JPS5918160Y2 - Rotating machine impeller device - Google Patents

Rotating machine impeller device

Info

Publication number
JPS5918160Y2
JPS5918160Y2 JP1978043121U JP4312178U JPS5918160Y2 JP S5918160 Y2 JPS5918160 Y2 JP S5918160Y2 JP 1978043121 U JP1978043121 U JP 1978043121U JP 4312178 U JP4312178 U JP 4312178U JP S5918160 Y2 JPS5918160 Y2 JP S5918160Y2
Authority
JP
Japan
Prior art keywords
groove
blade
radial direction
blade root
rotating machine
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.)
Expired
Application number
JP1978043121U
Other languages
Japanese (ja)
Other versions
JPS54145806U (en
Inventor
彰 小山
喜昭 池口
Original Assignee
川崎重工業株式会社
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 川崎重工業株式会社 filed Critical 川崎重工業株式会社
Priority to JP1978043121U priority Critical patent/JPS5918160Y2/en
Publication of JPS54145806U publication Critical patent/JPS54145806U/ja
Application granted granted Critical
Publication of JPS5918160Y2 publication Critical patent/JPS5918160Y2/en
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 本考案は、丁字形の溝に動翼を植えつけて製作する回転
機械の翼車装置の改良に関する。
[Detailed Description of the Invention] The present invention relates to an improvement of a blade wheel device for a rotating machine, which is manufactured by installing moving blades in a T-shaped groove.

回転機械の翼車装置は、回転基体の周囲に動翼を植付け
て製作する。
A blade wheel device for a rotating machine is manufactured by planting rotor blades around a rotating base.

動翼を植え付けるのには普通、回転基体に条溝などの溝
を切り、そこに動翼の翼根を嵌める。
To install rotor blades, grooves such as grooves are usually cut in the rotating base, and the blade roots of the rotor blade are fitted into these grooves.

その嵌め込みは大別して二通りある。There are two types of inlays.

太き目の溝に翼根を挿し込み適当な手段たとえばボルト
で締めつけるというやり方と、適当な形状の溝に同形の
翼根をぴったり嵌め込む、いわゆる「はめあい方式」と
がある。
There are two methods: inserting the blade root into a thick groove and tightening it with an appropriate means such as bolts, and the so-called "fitting method" in which a blade root of the same shape is tightly fitted into a groove of an appropriate shape.

ところで、軸流圧縮機、軸流タービンなど回転機械の翼
車装置の動翼はその翼根が遠心力、空気圧又は蒸気圧な
どによるスラスト力に耐え、また、振動の発生を防ぐよ
うにいろいろに工夫されなければならない。
By the way, the rotor blades of rotary machines such as axial flow compressors and axial flow turbines are designed to withstand thrust forces caused by centrifugal force, air pressure, steam pressure, etc., and to prevent vibrations. It must be devised.

そこで、嵌めあい方式では、できる限り、溝形状と翼根
形状とが同形であり、両者がぴったり嵌まり合うように
なされるのが普通である。
Therefore, in the fitting method, the groove shape and the blade root shape are usually made to have the same shape as much as possible so that they fit perfectly together.

溝は軸方向に又は円周方向に条溝として形成され、特に
円周方向に長く形成される条溝に断面が同形状の翼根を
挿入しようとすると、精度高く同形状に予め加工がなさ
れているわけであるが、精度が高ければ高いほど、その
挿入作業がきわめてむつかしい。
Grooves are formed as grooves in the axial direction or in the circumferential direction.In particular, when attempting to insert a blade root with the same shape in cross section into a groove that is formed long in the circumferential direction, it is difficult to precisely machine the same shape in advance. However, the higher the precision, the more difficult the insertion process becomes.

逆に、加工精度を故意に案悪くして、即ち、溝と翼根と
の間の隙間を予め設けるようにしておくと、動翼の固定
性が悪くなり、スラスト力などを受けあ動翼が振動し、
翼車性能が悪く耐久性も劣化してしまう。
On the other hand, if the machining accuracy is intentionally compromised, that is, by creating a gap between the groove and the blade root in advance, the fixation of the rotor blade will deteriorate, and the rotor blade will not be able to handle the thrust force. vibrates,
The performance of the blade wheel is poor and the durability is also degraded.

2つの方式にはそれぞれに一長一短があり、概にどちら
がよいとは言えず、その製作工場の技術の伝統、回転機
械の種別など諸般の事情で、その都度に十分の考慮が払
われて適切な方式がとられる。
Each of the two methods has its own merits and demerits, and it cannot be said that one is better in general.Due to various circumstances such as the technological tradition of the manufacturing factory and the type of rotating machinery, the appropriate method must be carefully considered in each case. A method is adopted.

この考案は、はめあい方式の翼車装置の上記欠点を除い
て、固定性にすぐれ耐振動性能にすぐれ、しかも、挿入
作業がきわめて容易な回転機械の翼車装置を提供するこ
とを目的とし、その溝形状がいわゆる丁字形のものにつ
いて改良しようとするものであり、溝幅が狭い中間部位
とその中間部位に半径方向に両側に連続する溝幅が広い
下位側部位と上位側部位とから戒る断面が工の字状条溝
に同形の翼根の動翼が当該条溝に沿って挿し込まれて嵌
められる回転機械の翼車装置において、上記条溝の中間
部位の半径方向の高さ幅をaとし、その中間部位の溝に
嵌まり込む翼根の当該相当部の半径方向の高さ幅をbと
すると、a<bであり、また、上記条溝の中間部位に下
位側に続く下位側部位の半径方向の高さ幅をCとし、こ
の下位側部位に嵌まり込む翼根の当該相当部位の半径方
向の高さ幅をdとすると、c>dであり、上記条溝に嵌
まる当該相当部位の翼根の底部とその条溝の底部との間
に、動翼を上方位に押し上げるようにこれら両者間を弾
発させる円筒状弾発材が介設され、この円筒状弾発材の
軸方向と上記条溝の条方向とは交叉していることを特徴
とする。
The purpose of this invention is to eliminate the above-mentioned drawbacks of the fitting type blade wheel device, provide a blade wheel device for a rotating machine that has excellent fixation and vibration resistance, and is extremely easy to insert. This is an attempt to improve the so-called T-shaped groove shape, and the groove width is narrow in the middle part, and the middle part has a lower part and an upper part in which the groove width is wider on both sides in the radial direction. In a blade wheel device of a rotating machine in which a rotor blade with a blade root having the same shape as a groove with a cross section is inserted along the groove, the height width in the radial direction of the intermediate portion of the groove. If a is the height width in the radial direction of the corresponding part of the blade root that fits into the groove in the intermediate part, then a<b, and the groove continues to the lower side in the intermediate part of the groove. If the height width in the radial direction of the lower side part is C, and the height width in the radial direction of the corresponding part of the blade root that fits into this lower side part is d, then c>d, and the groove is A cylindrical elastic material is interposed between the bottom of the blade root at the corresponding part to be fitted and the bottom of the groove, and the cylindrical elastic material is interposed between the two to push the rotor blade upward. It is characterized in that the axial direction of the resilient material and the direction of the grooves intersect with each other.

以下、本考案に係る実施形態を図面によって具体的に詳
しく説明する。
Hereinafter, embodiments of the present invention will be specifically described in detail with reference to the drawings.

第1図及び第2図で、1は翼根2を有する動翼、3は紙
面で左右の方向を軸方向とする車体の回転基体4につく
られている溝で、断面がいわゆる丁字形であるので一般
にT字溝と称されるが、本明細書では工の字状溝と称す
ることにする。
In Figures 1 and 2, 1 is a rotor blade having a blade root 2, and 3 is a groove made in the rotating base 4 of the car body whose axial direction is the left and right direction in the paper, and whose cross section is so-called T-shaped. Because of this, it is generally called a T-shaped groove, but in this specification it will be called a square-shaped groove.

この溝は、その溝幅が狭い中間部位3aと、この中間部
位3aに半径方向(紙面で上下方向)に両側に連続する
幅が広い下位側部位3bと上位側部位3Cとから成り、
従って、図示断面で工の字状の溝になっている。
This groove consists of an intermediate portion 3a with a narrow groove width, and a lower side portion 3b and an upper side portion 3C with a wider width that continue on both sides of the intermediate portion 3a in the radial direction (in the vertical direction on the paper),
Therefore, the cross section shown in the figure is a square-shaped groove.

また、この溝3は円周方向(図示断面位置で紙面に垂直
)に連続し、条溝である。
Further, this groove 3 is continuous in the circumferential direction (perpendicular to the paper surface at the illustrated cross-sectional position) and is a groove.

今、この条溝の中間部位の半径方向の高さ幅をaとし、
その中間部位の溝に嵌まり込む翼根の当該相当部2aの
半径方向の高さ幅をbとすると、a<bであり、また、
条溝3の中間部位3aに下位に続く下位側部位3bの半
径方向の高さ幅をCとし、この下位側部位に嵌まり込む
翼根2の当該相当部位2bの半径方向の高さ幅をdとす
ると、c>dとなるように、大小関係が定められる。
Now, let the height width in the radial direction of the middle part of this groove be a,
If b is the height width in the radial direction of the corresponding portion 2a of the blade root that fits into the groove in the intermediate portion, a<b, and
Let C be the height width in the radial direction of the lower part 3b following the intermediate part 3a of the groove 3, and the height width in the radial direction of the corresponding part 2b of the blade root 2 that fits into this lower part. If d, then the magnitude relationship is determined so that c>d.

この大小の程度は、説明するまでもなく経験的に判断さ
れるものであるが、敢えて述べると、翼根を溝に無理矢
理に変位させなくとも容易に(両者が接触しあうことな
く)両者の相対変位を行なわせうる程度である。
The degree of this size need not be explained and is determined empirically, but I would like to state that it is possible to easily separate the two blades without forcibly displacing the blade root into the groove (without the two contacting each other). This is the extent to which relative displacement can be performed.

条溝3に嵌まり込む翼根2の底部(たとえば、2d)と
当該条溝3(たとえば31.)の底部との間には、動翼
を上方位に押し上げるようにこれら両者間を弾発させる
円筒状弾発材5が介設され、この円筒状弾発材の軸方向
(第2図では紙面上左右方向、第3図では紙面に垂直)
と条溝3の条方向とは交叉している。
Between the bottom of the blade root 2 that fits into the groove 3 (e.g. 2d) and the bottom of the groove 3 (e.g. 31.), there is an elastic force between them so as to push the rotor blade upward. A cylindrical elastic material 5 is interposed to cause the cylindrical elastic material 5 to move in the axial direction of the cylindrical elastic material (in the left-right direction on the paper in FIG. 2, and perpendicular to the paper in FIG. 3).
and the direction of the groove 3 intersect with each other.

弾発材としては好ましくはロールピン、特に好ましくは
、円筒状割ピン5が用いられる。
As the resilient material, preferably a roll pin, particularly preferably a cylindrical split pin 5 is used.

第3図によく表われているように、条溝3の条方向が円
周方向である場合には、ロールピン5は軸方向に置かれ
ている。
As clearly shown in FIG. 3, when the direction of the grooves 3 is the circumferential direction, the roll pin 5 is placed in the axial direction.

6は動翼の底部に設けられた切欠きてロールピン5を動
翼に対して安定的に位置づけるためのものである。
6 is a notch provided at the bottom of the rotor blade for stably positioning the roll pin 5 with respect to the rotor blade.

ロールピン5の割ピン形態は第1図にみられるようにい
ろいろに工夫されうる。
The split pin form of the roll pin 5 can be devised in various ways as shown in FIG.

上述の実施例は条溝が車体4の円周方向に続くものであ
るが、軸方向に条溝を設ける場合もある。
In the above embodiment, the grooves continue in the circumferential direction of the vehicle body 4, but the grooves may be provided in the axial direction.

第3図に示す実施例において、図示していないが車体4
の一部に比較的に大きく放射方向に開けた穴から動翼1
の翼根2を落し込み、円周方向に翼根2を条溝3に挿し
込み、その際に、切欠き6に割ピン5を嵌めておき、動
翼全体を上方位から押して抑え込みながら前進させて行
くと、比較的に弱い抑え力で動翼全体を割ピン5上に転
ばせながら容易に奥の方へ嵌め込んで行くことができる
In the embodiment shown in FIG. 3, although not shown, the vehicle body 4
The rotor blade 1 is inserted through a relatively large hole drilled in the radial direction in a part of the rotor blade 1.
, and insert the blade root 2 into the groove 3 in the circumferential direction.At this time, fit the cotter pin 5 into the notch 6, and press the entire rotor blade from above to hold it down while moving forward. By doing so, the entire moving blade can be easily fitted to the rear while falling onto the cotter pin 5 with a relatively weak holding force.

上方からの押え込みをやめると、第2図に示すように、
動翼は、翼根2の下方部位2bの肩の上面が条溝3の下
方部位3bの上端部の面に突き当たり、定位置に弾発材
5で上方に押し上げられて止まっている。
When you stop pressing from above, as shown in Figure 2,
In the rotor blade, the upper surface of the shoulder of the lower part 2b of the blade root 2 abuts against the upper end surface of the lower part 3b of the groove 3, and is pushed upward by the resilient material 5 and stopped at a fixed position.

動翼を交換するために車体から取外すのも同じ要領で行
なう。
The same procedure is used to remove the rotor blades from the vehicle body for replacement.

上述したように本考案においては、寸法の設定を行なう
ことで翼根と溝との寸法精度を緩和したから加工コスト
が低減するだけでなく、動翼はめあい時の摺動がきわめ
て楽になる。
As mentioned above, in the present invention, the dimensional accuracy of the blade roots and grooves is relaxed by setting the dimensions, which not only reduces processing costs but also makes sliding when fitting the rotor blades extremely easy.

なお、きっちりとした嵌め合いのちのやボルト、楔止め
のものほどには、弾発材で押し上げられる本考案の動翼
の固定性が足りないように児女けられるが、高速回転す
る翼車では、動翼に働らく大きな遠心力が弾発力に付加
されるので、ボルト締めと同等の固定力が得られ、また
、ゆるみを避けるために必要以上に締めつけるボルトは
どの固定力は実は必要ではなく、遠心力と弾発力と動翼
に加えられる向心力とを合成した力に対し弾発材の弾性
係数をうまく定めることによって、微小な振幅の周期の
長い振動を許容しながら激しい衝撃の振動に関しては実
質上の無振動系をつくることができるので、振動防止の
点でもかえってすぐれるという結果を得ることができ、
−石二鳥の効果がある。
It should be noted that the fixedness of the rotor blade of this invention, which is pushed up by the explosive material, is not as strong as that of tightly fitted bolts or wedges. Since the large centrifugal force acting on the rotor blades is added to the elastic force, a fixing force equivalent to bolt tightening can be obtained, and the fixing force that is actually necessary is to tighten the bolts more than necessary to avoid loosening. Rather, by carefully determining the elastic modulus of the elastic material for the combined force of centrifugal force, elastic force, and centripetal force applied to the rotor blade, it is possible to tolerate intense impact while allowing minute amplitude and long-period vibration. As for vibrations, it is possible to create a virtually vibration-free system, which results in even better results in terms of vibration prevention.
-It has the effect of killing two birds.

きっちりした嵌め合い構造のものでは(連続面で接触し
合うことは実質上不可能で実際問題としては多点接触的
になる)、振動、位置ずれなどでかえって長時間の動翼
回転中にゆるみが発生し振動を起こす原因となるが、本
考案では長期にわたって定位置での固定性にすぐれ、従
って、ケーシング7と動翼1の先端部6との間の隙間e
が長期にわたって一定である一石二鳥の効果があり、し
かも、挿入組立て、取外し交換の作業がきわめて容易で
あるという一石二、三島の効果がある。
If the blades have a tight fitting structure (it is virtually impossible to contact each other on a continuous surface, and in reality it will be a multi-point contact), vibrations, misalignment, etc. may cause the rotor blades to loosen during long rotations. However, the present invention has excellent stability in fixed position over a long period of time, and therefore the gap e between the casing 7 and the tip 6 of the rotor blade 1 is reduced.
It has the effect of killing two birds with one stone in that it remains constant over a long period of time, and it also has the effect of killing two or three birds with one stone in that it is extremely easy to insert, assemble, remove and replace.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案の円筒状弾発材の具体例を示す斜視図、
第2図は本考案の1実施例を示す側面断面図、第3図は
組立状態を示す正面図である。
FIG. 1 is a perspective view showing a specific example of the cylindrical elastic material of the present invention;
FIG. 2 is a side sectional view showing one embodiment of the present invention, and FIG. 3 is a front view showing an assembled state.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 溝幅が狭い中間部位とその中間部位に半径方向に両側に
連続する溝幅が広い下位側部位と上位側部位とから成る
断面が工の字状条溝に同形の翼根の動翼が当該条溝に沿
って挿し込まれて嵌められる回転機械の翼車装置におい
て、上記条溝の中間部位の半径方向の高さ幅をaとし、
その中間部位の溝に嵌まり込む翼根の当該相当部の半径
方向の高さ幅をbとすると、a<bであり、また、上記
条溝の中間部位に下位側に続く下位側部位の半径方向の
高さ幅をCとし、この下位側部位に嵌まり込む翼根の当
該相当部位の半径方向の高さ幅をdとすると、c>dで
あり、上記条溝に嵌まる当該相当部位の翼根の底部とそ
の条溝の底部との間に、動翼を上方位に押し上げるよう
にこれら両者間を弾発させる円筒状弾発材が介設され、
この円筒状弾発材の軸方向と上記条溝の条方向とは交叉
していることを特徴とする、回転機械の翼車装置。
The rotor blade has a blade root whose cross section is the same shape as the square-shaped groove, which is composed of an intermediate part with a narrow groove width, and a lower part and an upper part with a wide groove that continues in the radial direction on both sides of the intermediate part. In a blade wheel device of a rotating machine that is inserted and fitted along a groove, the height width in the radial direction of the intermediate portion of the groove is a,
If b is the height width in the radial direction of the corresponding part of the blade root that fits into the groove in the middle part, then a<b, and also, If the height width in the radial direction is C, and the height width in the radial direction of the corresponding part of the blade root that fits into this lower side part is d, then c>d, and the corresponding part that fits into the groove A cylindrical elastic material is interposed between the bottom of the blade root and the bottom of the groove of the part, and the elastic material is interposed between the two so as to push the rotor blade upward.
A blade wheel device for a rotating machine, characterized in that the axial direction of the cylindrical elastic material and the direction of the grooves intersect.
JP1978043121U 1978-03-31 1978-03-31 Rotating machine impeller device Expired JPS5918160Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1978043121U JPS5918160Y2 (en) 1978-03-31 1978-03-31 Rotating machine impeller device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1978043121U JPS5918160Y2 (en) 1978-03-31 1978-03-31 Rotating machine impeller device

Publications (2)

Publication Number Publication Date
JPS54145806U JPS54145806U (en) 1979-10-09
JPS5918160Y2 true JPS5918160Y2 (en) 1984-05-25

Family

ID=28916925

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1978043121U Expired JPS5918160Y2 (en) 1978-03-31 1978-03-31 Rotating machine impeller device

Country Status (1)

Country Link
JP (1) JPS5918160Y2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2386721A1 (en) * 2010-05-14 2011-11-16 Siemens Aktiengesellschaft Fastening assembly for blades of axial fluid flow turbo machines and procedure for producing the same
US9194238B2 (en) * 2012-11-28 2015-11-24 General Electric Company System for damping vibrations in a turbine

Also Published As

Publication number Publication date
JPS54145806U (en) 1979-10-09

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