JPS58176404A - Drain removing device - Google Patents

Drain removing device

Info

Publication number
JPS58176404A
JPS58176404A JP5734082A JP5734082A JPS58176404A JP S58176404 A JPS58176404 A JP S58176404A JP 5734082 A JP5734082 A JP 5734082A JP 5734082 A JP5734082 A JP 5734082A JP S58176404 A JPS58176404 A JP S58176404A
Authority
JP
Japan
Prior art keywords
drain
groove
lid
gutter
stationary blade
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
Application number
JP5734082A
Other languages
Japanese (ja)
Inventor
Masatoshi Shimakita
嶋北 正俊
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP5734082A priority Critical patent/JPS58176404A/en
Publication of JPS58176404A publication Critical patent/JPS58176404A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32Collecting of condensation water; Drainage ; Removing solid particles

Abstract

PURPOSE:To improve a drain removing effect, by mounting a lid such as a porous plate,a wire gauze and the like on a drain removing gutter defined in a web of a stationary blade of steam turbine and by properly selecting an opening amount of the lid. CONSTITUTION:A lid 5 constituted by a porous plate, a wire gauze or a slit plate for forming a fluid channel is mounted on a drain gutter 3 defined in the web of the stationary blade of a turbine 1. The gutter 3 communicates with a discharge outlet 4 and receives a low pressure of a condenser and the like. Moreover, a resistance imposed by a porous plate and the like during its passage is distributed in predetermined values by properly selecting an opening amount of the lid 5 relative to a radial direction. In this manner, since a low pressure of a condenser and the like affects upon an entire length of drain removing gutter 3,a drain removing effect can be improved.

Description

【発明の詳細な説明】 本発明はドレン除去装置に関するものであり、更に詳細
には、タービン静翼のドレン排出溝の改良に関するもの
である。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a drain removal device, and more particularly to an improvement in a drain discharge groove of a turbine stationary blade.

蒸気タービンの低圧段等湿り蒸気中で作動するターボ機
械では、翼の効率を向上させ、タービン内各部、特に翼
の入口縁の浸食を防止するために。
In turbomachinery that operates in humid steam, such as the low-pressure stage of a steam turbine, it is used to improve the efficiency of the blades and to prevent erosion of various parts within the turbine, especially the inlet edges of the blades.

発生したドレン(湿分)を効果的に作動流体から分離排
出することが重要である。作動流体中に発生しだ液滴粒
子(ドレン)は通常タービン静翼の腹面に集積し、静翼
腹面に薄い液膜を形成して主蒸気流に引きずられて翼後
縁付近に移動してい(。
It is important to effectively separate and discharge the generated condensate (moisture) from the working fluid. Droplet particles (drain) generated in the working fluid usually accumulate on the ventral surface of the turbine stator blade, form a thin liquid film on the ventral surface of the stator blade, and are dragged by the main steam flow and moved to the vicinity of the trailing edge of the blade. (.

上記の現象に着目して湿分の除去を行うものに、従来か
ら「溝付静翼」がある。即ち第1、第2図にその構成を
示す。静翼(1)は内径側(翼根)と外径側(翼端)で
静翼環(2)に溶接等の方法で接合固定されている。そ
して静翼(1)の腹面に溝(3)を設け、ここに溜った
液滴塊を翼端に設けられた抜出口(4)を通じてコンデ
ンサ等の低圧を利用して翼表面から除去している。この
とき、溝(3)は主流に対して直交方向からやや傾くよ
うに設けられ、主流の剪断成分がドレンの排出作用をも
つように構成されている。
Grooved stator vanes have traditionally been used to remove moisture by focusing on the above phenomenon. That is, the configuration is shown in FIGS. 1 and 2. The stator blade (1) is fixed to the stator blade ring (2) by welding or the like on the inner diameter side (blade root) and the outer diameter side (blade tip). Then, a groove (3) is provided on the ventral surface of the stationary blade (1), and the droplet mass accumulated there is removed from the blade surface using low pressure from a condenser etc. through an extraction port (4) provided at the blade tip. There is. At this time, the groove (3) is provided so as to be slightly inclined from the direction perpendicular to the mainstream, so that the shear component of the mainstream has a draining effect.

上記静翼溝(3)は主蒸気流に対して開口しており、こ
のための抜出口(4)を通じて導入された低圧も溝(3
)の翼端部付近にしか作用しない。従って静翼の翼高さ
方向に長(設けた溝(3)もドレン除去に有効に作用せ
ず、溝(3)に蓄積した液膜は溝(3)からあふれて再
び主流中に飛散することがある。
The stationary blade groove (3) is open to the main steam flow, and the low pressure introduced through the outlet (4) for this purpose is also opened to the groove (3).
) only acts near the wing tips. Therefore, the groove (3), which is long in the height direction of the stator blade, does not effectively remove the drain, and the liquid film accumulated in the groove (3) overflows from the groove (3) and scatters into the mainstream again. Sometimes.

本発明は、上記のような従来のタービン静翼におけるド
レン排出上の欠点を解決するものであり、タービン静翼
に設けたドレン排出口のドレン排出能力を向上させるこ
とを目的とするものである。
The present invention solves the above-mentioned disadvantages in drain discharge in conventional turbine stator blades, and aims to improve the drain discharge ability of the drain outlet provided in the turbine stator blades. .

上記目的を達成するために、本発明においてはタービン
静翼の腹面に設けたドレン排出溝に多孔板、金網等の溝
蓋な設け、その開口比をドレン排出溝の長手方向に適当
に定めるものである。上記のような構成にすることによ
って、ドレン排出溝の長手方向に一様の吸引力が作用し
て、ドレン排出溝全長にわたってドレン排出力が生じる
のである。
In order to achieve the above object, in the present invention, a drain discharge groove provided on the ventral surface of a turbine stator blade is provided with a groove cover such as a perforated plate or a wire mesh, and the opening ratio of the groove cover is appropriately determined in the longitudinal direction of the drain discharge groove. It is. With the above structure, a uniform suction force acts in the longitudinal direction of the drain groove, and a drain discharge force is generated over the entire length of the drain groove.

本発明の実施例を図面と共に説明する。Embodiments of the present invention will be described with reference to the drawings.

第3図に示す第1実施例において、タービン静翼(1)
の腹面に設けたドレン排出溝(3)に、流体通路になる
多孔板、金網又はスリット板で構成された溝蓋(5)を
設ける。上記溝(3)は勿論、第1図に示すような排出
口(4)に通じており、コンデンサ等の低圧を作用させ
るものである。このような構成により、多孔板等の吸込
抵抗を利用して排出口から導入されるコンデンサ等の低
圧をドレン排出溝(3)の全長にわたって利用できる。
In the first embodiment shown in FIG. 3, a turbine stationary blade (1)
A drain groove (3) provided on the ventral surface of the drain groove (3) is provided with a groove cover (5) made of a perforated plate, wire mesh, or slit plate to serve as a fluid passage. The groove (3) is, of course, connected to an outlet (4) as shown in FIG. 1, which is used to apply a low pressure such as a condenser. With this configuration, the low pressure of a condenser or the like introduced from the outlet can be utilized over the entire length of the drain outlet (3) by utilizing the suction resistance of the perforated plate or the like.

更に上記溝蓋(5)の開口率を半径方向に対応して適当
に定めることにより、半径位置に対応して多孔板等の通
過抵抗値を所要の値に分布させることが可能になり、こ
の結果、主流によって定まる半径位置の圧力勾配に合致
させて、抵抗値の配分を行うことができるので、静翼溝
(3)をその全長にわたってドレン除去に活用すること
が可能になる。
Furthermore, by appropriately determining the aperture ratio of the groove cover (5) corresponding to the radial direction, it becomes possible to distribute the passage resistance value of the perforated plate etc. to a required value corresponding to the radial position. As a result, the resistance value can be distributed in accordance with the pressure gradient at the radial position determined by the main flow, so that the stationary blade groove (3) can be utilized for drain removal over its entire length.

第4図に示す第2実施例においては、多孔板(6)に液
溜り作用を持たせるように、タービン静翼の腹面に設け
たドレン排出溝(3)の内方に向って、多孔板(6)の
一端を傾斜させるような形状にする。上記のような多孔
板の形状にすることにより、多孔板の吸込抵抗を利用す
ると共に多孔板(6)の低い方にドレンが溜り、第3図
の第1実施例と同様にドレン排出溝(3)に連通してい
る排出口から導入されるコンデンサ等の低圧がドレン排
出溝(3)の全長にわたって作用するので、更にドレン
除去効果を向上させることができる。
In the second embodiment shown in FIG. 4, the perforated plate (6) is arranged inwardly of the drain discharge groove (3) provided on the ventral surface of the turbine stationary blade so that the perforated plate (6) has a liquid pooling effect. (6) Shape one end to be inclined. By making the perforated plate into the shape described above, the suction resistance of the perforated plate is utilized, and the drain accumulates in the lower part of the perforated plate (6), and the drain discharge groove ( Since the low pressure of a condenser or the like introduced from the discharge port communicating with drain drain groove (3) acts over the entire length of the drain drain groove (3), the drain removal effect can be further improved.

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

第1図は従来のタービン静翼の正面図、第2図は第1図
の■−■線に沿った断面図、第3図は本発明の第1実施
例を示すタービン静翼の一部断面図、第4図は本発明の
第2実施例を示すタービン静翼の一部断面図である。 1・・タービン静翼、2・・静翼環、3・・ドレン排出
溝、4・・排出口、5・・溝蓋。
Fig. 1 is a front view of a conventional turbine stator blade, Fig. 2 is a sectional view taken along the line ■-■ in Fig. 1, and Fig. 3 is a part of a turbine stator blade showing the first embodiment of the present invention. 4 is a partial sectional view of a turbine stator blade showing a second embodiment of the present invention. 1. Turbine stationary blade, 2. Stationary blade ring, 3. Drain discharge groove, 4. Discharge port, 5. Groove cover.

Claims (1)

【特許請求の範囲】[Claims] タービン静翼の腹面に設けられたドレン排出溝に、流体
通路を有する溝蓋な設けたことを特徴とするドレン除去
装置。
A drain removal device characterized in that a drain discharge groove provided on the ventral surface of a turbine stationary blade is provided with a groove cover having a fluid passage.
JP5734082A 1982-04-08 1982-04-08 Drain removing device Pending JPS58176404A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5734082A JPS58176404A (en) 1982-04-08 1982-04-08 Drain removing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5734082A JPS58176404A (en) 1982-04-08 1982-04-08 Drain removing device

Publications (1)

Publication Number Publication Date
JPS58176404A true JPS58176404A (en) 1983-10-15

Family

ID=13052834

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5734082A Pending JPS58176404A (en) 1982-04-08 1982-04-08 Drain removing device

Country Status (1)

Country Link
JP (1) JPS58176404A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62190803U (en) * 1986-05-23 1987-12-04
EP0726384A1 (en) * 1995-02-13 1996-08-14 Abb Research Ltd. Stator blade for steam turbines
EP0863296A3 (en) * 1997-03-08 2001-03-21 Abb Research Ltd. Guide vane for steam turbines
US6474942B2 (en) * 2000-01-03 2002-11-05 General Electric Company Airfoil configured for moisture removal from steam turbine flow path
GB2424454A (en) * 2005-03-24 2006-09-27 Alstom Technology Ltd Water extracting turbine stator blade
EP1744018A1 (en) * 2005-07-15 2007-01-17 Kabushiki Kaisha Toshiba Steam turbine nozzle vane, nozzle rings and method of fabricating the vane
JP2015031185A (en) * 2013-08-01 2015-02-16 三菱日立パワーシステムズ株式会社 Moisture separator of steam turbine and steam turbine stator vane

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5120322U (en) * 1974-07-31 1976-02-14

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5120322U (en) * 1974-07-31 1976-02-14

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62190803U (en) * 1986-05-23 1987-12-04
EP0726384A1 (en) * 1995-02-13 1996-08-14 Abb Research Ltd. Stator blade for steam turbines
EP0863296A3 (en) * 1997-03-08 2001-03-21 Abb Research Ltd. Guide vane for steam turbines
US6474942B2 (en) * 2000-01-03 2002-11-05 General Electric Company Airfoil configured for moisture removal from steam turbine flow path
GB2424454A (en) * 2005-03-24 2006-09-27 Alstom Technology Ltd Water extracting turbine stator blade
EP1744018A1 (en) * 2005-07-15 2007-01-17 Kabushiki Kaisha Toshiba Steam turbine nozzle vane, nozzle rings and method of fabricating the vane
JP2015031185A (en) * 2013-08-01 2015-02-16 三菱日立パワーシステムズ株式会社 Moisture separator of steam turbine and steam turbine stator vane
EP2832954A3 (en) * 2013-08-01 2015-05-06 Mitsubishi Hitachi Power Systems, Ltd. Moisture separator unit for steam turbine and steam-turbine stationary blade
US9745866B2 (en) 2013-08-01 2017-08-29 Mitsubishi Hitachi Power Systems, Ltd. Moisture separator unit for steam turbine and steam-turbine stationary blade

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