JP2000297605A - Movable blade fastening device on fluid machine - Google Patents
Movable blade fastening device on fluid machineInfo
- Publication number
- JP2000297605A JP2000297605A JP11103774A JP10377499A JP2000297605A JP 2000297605 A JP2000297605 A JP 2000297605A JP 11103774 A JP11103774 A JP 11103774A JP 10377499 A JP10377499 A JP 10377499A JP 2000297605 A JP2000297605 A JP 2000297605A
- Authority
- JP
- Japan
- Prior art keywords
- wheel
- dovetail
- hole
- moving blade
- steel ball
- 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
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、蒸気タービン,ガ
スタービン,軸流圧縮機等の流体機械に使用されている
動翼をホイールに固定するための固定装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fixing device for fixing a moving blade used in a fluid machine such as a steam turbine, a gas turbine, and an axial compressor to a wheel.
【0002】[0002]
【従来の技術】一般的な動翼の軸方向固定装置として
は、動翼とホイールとの溝部はめ合い面に板を挟め、動
翼を挿入後両端を折り曲げて固定する装置が実開平4−1
19392 号に提案されている。2. Description of the Related Art As a general moving blade fixing device in the axial direction, a device for fixing a plate by sandwiching a plate on a groove fitting surface between a moving blade and a wheel, inserting the moving blade, and bending both ends thereof is known. 1
Proposed in 19392.
【0003】または、動翼ダブテイル底部にテーパピン
を用いて固定する装置が特開昭62−55402 号に提案され
ている。[0003] Alternatively, an apparatus for fixing the rotor blade dovetail to the bottom using a taper pin has been proposed in Japanese Patent Application Laid-Open No. Sho 62-55402.
【0004】更に、簡単な固定方法としては、動翼ダブ
テイルが挿入される付近のホイールをかしめることによ
って固定されている。Further, as a simple fixing method, the rotor blade is fixed by caulking a wheel near a blade dovetail.
【0005】[0005]
【発明が解決しようとする課題】前記実開平4−119392
号の固定装置にあっては、ホイール両端面と板との間
に、板折り曲げ加工時できるR部によって隙間が発生
し、タービン運転時の動翼のガタとなり問題がある。SUMMARY OF THE INVENTION
In the fixing device for the wheel, there is a problem that a gap is generated between the both end surfaces of the wheel and the plate due to the R portion that can be formed at the time of plate bending, which causes play of the moving blade during turbine operation.
【0006】また、前記特開昭62−55402 号の固定装置
にあっては、テーパピン長さがホイール間隔以上になる
と組立不可能となる問題がある。Further, the fixing device disclosed in Japanese Patent Application Laid-Open No. 62-55402 has a problem that if the length of the taper pin is longer than the wheel interval, it becomes impossible to assemble.
【0007】更に、前記ホイールをかしめることによる
固定は、分解の時にホイールかしめ部を削ってしまうた
め強度上の問題がある。Further, the fixing by caulking the wheel has a problem in strength because the caulked portion of the wheel is shaved during disassembly.
【0008】本発明の目的は、これらの点に考慮し運転
状態に於けるホイールと動翼を軸方向位置を高強度で確
実な固定が行え、加工が容易で少スペースとなる固定装
置を提供することにある。SUMMARY OF THE INVENTION An object of the present invention is to provide a fixing device in which the axial position of a wheel and a moving blade in an operating state can be securely fixed with high strength in an operating state in consideration of these points, and the machining is easy and requires a small space. Is to do.
【0009】[0009]
【課題を解決するための手段】本発明は、動翼ダブテイ
ル部に軸方向横穴と、この軸穴につながるホイール中心
に向かいダブテイル底部から貫通する縦穴を加工し、ホ
イールにはダブテイル底部から突き抜ける縦穴と組立時
に同位置となる半球状の溝を加工し、更に動翼とホイー
ルを組立後、動翼に加工した横穴から鋼球を挿入し、縦
穴を通してホイール溝部に鋼球を挿入することによっ
て、動翼ダブテイル底部とホイールの合わせ目に鋼球を
挿入した後、動翼ダブデイル部横穴にノックピンを挿入
し動翼ダブテイル底部とホイールの合わせ目に鋼球を固
定することによって、運転状態に於ける動翼とホイール
の軸方向位置を固定する。SUMMARY OF THE INVENTION According to the present invention, there is provided a blade dovetail portion having an axial lateral hole and a vertical hole penetrating from the dovetail bottom toward the center of the wheel connected to the axial hole, and the wheel has a vertical hole penetrating from the dovetail bottom. By processing the hemispherical groove that will be in the same position at the time of assembly and further assembling the moving blade and the wheel, inserting a steel ball from the horizontal hole processed into the moving blade, and inserting a steel ball into the wheel groove through the vertical hole, After inserting a steel ball at the joint between the rotor blade dovetail bottom and the wheel, insert a knock pin into the side hole of the rotor blade dovetail section, and fix the steel ball at the joint between the rotor blade dovetail bottom and the wheel. Fix the axial position of the bucket and wheel.
【0010】[0010]
【発明の実施の形態】以下に本発明の実施例を詳細に説
明する。図1は、動翼3とホイール1の結合部を一部断
面して示した図であり、ホイール1に設けられた軸方向
のダブテイル溝8に丁度はまり合う形状のダブテイル9
を動翼3基部に形成し、両者をはめ合うことで結合して
いる。動翼3がホイール1に差し込まれた状態を維持す
るために、動翼3とホイール1に固定装置が設けられ
る。DESCRIPTION OF THE PREFERRED EMBODIMENTS The embodiments of the present invention will be described below in detail. FIG. 1 is a partial cross-sectional view of a connecting portion between the rotor blade 3 and the wheel 1, and a dovetail 9 having a shape just fitted into an axial dovetail groove 8 provided in the wheel 1.
Are formed at the bases of the three moving blades, and they are joined by fitting each other. In order to keep the moving blade 3 inserted into the wheel 1, a fixing device is provided to the moving blade 3 and the wheel 1.
【0011】図4に動翼側固定装置を示し、動翼3には
予めダブテイル9端面からホイール1の軸方向に向かう
横穴5と横穴5から動翼3のダブテイル9底面まで貫通
する縦穴4を穿ける。横穴5と縦穴4は後に示す鋼球6
がスムーズに通り、かつ大きすぎない穴径とする。FIG. 4 shows a moving blade side fixing device. The moving blade 3 is provided with a horizontal hole 5 extending from the end face of the dovetail 9 in the axial direction of the wheel 1 and a vertical hole 4 penetrating from the horizontal hole 5 to the bottom of the dovetail 9 of the moving blade 3. I can. The horizontal hole 5 and the vertical hole 4 are steel balls 6 shown later.
Pass smoothly, and the hole diameter should not be too large.
【0012】また、横穴5と縦穴4の中心線が交わるホ
イール1の軸方向位置に於いて、縦穴4のダブテイル9
底面からの高さが、鋼球6の半径と等しくなるものとす
る。更に、横穴5は前記横穴5と縦穴4の中心線が交わ
るホイール1の軸方向位置に於いて、前記縦穴4の高さ
条件を満たす位置に穿ける。Further, at the axial position of the wheel 1 where the center line of the horizontal hole 5 and the vertical hole 4 intersect, the dovetail 9 of the vertical hole 4
It is assumed that the height from the bottom surface is equal to the radius of the steel ball 6. Further, the horizontal hole 5 can be drilled at a position satisfying the height condition of the vertical hole 4 at the axial position of the wheel 1 where the center line of the horizontal hole 5 and the vertical hole 4 intersect.
【0013】図7にホイール側固定装置を示し、ホイー
ル1のダブテイル溝8部上面に予め前記動翼3の横穴5
と縦穴4の中心線が交わるホイール1の軸方向位置にホ
イール1中心に向かう半球状の溝2を穿ける。FIG. 7 shows a wheel-side fixing device, in which a lateral hole 5 of the rotor blade 3 is previously provided on the upper surface of the dovetail groove 8 of the wheel 1.
A hemispherical groove 2 extending toward the center of the wheel 1 is formed at an axial position of the wheel 1 where the center line of the vertical hole 4 intersects with the center line of the wheel 1.
【0014】半球状の溝2は流体機械の運転状態に於い
て、動翼3のダブテイル9底部に中心があり、鋼球6の
径と等しい径を持つ溝とする。The hemispherical groove 2 has a center at the bottom of the dovetail 9 of the moving blade 3 and has a diameter equal to the diameter of the steel ball 6 in the operating state of the fluid machine.
【0015】ホイール1と動翼3を組立後、縦穴4がホ
イール1の真上に来る位置にホイールを回転させ、横穴
5から鋼球6を挿入し、縦穴4から動翼3のダブテイル
9底面に落とすことによって、鋼球6は半球状の溝2に
納まる。After assembling the wheel 1 and the rotor blade 3, the wheel is rotated so that the vertical hole 4 is located directly above the wheel 1, a steel ball 6 is inserted from the horizontal hole 5, and the dovetail 9 of the rotor blade 3 is inserted from the vertical hole 4 to the bottom surface. , The steel ball 6 fits into the hemispherical groove 2.
【0016】更に、横穴5と同径で、横穴5のある動翼
3のダブテイル9端面から、前記動翼3の横穴5と縦穴
4の中心線が交わるホイール1の軸方向位置までの距離
より長く、横穴5の全長にほぼ等しいノックピン7を横
穴に挿入し、動翼3のダブテイル9端面をかしめること
によって固定する。ここで、分解時を考慮してノックピ
ン7の端面は予めねじ穴を加工しておく。Further, the distance from the end face of the dovetail 9 of the rotor blade 3 having the same diameter as the horizontal hole 5 and having the horizontal hole 5 to the axial position of the wheel 1 where the center line of the horizontal hole 5 and the vertical hole 4 of the rotor blade 3 intersects. A long dowel pin 7 approximately equal to the entire length of the lateral hole 5 is inserted into the lateral hole, and the dovetail 9 end face of the bucket 3 is fixed by caulking. Here, a screw hole is formed in advance on the end face of the knock pin 7 in consideration of disassembly.
【0017】以上により、運転状態に於いてホイール1
と動翼3は鋼球6によって軸方向位置が固定される。As described above, the wheel 1 in the driving state
And the rotor blades 3 have their axial positions fixed by steel balls 6.
【0018】また、ホイール1と動翼3の分解時には、
動翼3のダブテイル9端面のかしめ部分を削り、ノック
ピン7を前記ねじ穴を利用し抜き取る。When disassembling the wheel 1 and the rotor blade 3,
The swaged portion of the end face of the dovetail 9 of the rotor blade 3 is shaved, and the knock pin 7 is pulled out using the screw hole.
【0019】更に、縦穴4がホイール1の真下に来るよ
うホイール1を回転させる。これにより鋼球6は半球状
の溝2から縦穴4を通って横穴5まで抜け、ホイール1
から動翼3を外すことが出来る。Further, the wheel 1 is rotated so that the vertical hole 4 is directly below the wheel 1. As a result, the steel ball 6 comes out of the hemispherical groove 2 through the vertical hole 4 to the horizontal hole 5, and the wheel 1
Can be removed from the moving blade 3.
【0020】他の実施例として、縦穴4,横穴5をホイ
ール1を穿け、半球状の溝2の動翼3のダブテイル9底
部に穿けることによっても本構造は可能である。As another embodiment, this structure is also possible by drilling the vertical hole 4 and the horizontal hole 5 in the wheel 1 and drilling the hemispherical groove 2 at the bottom of the dovetail 9 of the bucket 3.
【0021】また、前記ホイール1のダブテイル溝8に
設ける半球状の溝2を前記中心位置を基準に、ホイール
軸方向と直角方向に伸し横長の溝にすることにより、ホ
イール溝直角方向に余裕を持たせ、組立作業を容易にす
ることが可能である。Further, the hemispherical groove 2 provided in the dovetail groove 8 of the wheel 1 is extended in a direction perpendicular to the wheel axis direction with respect to the center position as a laterally elongated groove, so that a margin is provided in a direction perpendicular to the wheel groove. To facilitate the assembly operation.
【0022】更に、前記ホイール1のダブテイル溝8に
設ける判球状の溝2は、ドリル先端で加工することによ
り出来る円錐形状の溝に変更し、加工作業を簡素化する
ことが可能である。Furthermore, the spherical groove 2 provided in the dovetail groove 8 of the wheel 1 can be changed to a conical groove formed by processing with a drill tip, thereby simplifying the processing operation.
【0023】本発明による固定装置は、運転状態に於い
て、ホイール1の軸方向長さを越えることなく、ホイー
ル1の前後段落との間隔がノックピン7の長さ以上あれ
ば組立可能である。The fixing device according to the present invention can be assembled without exceeding the axial length of the wheel 1 if the distance between the front and rear sections of the wheel 1 is longer than the length of the knock pin 7 in the operating state.
【0024】[0024]
【発明の効果】以上述べたように本発明によれば、従来
形固定装置に比べてホイールの軸方向スペースをより節
約できる。As described above, according to the present invention, the axial space of the wheel can be further reduced as compared with the conventional fixing device.
【0025】即ち、動翼に作用する軸方向力に対しては
鋼球の剪断強さ相当まで耐えることができるためダブテ
イル溝上部の限られたスペース内に収まる充分小さな鋼
球径で必要な軸方向力に耐えることができる。このため
従来形のように、軸方向固定のための軸方向の余長スペ
ースを必要としない。That is, since the axial force acting on the rotor blade can withstand the shear strength of the steel ball, it is necessary to use a shaft having a sufficiently small steel ball diameter that can be accommodated in the limited space above the dovetail groove. Can withstand directional forces. Therefore, unlike the conventional type, there is no need for an extra axial space for fixing in the axial direction.
【0026】また、従来形固定装置に比べてより構造が
単純で製作・組立が容易である。Further, the structure is simpler than that of the conventional fixing device, and it is easy to manufacture and assemble.
【図1】本発明の全体構造を示す断面図。FIG. 1 is a sectional view showing the entire structure of the present invention.
【図2】図1のII−II線に沿う断面図。FIG. 2 is a sectional view taken along the line II-II in FIG.
【図3】図1の矢印A方向から見た側面図。FIG. 3 is a side view seen from the direction of arrow A in FIG. 1;
【図4】動翼の正面図。FIG. 4 is a front view of a moving blade.
【図5】図4のV−V線に沿う断面図。FIG. 5 is a sectional view taken along the line VV in FIG. 4;
【図6】図4の矢印B方向から見た側面図。FIG. 6 is a side view as seen from the direction of arrow B in FIG. 4;
【図7】ホイールの断面図。FIG. 7 is a sectional view of a wheel.
【図8】ホイールの平面図。FIG. 8 is a plan view of a wheel.
【図9】図7の矢印C方向から見た側面図。FIG. 9 is a side view as seen from the direction of arrow C in FIG. 7;
1…ホイール、2…半球状の溝、3…動翼、4…縦穴、
5…横穴、6…鋼球、7…ノックピン、8…ダブテイル
溝、9…ダブテイル。1 ... wheel, 2 ... hemispherical groove, 3 ... rotor blade, 4 ... vertical hole,
5 ... side hole, 6 ... steel ball, 7 ... knock pin, 8 ... dovetail groove, 9 ... dovetail.
───────────────────────────────────────────────────── フロントページの続き (72)発明者 小堀 充夫 茨城県日立市幸町三丁目2番2号 株式会 社日立エンジニアリングサービス内 Fターム(参考) 3G002 FA04 FA08 FA10 FA11 FB02 FB06 ────────────────────────────────────────────────── ─── Continued on the front page (72) Inventor Mitsuo Kobori 3-2-2, Sachimachi, Hitachi-shi, Ibaraki F-term in Hitachi Engineering Services Co., Ltd. (Reference) 3G002 FA04 FA08 FA10 FA11 FB02 FB06
Claims (4)
ダブテイル溝に軸方向から挿入して、ホイールに動翼を
取付ける構造に於いて、前記動翼のダブテイル部に軸方
向端面から軸方向に伸びる横穴と、これにつながりホイ
ールと動翼の組立時にホイール中心に向かいダブテイル
底面まで貫通した縦穴を設け、且つホイールと動翼の組
立時に前記縦穴と同芯に中心線を持つ溝を前記ダブテイ
ル溝上面に設け、ホイールに動翼を挿入後、前記横穴か
ら前記縦穴を介し前記ダブテイル溝に設けた溝に鋼球を
挿入した後、前記横穴にノックピンを挿入することによ
って、運転状態に於けるホイールと動翼の軸方向位置を
固定する固定装置。1. A structure in which a dovetail of a moving blade is axially inserted into a dovetail groove provided in a wheel and a moving blade is mounted on the wheel, wherein the dovetail portion of the moving blade is axially inserted from an axial end face. The dovetail groove is provided with a lateral hole extending therethrough and a longitudinal hole connected therewith and penetrating to the center of the wheel to the bottom of the dovetail when assembling the wheel and the moving blade, and having a center line concentric with the longitudinal hole when assembling the wheel and the moving blade. After the blade is inserted into the wheel, the blade is inserted into the wheel, the steel ball is inserted into the groove provided in the dovetail groove from the lateral hole through the vertical hole, and then the knock pin is inserted into the lateral hole, whereby the wheel in an operating state is obtained. A fixing device that fixes the axial position of the rotor and blade.
境界面が前記鋼球の中心を通るように溝の深さを設定し
た、ホイールと動翼の軸方向位置を固定する固定装置。2. The fixing device according to claim 1, wherein the depth of the groove is set so that the boundary surface between the moving blade and the wheel passes through the center of the steel ball, and the axial position of the wheel and the moving blade is fixed. apparatus.
イール側面に設け、前記動翼ダブテイルに溝を設けるこ
とにより請求項1と同等の機能を得る固定装置。3. The fixing device according to claim 1, wherein the horizontal hole and the vertical hole are provided in a side surface of the wheel, and the bucket dovetail is provided with a groove to achieve the same function as in the first embodiment.
ックス,Ni基合金及びCo基合金等、鋼球と同等又は
それ以上の機械的強度を有する材質とした、ホイールと
動翼の軸方向位置を固定する固定装置。4. A wheel and a moving blade according to claim 1, wherein said steel ball is made of a material having a mechanical strength equal to or higher than that of the steel ball, such as ceramics, Ni-based alloy and Co-based alloy. A fixing device that fixes the axial position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11103774A JP2000297605A (en) | 1999-04-12 | 1999-04-12 | Movable blade fastening device on fluid machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11103774A JP2000297605A (en) | 1999-04-12 | 1999-04-12 | Movable blade fastening device on fluid machine |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2000297605A true JP2000297605A (en) | 2000-10-24 |
Family
ID=14362804
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11103774A Pending JP2000297605A (en) | 1999-04-12 | 1999-04-12 | Movable blade fastening device on fluid machine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2000297605A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1728972A3 (en) * | 2005-05-31 | 2011-05-04 | Rolls-Royce Deutschland Ltd & Co KG | Blocking element for a turbine blade |
JP2012172555A (en) * | 2011-02-18 | 2012-09-10 | Hitachi Ltd | Turbine rotor |
-
1999
- 1999-04-12 JP JP11103774A patent/JP2000297605A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1728972A3 (en) * | 2005-05-31 | 2011-05-04 | Rolls-Royce Deutschland Ltd & Co KG | Blocking element for a turbine blade |
JP2012172555A (en) * | 2011-02-18 | 2012-09-10 | Hitachi Ltd | Turbine rotor |
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