JPS643761Y2 - - Google Patents
Info
- Publication number
- JPS643761Y2 JPS643761Y2 JP1983053457U JP5345783U JPS643761Y2 JP S643761 Y2 JPS643761 Y2 JP S643761Y2 JP 1983053457 U JP1983053457 U JP 1983053457U JP 5345783 U JP5345783 U JP 5345783U JP S643761 Y2 JPS643761 Y2 JP S643761Y2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- groove
- steam
- opening
- drain
- 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
Links
- 239000000463 material Substances 0.000 claims description 12
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 14
- 239000012530 fluid Substances 0.000 description 5
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Description
【考案の詳細な説明】
本考案は蒸気タービンの静翼等に関し、特に、
翼面から有効にドレンを除去しうる溝付静翼の改
良に関するものである。[Detailed description of the invention] The present invention relates to stator blades of steam turbines, etc., and in particular,
The present invention relates to an improvement in a grooved stationary blade that can effectively remove condensate from the blade surface.
一般に、タービン段落は、例えば高温高圧の蒸
気などの作動流体を静翼より流入させ、静翼によ
り作動流体の熱エネルギを速度エネルギに変換し
て高速の作動流体をつくり、そのエネルギを動翼
に当てて運動量の変化によつて生じる作動流体の
衝動作用又は衝動作用と反動作用を組合せて動翼
を回転させている。 Generally, in a turbine stage, a working fluid such as high-temperature, high-pressure steam flows in through stator vanes, and the stator vanes convert the thermal energy of the working fluid into velocity energy to create a high-speed working fluid, which is then transferred to the rotor blades. The rotor blades are rotated by an impulse action or a combination of an impulse action and a reaction action of the working fluid caused by a change in momentum.
ところで、第1図及び第2図に示されているよ
うに、従来の蒸気タービンの静翼1にはリング材
22が付設され、リング材2はケーシング(図示
せず)の所定位置に支持されている。 By the way, as shown in FIGS. 1 and 2, a ring material 22 is attached to the stationary blade 1 of a conventional steam turbine, and the ring material 2 is supported at a predetermined position of a casing (not shown). ing.
蒸気は静翼1に形成されている通路を通過して
から動翼(図示せず)に当り、動翼に回転を与え
るが、蒸気は上記蒸気通路を通過中に水滴とな
り、これが成長してその流速が低下し、静翼1で
は主としてその腹面に集積した微小水滴が翼表面
を主流方向に流れる水膜となつて翼後縁に集ま
り、ついには粗大水滴となつて再び蒸気主流に乗
り、次いで高速回転する動翼に衝突して、いわゆ
るドレンアタツク又はドレンエロージヨンを発生
する現象が生じる。 The steam passes through the passage formed in the stationary blade 1 and then hits the rotor blade (not shown), giving rotation to the rotor blade.While passing through the steam passage, the steam turns into water droplets, which grow. The flow velocity decreases, and in the stator blade 1, the minute water droplets that mainly accumulate on the ventral surface become a water film flowing in the mainstream direction on the blade surface, gather at the trailing edge of the blade, and finally become coarse water droplets that flow into the steam mainstream again. Then, the liquid collides with the rotor blades rotating at high speed, causing a phenomenon called drain attack or drain erosion.
上記エロージヨンを軽減するために、静翼表面
に集積した水膜の状態で、静翼からドレンを除去
する目的で、第1図及び第2図に示すように、翼
表面に溝3を設けることがある。溝3で集めめれ
た水膜は主流に対して直交ではなくやや傾斜した
方向に設けられている溝の配置によつて主流蒸気
から駆動力を受けて翼外周部に設けられたリング
材2の排出口4に集まり、ここから蒸気差圧を利
用してタービン段落外に排出される。 In order to reduce the above-mentioned erosion, grooves 3 are provided on the vane surface as shown in Figs. 1 and 2 for the purpose of removing condensate from the stator vane in the state of water film accumulated on the vane surface. There is. The water film collected in the groove 3 receives a driving force from the mainstream steam due to the arrangement of the groove, which is not perpendicular to the mainstream, but is slightly inclined, and is transferred to the ring material 2 provided on the outer periphery of the blade. The steam collects at the exhaust port 4, and is discharged from there to the outside of the turbine stage using the steam differential pressure.
しかしながら、上記従来の差付静翼には下記の
ような欠点があつた。 However, the above-mentioned conventional stator vanes have the following drawbacks.
(1) 溝3はある程度の深さを要するので、望まし
い場所である翼後縁付近ではなく、かなり上流
であつて、翼厚が充分厚い場所に設けなくては
ならない。それゆえ十分水膜を収集できないの
で、依然としてドレンアタツクが生じる。(1) Since the groove 3 requires a certain depth, it must be provided not near the trailing edge of the blade, which is a desirable location, but rather far upstream and in a location where the blade is sufficiently thick. Therefore, not enough water film can be collected, so drain attack still occurs.
(2) 溝3に集めた水膜を効果的に翼外周部に移動
させるためには、溝3の開口幅は充分大きいこ
とが必要であり、水膜厚さの数十倍の開口幅を
持つのが普通である。このため、翼プロフアイ
ル損失の増加が懸念される。(2) In order to effectively move the water film collected in the groove 3 to the outer circumference of the blade, the opening width of the groove 3 must be sufficiently large, and the opening width should be several tens of times the water film thickness. It is normal to have one. Therefore, there is a concern that the blade profile loss will increase.
(3) 溝3に集められた水膜の流れからみて、静翼
1の外周部に行く程、溝の断面積は大きくする
必要があり、リング材2が傾斜して配置されて
いる関係もあつて、外周部程溝3を深くするこ
とが困難である。また溝幅を変化させることも
上記(2)の理由から容易ではない。(3) In view of the flow of the water film collected in the groove 3, the cross-sectional area of the groove needs to increase toward the outer periphery of the stator blade 1, and the ring material 2 is arranged at an angle. Therefore, it is difficult to make the groove 3 deeper toward the outer periphery. Furthermore, it is not easy to change the groove width due to the reason (2) above.
本考案は、上記の欠点を改善するものであつ
て、その目的とするところは、翼面から有効にド
レンを除去しうる溝付静翼を提供することにあ
る。 The present invention aims to improve the above-mentioned drawbacks, and its purpose is to provide a grooved stationary blade that can effectively remove condensate from the blade surface.
上記目的を達成するために、本考案は、ドレン
排出用溝を翼材とは別個の薄板で形成し、翼面に
突起部を形成することなく溝の開口部を溝と分離
して設定しうるように構成したことを特徴とする
ものである。 In order to achieve the above object, the present invention forms the drain discharge groove with a thin plate separate from the blade material, and sets the opening of the groove separately from the groove without forming a protrusion on the blade surface. It is characterized by being constructed so that it can be wetted.
以下、本考案による蒸気タービンの静翼の実施
例を第3図及び第4図を参照して説明する。 Hereinafter, embodiments of a stator blade for a steam turbine according to the present invention will be described with reference to FIGS. 3 and 4.
第3図及び第4図において、静翼1の外周部に
はリング材2を付設し、また静翼1材料の後縁の
背面に別体の薄板11を接着し、同薄板11の一
端側であつて翼後縁前面側に他の薄板12を銀ロ
ウ等で接着部13を静翼後縁部に形成する。そし
て上記翼材の後縁前面と薄板12の接着部13の
端部と対向する他端との間に開口部14を形成す
る。これにより、薄板11,12の間には捕集さ
れたドレン移送通路となる溝16が形成される。
この溝16はリング材2に向つてのび、リング材
2に設けられた排出口4に連通している。 In FIGS. 3 and 4, a ring material 2 is attached to the outer periphery of the stator blade 1, and a separate thin plate 11 is glued to the back of the trailing edge of the stator blade 1 material, and one end of the thin plate 11 Another thin plate 12 is attached to the front side of the trailing edge of the blade, and an adhesive part 13 is formed on the trailing edge of the stationary blade using silver solder or the like. An opening 14 is formed between the front surface of the trailing edge of the wing material and the other end of the thin plate 12 opposite to the end of the bonded portion 13. As a result, a groove 16 is formed between the thin plates 11 and 12 to serve as a passage for transporting the collected drain.
This groove 16 extends toward the ring material 2 and communicates with a discharge port 4 provided in the ring material 2.
必要ならば薄板11,12の間に中間支持材1
5を設けることも可能である。 If necessary, an intermediate support 1 may be placed between the thin plates 11 and 12.
It is also possible to provide 5.
次に上記のように構成された溝付静翼の作用に
ついてのべると、静翼面に沿つて流れる水膜は開
口部14に集まる。ここで開口部14における蒸
気と排出口4付近との蒸気とでは、排出口4付近
の蒸気の方が低圧であるので、開口部14に集ま
つた水膜は溝16内に入り、溝16に沿つて流れ
てドレンとなり排出口4から排出される。 Next, regarding the function of the grooved stator vane configured as described above, the water film flowing along the stator vane surface gathers at the opening 14. Here, between the steam at the opening 14 and the steam near the outlet 4, the steam near the outlet 4 has a lower pressure, so the water film collected at the opening 14 enters the groove 16. It flows along the drain and becomes drain and is discharged from the discharge port 4.
上記のように構成したので下記のような効果を
奏する。 The configuration as described above provides the following effects.
(1) 薄板11,12により溝16を形成したの
で、溝開口部14は溝深さに関係なく充分静翼
の後端近傍に設定できる。(1) Since the groove 16 is formed by the thin plates 11 and 12, the groove opening 14 can be set sufficiently close to the rear end of the stator blade regardless of the groove depth.
(2) 開口部14を水膜厚さと同程度まで狭くする
ことができるので、溝16に比べて開口部14
の面積が充分小さくなり、従つて、排出用蒸気
差圧のもとになる排出口4の低圧力が溝16ま
で遡及することになり、水膜は、開口部14を
介して蒸気差圧により積極的に吸引されると共
に、従来、必要としていた主流に対する溝の傾
斜も不要となる。(2) Since the opening 14 can be made narrower to the same extent as the water film thickness, the opening 14 is narrower than the groove 16.
area becomes sufficiently small, and therefore, the low pressure at the outlet 4, which is the source of the differential steam pressure for discharging, will be traced back to the groove 16, and the water film will flow through the opening 14 due to the differential pressure of the steam. In addition to being actively sucked, there is no need to incline the groove with respect to the mainstream, which was required in the past.
(3) ドレン排出通路となる溝16は薄板11,1
2で形成されるので、溝16の選定は薄板1
1,12の選定により比較的自由に設定でき、
これにより開口部14は溝16と分離して独立
に設定できる。(3) The groove 16 which becomes the drain discharge passage is formed by the thin plates 11 and 1.
2, the groove 16 is selected from the thin plate 1.
You can set relatively freely by selecting 1 and 12,
Thereby, the opening 14 can be set separately and independently from the groove 16.
(4) ドレン排出部が翼面に対して突起しない構造
となるため、ドレン排出部が流体の流れを乱し
て静翼の性能低下をきたすことなくドレンを除
去できる。(4) Since the drain discharge part does not protrude from the blade surface, the drain discharge part can remove the drain without disturbing the fluid flow and reducing the performance of the stationary blade.
以上、説明したように、本考案によれば、静翼
の性能低下をきたすことなくドレンの排除を効果
的に行うことができ、ドレンアタツクが生じない
ので保守が軽減される。 As described above, according to the present invention, drain can be effectively removed without deteriorating the performance of the stator blade, and maintenance is reduced because drain attack does not occur.
その他、本考案は上記し、図面に示す蒸気ター
ビンによる実施例にのみ限定されるものではな
く、要旨を逸脱しない範囲内でガスタービン、等
回転機械に適宜変形して実施しうることは勿論で
ある。 In addition, the present invention is not limited to the embodiment using the steam turbine described above and shown in the drawings, but can of course be implemented by appropriately modifying it to a gas turbine or a rotating machine without departing from the scope of the invention. be.
第1図は従来の蒸気タービンの静翼の正面図、
第2図は第1図の−矢視方向切断断面図、第
3図は本考案の蒸気タービンの静翼の正面図、第
4図は第3図の−矢視方向切断断面図であ
る。
1……静翼、2……リング材、4……排出口、
11,12……薄板、13……接着部、14……
開口部、15……中間支持材、16……溝。
Figure 1 is a front view of a conventional steam turbine stationary blade.
2 is a sectional view taken in the - arrow direction of FIG. 1, FIG. 3 is a front view of a stationary blade of the steam turbine of the present invention, and FIG. 4 is a sectional view taken in the - arrow direction of FIG. 3. 1... Stationary blade, 2... Ring material, 4... Discharge port,
11, 12...Thin plate, 13...Adhesive part, 14...
Opening portion, 15... intermediate support member, 16... groove.
Claims (1)
て、前記溝を翼材と別個の薄板で形成し、翼面に
突起部を形成することなく前記溝の開口部を前記
溝と独立に設定しうることを特徴とする溝付静
翼。 In a stationary blade with a drain discharge groove provided on the trailing edge of the blade, the groove is formed of a thin plate separate from the blade material, and the opening of the groove is set independently of the groove without forming a protrusion on the blade surface. A grooved stator blade that is characterized by the ability to
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5345783U JPS59159702U (en) | 1983-04-12 | 1983-04-12 | Grooved stationary blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5345783U JPS59159702U (en) | 1983-04-12 | 1983-04-12 | Grooved stationary blade |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS59159702U JPS59159702U (en) | 1984-10-26 |
JPS643761Y2 true JPS643761Y2 (en) | 1989-02-01 |
Family
ID=30183801
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP5345783U Granted JPS59159702U (en) | 1983-04-12 | 1983-04-12 | Grooved stationary blade |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59159702U (en) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4422806Y1 (en) * | 1966-03-11 | 1969-09-26 |
-
1983
- 1983-04-12 JP JP5345783U patent/JPS59159702U/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4422806Y1 (en) * | 1966-03-11 | 1969-09-26 |
Also Published As
Publication number | Publication date |
---|---|
JPS59159702U (en) | 1984-10-26 |
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