 in the circumferential direction, so that the pin hole of the connecting plate 15 and the pin 16 are repeatedly hit at one point to cause the fretting. Causes abnormal wear such as ting wear. Especially, since the link plate 14 and the connecting plate 15 are moved without lubrication at high temperature, the above problem is remarkable.

【0004】そこで、本発明は、連結板のピン孔とピン
との間で一点局部的な衝突が起らないようにして、連結
板とピンとの連結部に異常摩耗が発生することがないよ
うにしようとするものである。
Therefore, according to the present invention, a single point local collision does not occur between the pin hole of the connecting plate and the pin so that abnormal wear does not occur at the connecting part between the connecting plate and the pin. Is what you are trying to do.

【0005】[0005]

【課題を解決するための手段】本発明は、上記課題を解
決するために、タービン車室内のタービン翼車の外周に
配列した複数のノズルベーンにそれぞれリンク板の一端
部を結合すると共に、該各隣り合うリンク板の他端部間
を連結板により周方向にピン連結し、該連結板の周方向
移動変位をリンク板を介して各ノズルベーンに伝えるこ
とにより各ノズルベーン間のスロートを調整するように
してある可変容量型過給機において、上記連結板を、ピ
ン孔を設けた両端の環状部と該環状部間を一体連結する
アーム部とからなる構成とし、且つ両ピン孔の中心を結
ぶ直線に対してアーム部を適宜傾斜させてなる構成とす
る。
In order to solve the above-mentioned problems, the present invention connects one end of a link plate to each of a plurality of nozzle vanes arranged on the outer periphery of a turbine impeller in a turbine casing, and The other ends of the adjacent link plates are pin-connected in the circumferential direction by a connecting plate, and the displacement in the circumferential direction of the connecting plate is transmitted to each nozzle vane via the link plate so that the throat between the nozzle vanes is adjusted. In the variable displacement supercharger, the connecting plate is composed of an annular part at both ends provided with pin holes and an arm part integrally connecting the annular parts, and a straight line connecting the centers of both pin holes. The arm part is appropriately inclined with respect to the above.

【0006】[0006]

【作用】各ノズルベーンに結合したリンク板を連結する
連結板が、環状部のピン孔中心間を結ぶ直線に対してア
ーム部を傾斜させた形状となっているため、ノズルベー
ン間に発生した脈動が連結板に周方向の振動として伝わ
っても、連結板のピン孔とピンとの衝突力がピン回りに
分散されること、更には連結板が弾性変形させられるこ
とから、連結板とピンとの連結部に一点局部的な繰り返
しの衝突力が加わらなくなり、異常摩耗が防止されるこ
とになる。
[Operation] Since the connecting plate for connecting the link plates connected to the respective nozzle vanes has a shape in which the arm portion is inclined with respect to the straight line connecting the pin hole centers of the annular portion, pulsation generated between the nozzle vanes Even if the vibration is transmitted to the connecting plate in the circumferential direction, the collision force between the pin hole of the connecting plate and the pin is dispersed around the pin, and further, the connecting plate is elastically deformed. In addition, no one point local repeated collision force is applied, and abnormal wear is prevented.

【0007】[0007]

【実施例】以下、本発明の実施例を図面を参照して説明
する。
Embodiments of the present invention will be described below with reference to the drawings.

【0008】図1乃至図3は本発明の一実施例を示すも
ので、図6及び図7に示すものと同様に、タービン車室
1内のタービン翼車4の外周に配列した複数のノズルベ
ーン12にそれぞれリンク板14の一端部を結合し、該
各隣り合うリンク板14の他端部間を連結板15により
ピン16を用いて周方向に連結し、該連結板15の周方
向移動変位をリンク板14を介して各ノズルベーン12
に伝えることにより、各ノズルベーン12間のスロート
Sを広狭調整してエンジンから導入されるガスの流量を
調整させられるようにしてある可変容量型過給機におい
て、上記連結板15を、図3に拡大して示す如く、ピン
孔22を設けた両端の環状部20と、該環状部20間を
一体連結するアーム部21とからなる構成とし、且つ上
記両ピン孔22の中心O間を結ぶ直線Aに対して上記ア
ーム部21の軸心線(長手方向中心線)Bを適宜角度α
傾斜させてなる構成とする。
FIGS. 1 to 3 show an embodiment of the present invention, and like the ones shown in FIGS. 6 and 7, a plurality of nozzle vanes arranged on the outer periphery of the turbine impeller 4 in the turbine casing 1. 12, one end of each link plate 14 is connected to each other, and the other ends of the adjacent link plates 14 are connected in the circumferential direction by the connecting plate 15 using the pin 16 to move the connecting plate 15 in the circumferential direction. Each nozzle vane 12 through the link plate 14
In the variable displacement supercharger in which the flow rate of the gas introduced from the engine is adjusted by adjusting the throat S between the nozzle vanes 12 to a wide range by transmitting the above to the connecting plate 15 shown in FIG. As shown in an enlarged manner, it is constituted by an annular portion 20 provided with pin holes 22 at both ends and an arm portion 21 integrally connecting the annular portions 20, and a straight line connecting the centers O of the both pin holes 22. The axial center line (longitudinal center line) B of the arm portion 21 relative to A is appropriately angled α
It is configured to be inclined.

【0009】上記アーム部21の傾斜角αは、ピン16
とピン孔22との間のクリアランスをaとし、アーム部
21の長手方向中心線Bに対するピン孔22の中心Oか
らの垂線距離をbとしたとき、b>2aの関係となるよ
うに選定する。
The inclination angle α of the arm portion 21 is determined by the pin 16
When the clearance between the pin hole 22 and the pin hole 22 is a, and the perpendicular distance from the center O of the pin hole 22 to the longitudinal center line B of the arm portion 21 is b, the relation b> 2a is selected. .

【0010】ノズルベーン12間に脈動が発生し、その
脈動がノズルベーン12からリンク板14、ピン16を
介して連結板15に周方向の振動として伝わると、従来
では、連結板15とピン16との連結部に一点局部的な
衝突力が作用していたが、本発明においては、連結板1
5の形状が、環状部20のピン孔中心O間を結ぶ直線A
に対してアーム部21を傾斜させた形状となっているた
め、上記一点局部的な衝突力が緩衝緩和されることにな
る。
When pulsation is generated between the nozzle vanes 12, and the pulsation is transmitted as vibration in the circumferential direction from the nozzle vanes 12 to the connecting plate 15 via the link plate 14 and the pin 16, conventionally, the connecting plate 15 and the pin 16 are separated from each other. Although a one-point local collision force acts on the connecting portion, in the present invention, the connecting plate 1
The shape of 5 is a straight line A connecting the pin hole centers O of the annular portion 20.
On the other hand, since the arm portion 21 is inclined, the one-point local collision force is buffered and relaxed.

【0011】すなわち、本発明の場合、連結板15は、
環状部20のピン孔中心O間を結ぶ直線Aに対して、環
状部20間を一体連結するアーム部21の長手方向中心
線Bが傾斜しているため、脈動に起因する振動が発生し
ても、その力が一方の環状部20からアーム部21を介
して他方の環状部20へ伝わろうとするときに、連結板
15全体を重心Gを中心にねじる(回転させる)ような
力の伝達が行われることになり、これによりピン孔22
とピン16との衝突力がピン16回りに分散されること
になる。又、アーム部21が傾斜していることから、上
記ねじり力が発生すると、連結板15は環状部20間で
弾性変形させられることになる。したがって、連結板1
5とピン16との連結部には一点局部的な繰り返しの衝
突力が作用しなくなり、異常摩耗の発生が防止される。
That is, in the case of the present invention, the connecting plate 15 is
Since the longitudinal center line B of the arm portion 21 that integrally connects the annular portions 20 is inclined with respect to the straight line A that connects the pin hole centers O of the annular portion 20, vibration due to pulsation occurs. However, when the force is transmitted from one annular portion 20 to the other annular portion 20 via the arm portion 21, the transmission of the force such as twisting (rotating) the entire connecting plate 15 about the center of gravity G is performed. Will be carried out, which results in pin holes 22
The collision force between the pin 16 and the pin 16 is dispersed around the pin 16. Further, since the arm portion 21 is inclined, when the above-mentioned twisting force is generated, the connecting plate 15 is elastically deformed between the annular portions 20. Therefore, the connecting plate 1
A single point local repeated collision force does not act on the connecting portion between the pin 5 and the pin 16, and abnormal wear is prevented from occurring.

【0012】因に、本発明の過給機と従来の過給機との
ピン連結部の摩耗量を経時的に比較したところ、図5に
示す如く、本発明の場合、曲線イの如くなり、従来例の
曲線ロに比して1/3程度の摩耗量であるという結果が
得られた。
Incidentally, when the wear amounts of the pin connecting portions of the supercharger of the present invention and the conventional supercharger are compared with each other with time, as shown in FIG. The result is that the wear amount is about 1/3 of that of the curve B of the conventional example.

【0013】なお、本発明は上記実施例のみに限定され
るものではなく、連結板15としては、図4に示す如き
S字形のものを用いるようにしてもよいこと、その他本
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 embodiment, and the connecting plate 15 may be S-shaped as shown in FIG. 4, and other points of the present invention will be described. It goes without saying that various changes can be made without departing from the scope.

【0014】[0014]

【発明の効果】以上述べた如く、本発明の可変容量型過
給機によれば、各ノズルベーンに結合したリンク板を周
方向にピン連結するための連結板を、環状部のピン孔中
心間を結ぶ直線に対してアーム部が傾斜するような形状
としたので、ノズルベーン間の脈動が連結板に周方向の
振動として伝えられても、連結板のピン孔とピンとの衝
突力をピン回りに分散させることができると共に、連結
板を弾性変形させることができ、これにより、連結板と
ピンとの連結部に一点局部的に加えられようとする衝突
力を緩衝緩和させることができ、異常摩耗の発生を防止
することができる、という優れた効果を発揮する。
As described above, according to the variable capacity supercharger of the present invention, the connecting plate for connecting the link plates connected to the nozzle vanes in the circumferential direction with the connecting plate is provided between the centers of the pin holes of the annular portion. Since the arm part is inclined with respect to the straight line connecting the connecting lines, even if the pulsation between the nozzle vanes is transmitted to the connecting plate as circumferential vibration, the collision force between the pin hole of the connecting plate and the pin is moved around the pin. In addition to being able to disperse, the connecting plate can be elastically deformed, whereby the collision force that is about to be locally applied to the connecting part between the connecting plate and the pin can be buffered and relaxed, and abnormal wear can be prevented. It has an excellent effect that it can be prevented from occurring.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の可変容量型過給機の一実施例を示す部
分概略図である。
FIG. 1 is a partial schematic view showing an embodiment of a variable displacement supercharger of the present invention.

【図2】図1の一部を切断して示す平面図である。FIG. 2 is a plan view showing a part of FIG. 1 cut away.

【図3】連結板の拡大図である。FIG. 3 is an enlarged view of a connecting plate.

【図4】連結板の他の例を示す拡大図である。FIG. 4 is an enlarged view showing another example of the connecting plate.

【図5】本発明と従来例とのピン連結部摩耗量を比較し
た実験結果を示す図である。
FIG. 5 is a diagram showing an experimental result comparing the amount of wear of a pin connecting portion between the present invention and a conventional example.

【図6】従来の可変容量型過給機の一例を示す概要図で
ある。
FIG. 6 is a schematic diagram showing an example of a conventional variable displacement supercharger.

【図7】図6の VII方向矢視図である。FIG. 7 is a view on arrow VII in FIG.

【符号の説明】[Explanation of symbols]

1 タービン車室 4 タービン翼車 12 ノズルベーン 14 リンク板 15 連結板 16 ピン 20 環状部 21 アーム部 22 ピン孔 S スロート O 中心 A 直線 α 傾斜角 1 Turbine Cabin 4 Turbine Impeller 12 Nozzle Vane 14 Link Plate 15 Connecting Plate 16 Pin 20 Annular Part 21 Arm Part 22 Pin Hole S Throat O Center A Straight Line α Inclination Angle

───────────────────────────────────────────────────── フロントページの続き (72)発明者 三堀 健 東京都江東区豊洲三丁目1番15号 石川島 播磨重工業株式会社東二テクニカルセンタ ー内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Ken Mori, 1-1-15 Toyosu, Koto-ku, Tokyo Ishikawajima Harima Heavy Industries Co., Ltd. Toni Technical Center

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 タービン車室内のタービン翼車の外周に
配列した複数のノズルベーンにそれぞれリンク板の一端
部を結合すると共に、該各隣り合うリンク板の他端部間
を連結板により周方向にピン連結し、該連結板の周方向
移動変位をリンク板を介して各ノズルベーンに伝えるこ
とにより各ノズルベーン間のスロートを調整するように
してある可変容量型過給機において、上記連結板を、ピ
ン孔を設けた両端の環状部と該環状部間を一体連結する
アーム部とからなる構成とし、且つ両ピン孔の中心を結
ぶ直線に対してアーム部を適宜傾斜させてなる構成とし
たことを特徴とする可変容量型過給機。
1. A plurality of nozzle vanes arranged on the outer periphery of a turbine impeller in a turbine casing are connected to respective one ends of link plates, and the other end of each adjacent link plate is circumferentially connected by a connecting plate. In a variable displacement supercharger in which pins are connected and the displacement in the circumferential direction of the connecting plate is transmitted to each nozzle vane via a link plate, the throat between the nozzle vanes is adjusted. It is configured to include an annular portion at both ends provided with holes and an arm portion integrally connecting the annular portions, and the arm portion is appropriately inclined with respect to a straight line connecting the centers of both pin holes. A characteristic variable capacity supercharger.
JP35488192A 1992-12-18 1992-12-18 Variable displacement turbocharger Expired - Fee Related JP3239499B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP35488192A JP3239499B2 (en) 1992-12-18 1992-12-18 Variable displacement turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP35488192A JP3239499B2 (en) 1992-12-18 1992-12-18 Variable displacement turbocharger

Publications (2)

Publication Number Publication Date
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014102981A1 (en) * 2012-12-27 2014-07-03 三菱重工業株式会社 Radial turbine rotor blade

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014102981A1 (en) * 2012-12-27 2014-07-03 三菱重工業株式会社 Radial turbine rotor blade
CN104854325A (en) * 2012-12-27 2015-08-19 三菱重工业株式会社 Radial turbine rotor blade
US9777578B2 (en) 2012-12-27 2017-10-03 Mitsubishi Heavy Industries, Ltd. Radial turbine blade

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