JPS60198306A - Controller for variable guide vane in supercharger and like - Google Patents
Controller for variable guide vane in supercharger and likeInfo
- Publication number
- JPS60198306A JPS60198306A JP59054544A JP5454484A JPS60198306A JP S60198306 A JPS60198306 A JP S60198306A JP 59054544 A JP59054544 A JP 59054544A JP 5454484 A JP5454484 A JP 5454484A JP S60198306 A JPS60198306 A JP S60198306A
- Authority
- JP
- Japan
- Prior art keywords
- lever
- link
- levers
- guide vane
- pin
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
Abstract
Description
【発明の詳細な説明】 〔発明の技術分野〕 本発明は過給機などの可変案内翼の制御装置に関する。[Detailed description of the invention] [Technical field of invention] The present invention relates to a control device for variable guide vanes such as a supercharger.
第1図は過給機の要部断面図、第2図は第1図の■−■
断面図である。Figure 1 is a sectional view of the main parts of the turbocharger, Figure 2 is from ■ to ■ in Figure 1.
FIG.
遠心式コンプレッサ、輻流タービン、過給機等において
は、流入する空気、量をコントロールするため可変式案
内翼を使用している。図面において1は過給機、2はハ
ウジング、3はシュラウド、4はタービンホイール、5
はフランジ、6は案内翼である。案内翼6は支軸7にブ
ツシュ8を介してシュラウド3に複数個取シ付けられて
いる。9はレバー、10はりング、11はピンである。Centrifugal compressors, flow turbines, superchargers, etc. use variable guide vanes to control the amount of air flowing in. In the drawings, 1 is a supercharger, 2 is a housing, 3 is a shroud, 4 is a turbine wheel, and 5 is a
is a flange, and 6 is a guide wing. A plurality of guide vanes 6 are attached to the shroud 3 via bushes 8 on the support shaft 7. 9 is a lever, 10 is a ring, and 11 is a pin.
ここで隣接するレバー9間のなす角度αは360゜
α= (N:翼枚数)
でアシ、レバー9上におけるピン11間のなす角をαに
設定すると、第2図の2点鎖線Aで示すようにレバー9
とリンク10とで平行四辺形を形成することができる。Here, the angle α between adjacent levers 9 is 360° α = (N: number of blades), and if the angle between the pins 11 on the lever 9 is set to α, then the angle α between the pins 11 on the lever 9 is set as Lever 9 as shown
and the link 10 can form a parallelogram.
従ってレバー9の一つに他のリンク機構を連結させて回
転させると、他のレバーも同じ角度だけ回転させること
ができる。Therefore, if one of the levers 9 is connected to another link mechanism and rotated, the other levers can also be rotated by the same angle.
1)隣接するレバー9をリンク10で連結しているので
、リンク10同士の干渉を避けるためレバー9が・長く
なり、ハウジング2を大きくしなければならない。1) Adjacent levers 9 are connected by links 10, so in order to avoid interference between the links 10, the levers 9 become longer and the housing 2 must be made larger.
2)隣接するレバー9をリンク10で連結しているので
、リンク数が多くなシ各レバー9とリンク10の取付は
ガタが集積されて案内翼6の回転角に誤差が生じること
がある。2) Since adjacent levers 9 are connected by links 10, the number of links is large, and looseness may accumulate in the attachment of each lever 9 and link 10, resulting in an error in the rotation angle of the guide vane 6.
本発明の目的は、前記従来装置の問題点を解消し、案内
翼を動かすレバーとリンク間のガタの集積による案内翼
の回転誤差を少なくするとともに、ハウジングの小形化
を図った過給機等における可変案内v・;4の制御装置
を提供するにある。It is an object of the present invention to solve the problems of the conventional device described above, to reduce the rotation error of the guide vane due to the accumulation of play between the lever and the link that moves the guide vane, and to reduce the size of the housing of a supercharger etc. The present invention provides a control device for a variable guide v.;4.
レバーを1つおきに連結して前側及び裏側の2系列とし
又案内翼が奇数個の場合にも適用できる連結機構を採用
し、前記目的を達成できるように構成したものである。The levers are connected every other lever to form two lines on the front side and the back side, and a connecting mechanism that can be applied even when there is an odd number of guide vanes is adopted, so that the above object can be achieved.
以下第3〜8図によって、本発明の一実施例について説
明する。第3〜4図は案内翼が偶数個の場合のり/り処
理を示す。第3図は案内翼を連結するリンク機構の構造
図、第3図は第4図の■矢視図、第4図は第3図のIV
−IV断面図である。An embodiment of the present invention will be described below with reference to FIGS. 3 to 8. 3 and 4 show the gluing/gluing process when there is an even number of guide vanes. Figure 3 is a structural diagram of the link mechanism that connects the guide vanes, Figure 3 is a view from the ■ arrow in Figure 4, Figure 4 is the IV in Figure 3.
-IV sectional view.
又第5〜8図は案内翼が奇数個の場合のリンク処理を示
し、第5図は従来例の第3図に相当する図面、第6図は
第5図の背面図、第7図は第5図の■矢視図、第8図は
第5図の■−■断面図である。5 to 8 show link processing when there is an odd number of guide vanes, FIG. 5 is a drawing corresponding to FIG. 3 of the conventional example, FIG. 6 is a rear view of FIG. 5, and FIG. FIG. 5 is a view taken along the arrow ■, and FIG. 8 is a sectional view taken along the line ■-■ in FIG.
図で21はハウジング、22はシュラウド、23は案内
翼、24は支軸、25はプツシ−126はレバー、27
はリング、28はピンである。In the figure, 21 is a housing, 22 is a shroud, 23 is a guide vane, 24 is a support shaft, 25 is a push-piece, 126 is a lever, 27
is a ring, and 28 is a pin.
リンク27はレバー726の表および裏に配設される2
つの系列からなシ、各レバー26を1つおきに連結して
円環状に形成される。(以下表側の系列には J裏側の
系列にはbの添字をつける)ここで隣接するレバー26
間のなす角度αはであシ、レバー26上にあるピン28
間のなす角度をβ=2αと設定すると、第3図の2点鎖
線Bに示すようにレバー26とリンク27とで平行四辺
形を形成することかでさる。従って1つのレバー26を
回転させると他のレバー26も同じ角度だけ回転させる
ことができる。The links 27 are provided on the front and back sides of the lever 726.
The levers 26 are formed in a ring shape by connecting every other lever 26 in two series. (Hereinafter, the series on the front side will be suffixed J, and the series on the back side will be suffixed with b.) Here, the adjacent lever 26
The angle α between the pin 28 on the lever 26 is
If the angle between them is set to β=2α, the lever 26 and the link 27 form a parallelogram as shown by the two-dot chain line B in FIG. Therefore, when one lever 26 is rotated, the other levers 26 can also be rotated by the same angle.
次に表側および裏側のリンク系列の連結機構について説
明する。Next, the connection mechanism of the link series on the front side and the back side will be explained.
案内翼が偶数個の場合には上表側と裏側の各系列は同数
となシ、前側のレバー27aの1つと、裏側のし□z−
27bの1らとを他のり・り機構によシ連動させれば、
同時に案内翼23を回転させることができるが、案内翼
23が奇数個の場合には余るものが出るので、単純に1
つおきに連結することはできない。If there is an even number of guide vanes, the number of each series on the upper front side and the back side must be the same, and one of the levers 27a on the front side and the lever 27a on the back side
If 1 and 27b are interlocked with another linkage mechanism,
The guide vanes 23 can be rotated at the same time, but if there is an odd number of guide vanes 23, some will be left over, so simply
Cannot be concatenated every other time.
以下案内翼が奇数個の場合のリンク処理について第5〜
8図によって説明する。なお説明の都合上者リンク及び
ピンに1.2.3の添字をつける。Below is section 5 about link processing when there is an odd number of guide vanes.
This will be explained with reference to Figure 8. For convenience of explanation, the subscripts 1.2.3 are added to links and pins.
30はリンクである。30 is a link.
リンク30は表側に位置する平坦部31、裏側に位置す
る平坦部32、平坦部31.32に接続する上面部33
および平坦部31に接続し、他のリンク機構に連結する
34とから形成される。なお前記31,32.33には
レバー26、リンク27と干渉しないように適当な切欠
きおよび高さ等を設ける。35はストツノやである。The link 30 has a flat part 31 located on the front side, a flat part 32 located on the back side, and an upper surface part 33 that connects to the flat parts 31 and 32.
and 34 connected to the flat part 31 and connected to other link mechanisms. Note that appropriate notches and heights are provided in the above-mentioned 31, 32, and 33 so as not to interfere with the lever 26 and the link 27. 35 is Stotsunoya.
リンク30は表側レバー26a1とピン28a2で、裏
側レバー26b2とピン28b3で連結する。The link 30 is connected by a front side lever 26a1 and a pin 28a2, and a back side lever 26b2 and a pin 28b3.
次に前記実施例の作用について説明する。Next, the operation of the above embodiment will be explained.
案内翼が偶数個の場合には、表側と裏側の系列のリンク
のうち各1つと連動させて他のリンク機構によ)、案内
翼を同時に回転させることができる。If there is an even number of guide vanes, the guide vanes can be rotated simultaneously by interlocking with each one of the front and back series of links (by means of other link mechanisms).
案内翼が奇数個の場合には、リンク3oを他のり/り機
構によシ作動させることにより、表側と裏側の系列のリ
ンクを同時に作動させて案内翼を回転させることができ
る。When there is an odd number of guide vanes, by operating the link 3o by another sliding mechanism, the front and back series of links can be operated simultaneously to rotate the guide vanes.
1)リンクを1つおきに連結させて2系列としたことに
よシレバーとピン間の角度が従来装置の2倍となシ、レ
バーの高さを低くすることが可能となシ、ハウジンクの
小形化を図ることができる。1) By connecting every other link to form two series, the angle between the lever and the pin is twice that of the conventional device, and the height of the lever can be lowered. Miniaturization can be achieved.
2)表側および裏側の各系列ではリンクの数が半分とな
るので各リンクとレバーの取シ付はガタの集積を小さく
押えることができ案内翼の回転誤差が小さくなシ精度が
向上する。2) Since the number of links is halved in each series on the front side and the back side, the accumulation of looseness in the mounting of each link and lever can be suppressed to a minimum, and the rotational error of the guide vanes is reduced, improving accuracy.
3)案内翼が奇数個の場合には、レバーも奇数個となシ
通常の連結では1つが余シネ規則な連結となるが本発明
の連結手段ではすべてのレバーを1つおきに連結するこ
とができ、案内翼の回転を円滑に行うことができる。3) When there is an odd number of guide vanes, there is also an odd number of levers.In normal connection, one is connected regularly, but with the connection means of the present invention, all the levers are connected every other lever. This allows the guide vanes to rotate smoothly.
第1〜2図は従来装置に係るもので第1図は要部断面図
、第2図は第1図の■−■断面図、第3〜8図は本発明
に係るものでさらに第3〜4図は案内翼が偶数個の場合
、第3図は案内翼を表裏の2系列に連結したリンク機構
の構造図(第3図は第4図の■矢視図)、第4図は第3
図のIV −IV断面図である。第5〜8図は案内翼が
奇数個の場合のリンク処理を示し、第5図は従来例の第
3図に相当する図面、第6図は第5図の背面図、第7図
は第5図の■矢視図、第8図は第5図の■−■断面図で
ある。
23・・・案内翼、24・・・支軸、26・・・レバー
、27・・・リンク、28・・・ビン。
第1図1 to 2 are related to a conventional device, and FIG. 1 is a sectional view of a main part, FIG. 2 is a sectional view taken along the line ■-■ of FIG. 1, and FIGS. Figure 4 shows the structure of the link mechanism that connects the guide vanes in two series (front and back) (Figure 3 is a view from the ■ arrow in Figure 4), and Figure 4 shows the case where there is an even number of guide vanes. Third
It is a sectional view taken along IV-IV in the figure. 5 to 8 show link processing when there is an odd number of guide vanes, FIG. 5 is a drawing corresponding to FIG. 3 of the conventional example, FIG. 6 is a rear view of FIG. 5, and FIG. 5 is a view in the direction of the ■ arrow, and FIG. 8 is a sectional view taken along the line ■-■ in FIG. 23...Guide blade, 24...Spindle, 26...Lever, 27...Link, 28...Bin. Figure 1
Claims (1)
度を変化せしめるようにした過給機において、各支軸に
ピン結合されたレバーと、該レバーの反支軸側を円周方
向に一個おきにピン結合したリンクを具えたとと全特徴
とする過給機等における可変案内翼の制御装置。In a supercharger in which a guide vane is rotatably provided around its spindle to change its entrance/exit angle, a lever is connected to each spindle with a pin, and the side opposite to the spindle of the lever is attached to the circumference. A control device for a variable guide vane in a supercharger, etc., characterized by having links connected by pins every other direction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59054544A JPS60198306A (en) | 1984-03-23 | 1984-03-23 | Controller for variable guide vane in supercharger and like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59054544A JPS60198306A (en) | 1984-03-23 | 1984-03-23 | Controller for variable guide vane in supercharger and like |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS60198306A true JPS60198306A (en) | 1985-10-07 |
Family
ID=12973618
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP59054544A Pending JPS60198306A (en) | 1984-03-23 | 1984-03-23 | Controller for variable guide vane in supercharger and like |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60198306A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63143320A (en) * | 1986-12-05 | 1988-06-15 | Honda Motor Co Ltd | Movable vane driving mechanism of turbocharger |
JPS63143323A (en) * | 1986-12-05 | 1988-06-15 | Honda Motor Co Ltd | Movable vane driving mechanism of turbocharger |
US5028208A (en) * | 1989-01-10 | 1991-07-02 | Ishikawajima-Harima Jukogyo Kabushiki Kaisha | Nozzle blade angle adjustment device for variable geometry turbocharger |
US6582190B2 (en) * | 2000-05-22 | 2003-06-24 | Mitsubishi Heavy Industries, Ltd. | Variable-capacity turbine |
US6699010B2 (en) * | 2000-05-19 | 2004-03-02 | Mitsubishi Heavy Industries, Ltd. | Nozzle adjustment mechanism for variable-capacity turbine |
EP2525048A1 (en) * | 2011-05-18 | 2012-11-21 | Siemens Aktiengesellschaft | Drive lever arrangement |
-
1984
- 1984-03-23 JP JP59054544A patent/JPS60198306A/en active Pending
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63143320A (en) * | 1986-12-05 | 1988-06-15 | Honda Motor Co Ltd | Movable vane driving mechanism of turbocharger |
JPS63143323A (en) * | 1986-12-05 | 1988-06-15 | Honda Motor Co Ltd | Movable vane driving mechanism of turbocharger |
JPH0343450B2 (en) * | 1986-12-05 | 1991-07-02 | Honda Motor Co Ltd | |
JPH0343451B2 (en) * | 1986-12-05 | 1991-07-02 | Honda Motor Co Ltd | |
US5028208A (en) * | 1989-01-10 | 1991-07-02 | Ishikawajima-Harima Jukogyo Kabushiki Kaisha | Nozzle blade angle adjustment device for variable geometry turbocharger |
US6699010B2 (en) * | 2000-05-19 | 2004-03-02 | Mitsubishi Heavy Industries, Ltd. | Nozzle adjustment mechanism for variable-capacity turbine |
US6582190B2 (en) * | 2000-05-22 | 2003-06-24 | Mitsubishi Heavy Industries, Ltd. | Variable-capacity turbine |
EP2525048A1 (en) * | 2011-05-18 | 2012-11-21 | Siemens Aktiengesellschaft | Drive lever arrangement |
WO2012156180A1 (en) * | 2011-05-18 | 2012-11-22 | Siemens Aktiengesellschaft | Drive lever arrangement |
US9435352B2 (en) | 2011-05-18 | 2016-09-06 | Siemens Aktiengesellschaft | Drive lever arrangement |
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