JPS60153478A - Runner vane for propeller turbine - Google Patents
Runner vane for propeller turbineInfo
- Publication number
- JPS60153478A JPS60153478A JP59008848A JP884884A JPS60153478A JP S60153478 A JPS60153478 A JP S60153478A JP 59008848 A JP59008848 A JP 59008848A JP 884884 A JP884884 A JP 884884A JP S60153478 A JPS60153478 A JP S60153478A
- Authority
- JP
- Japan
- Prior art keywords
- runner
- runner vane
- blade
- face
- outercircumferential
- 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
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/04—Machines or engines of reaction type; Parts or details peculiar thereto with substantially axial flow throughout rotors, e.g. propeller turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B11/00—Parts or details not provided for in, or of interest apart from, the preceding groups, e.g. wear-protection couplings, between turbine and generator
- F03B11/04—Parts or details not provided for in, or of interest apart from, the preceding groups, e.g. wear-protection couplings, between turbine and generator for diminishing cavitation or vibration, e.g. balancing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Hydraulic Turbines (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の属する技術分野〕
本発明は断面翼形の板状体きして形成されたプロペラ水
車のランナ羽根に関し、#ランチ羽根の高圧面側から低
圧面側への流水の漏れ流れを抑制するようにしたもので
ある。[Detailed description of the invention] [Technical field to which the invention pertains] The present invention relates to a runner blade for a propeller water turbine formed by a plate-shaped body having an airfoil cross section. This is designed to suppress the leakage of running water.
一般に、プロペラ水車は約90m以下の低落差に適用さ
れる高比速度形水車で、立て軸構造のものと横軸構造の
ものとがある。立て軸構造のものは、約20m以上の落
差では7ランシス水車と同様なうず巻ケーシングが用い
られ、約20m以下の落差では半うず巻ケーシングが用
いられることが多い。横軸構造は約20m以下の低落差
に適用され、円筒ケーシングが用いられ一般にチューブ
ラ水車ともいう。この横軸構造では、一般に発電機もケ
ーシング内に設けられている。In general, propeller water turbines are high specific speed water turbines that are applied to low heads of about 90 m or less, and there are two types: vertical shaft structures and horizontal shaft structures. For those with a vertical shaft structure, a spiral casing similar to a 7 Rancis turbine is used for a head of about 20 m or more, and a semi-spiral casing is often used for a head of about 20 m or less. The horizontal shaft structure is applied to low heads of about 20 m or less, uses a cylindrical casing, and is generally called a tubular water turbine. In this horizontal shaft structure, the generator is also generally provided within the casing.
ランチには、4〜10枚のランナ羽根が設けられ、ラン
ナバンドは設けられない。ランチ羽根は可動形構造にさ
れることが多く、負荷および落差の変化に応じて、ガイ
ド羽根とランナ羽根の開度を変えることができる。この
場合、常に水車が最良の効率で運転できるように、調速
機に設けられたカムlこより、開度の相互関係は一定に
保たれる。The launch is provided with 4 to 10 runner blades and no runner band. Launch vanes are often of a movable structure, and the opening degree of the guide vanes and runner vanes can be changed in response to changes in load and head. In this case, the interrelationship of the opening degrees is kept constant by the cam l provided in the speed governor so that the water turbine can always operate at the best efficiency.
ランナ羽根の開閉は、多くの場合、ガイド羽根と同様に
圧油により自動的に行なわれる。このような自動調整式
可動羽根プロペラ水車をカブラン水車とも呼んでいる。In many cases, the runner blades are opened and closed automatically using pressure oil, similar to the guide blades. This type of self-adjusting movable blade propeller water turbine is also called a Kabran water turbine.
このような構造のプロペラ水車において、ランナ羽根の
外周部出口附近にはキャビテーションが発生し、水車効
率の低下ないしランナ羽根またはディスチャージリング
が異常な損傷を受けることから、ランチ羽根出口への漏
れ流れを減少させることが要望される。In a propeller-turbine with such a structure, cavitation occurs near the outlet of the outer periphery of the runner blades, reducing the efficiency of the turbine or causing abnormal damage to the runner blades or discharge ring. It is desired to reduce this.
第1図に横軸構造のプロペラ水車のランナ羽根要部の従
来例を示し、図において、ランナ10は複数枚のランチ
羽根1とランナボス2とからなり、ランナ羽根1は軸部
4を介してランナボス2に支承され、開度を変えられる
構造となっている。3は上述した円筒ケーシングの一部
で、図示しない吸出し管の上流側に連結されたランナ羽
根1の外囲となるディスチャージリングである。水は矢
印Aのように流れ、ランナ10は矢印Bのように回転し
、ランナ羽根1の外周面とディスチャージリング3の内
周面との間には、一定の隙間δが保たれている。!2図
は第1図のB−B断面拡大図で、水車運転中に上記隙間
δを通って矢印Pのようにランナ羽根の高圧面側1aの
流水が低圧面側1bに漏れ流れを生じ、水車効率を低下
させるさともに、ランチ羽根1外周部の出口附近にキャ
ビテーションが発生し、ランナ羽根1ないしはディスチ
ャージリング3の内周面が異常に損傷を受けるなどの欠
点があった。FIG. 1 shows a conventional example of the main part of the runner blades of a propeller water turbine with a horizontal shaft structure. It is supported by the runner boss 2 and has a structure that allows the opening degree to be changed. Reference numeral 3 denotes a discharge ring, which is a part of the above-mentioned cylindrical casing and serves as an outer circumference of the runner blade 1 connected to the upstream side of the suction pipe (not shown). Water flows as indicated by arrow A, runner 10 rotates as indicated by arrow B, and a constant gap δ is maintained between the outer circumferential surface of runner blade 1 and the inner circumferential surface of discharge ring 3. ! Fig. 2 is an enlarged cross-sectional view taken along line B-B in Fig. 1. During operation of the water turbine, water flowing from the high-pressure side 1a of the runner blade leaks to the low-pressure side 1b through the gap δ as shown by arrow P. In addition to reducing the efficiency of the water turbine, cavitation occurs near the outlet of the outer circumference of the launch blade 1, resulting in abnormal damage to the inner circumferential surface of the runner blade 1 or discharge ring 3.
本発明は上記のような点に鑑み、簡単な構造でランチ羽
根の高圧面側から低圧面側への流水の漏れ流れを抑制し
、水車効率を高め、ランナ羽根外周部出口のキャビテー
ション特性を向上させることができるプロペラ水車のラ
ンナ羽根を提供することを目的とする。In view of the above points, the present invention has a simple structure that suppresses leakage of flowing water from the high pressure side to the low pressure side of the launch blade, increases the efficiency of the water turbine, and improves the cavitation characteristics at the outlet of the outer peripheral part of the runner blade. The purpose of the present invention is to provide a runner blade for a propeller water turbine that can
本発明によれば上記の目的は、断面翼形の板状体として
形成されたプロペラ水車のランナ羽根において、該ラン
チ羽根の外周端面に前記翼形に沿って凹所を設けること
によって達せられる。According to the present invention, the above object is achieved by providing a runner blade of a propeller water turbine formed as a plate-like body with an airfoil cross section with a recess along the airfoil shape on the outer peripheral end face of the launch blade.
以下本発明を実施例を示す図面に基づいて説明する。第
3図および第4図は本発明の実施例を示し、第3図はラ
ンチ羽根の平面図を、@4図はそのC−C断面図であっ
て、図において、第1図ないし第2図と同じ構成要素に
は同一符号を付してその説明を省略する。ランチ羽根1
1は断面翼形の板状体として形成され、外周面に翼形の
長手方向に細長な凹所12を備えている。また、ランナ
羽根11の外周面とディスチャージリング3との間には
一定の隙間δが保たれ水はランナ羽根11の入口端に適
正な角度で流入し、翼形に沿った矢印Qのような流れを
形成している。The present invention will be described below based on drawings showing embodiments. 3 and 4 show an embodiment of the present invention, FIG. 3 is a plan view of the launch blade, and FIG. 4 is a cross-sectional view taken along line C-C. Components that are the same as those in the figures are given the same reference numerals and their explanations will be omitted. Lunch feathers 1
1 is formed as a plate-like body with an airfoil-shaped cross section, and is provided with an elongated recess 12 in the longitudinal direction of the airfoil on its outer peripheral surface. Also, a constant gap δ is maintained between the outer circumferential surface of the runner blade 11 and the discharge ring 3, and water flows into the inlet end of the runner blade 11 at an appropriate angle, and the water flows as shown by arrow Q along the airfoil shape. forming a flow.
このような構造において、ランナ羽根11とディスチャ
ージリング3との間にはラビリンス効果が生じ、ランナ
羽根の高圧面側11aに沿って流れる流水の矢印Sのよ
うな漏れ流は、ランチ羽根の外周端面に設けられた凹所
12による流路抵抗の増大で圧力低下し、低圧面側11
bへ漏れにくくなる。In such a structure, a labyrinth effect occurs between the runner blade 11 and the discharge ring 3, and the leakage flow as shown by the arrow S of the flowing water flowing along the high pressure side 11a of the runner blade is caused by the outer peripheral end surface of the launch blade. The pressure decreases due to the increase in flow path resistance due to the recess 12 provided on the low pressure side 11.
It becomes difficult to leak to b.
これにより、水車効率が高められ、ランチ羽根外周部出
口のキャビテーションの発生を抑制することができる。This increases the efficiency of the water turbine and suppresses the occurrence of cavitation at the outlet of the outer circumference of the launch blade.
同、上述した実施例はランナ羽根11の外周端面の翼形
の長手方向に細長な凹所12が1個あるものにつき述べ
たが、さらに板状体のランナ羽根 5−
で翼幅の大きなものには複数個の細長な凹所12を翼幅
に並列して設けてもよくこの場合には、ランチ羽根の高
圧面側から低圧面側への流水の漏れ流れをさらに少さく
することができる。In the above-mentioned embodiment, the runner blade 11 has one elongated recess 12 in the longitudinal direction of the airfoil shape on the outer circumferential end surface of the runner blade 11, but in addition, the runner blade 5- is a plate-shaped runner blade with a large blade span. A plurality of elongated recesses 12 may be provided in parallel to the blade span, and in this case, the leakage flow of flowing water from the high pressure side to the low pressure side of the launch vane can be further reduced. .
本発明は上記のように、翼形断面の板状体として形成さ
れたプロペラ水車のランチ羽根において、該ランナ羽根
の外周端面に翼形の長手方向に細長な凹所を設けたこと
により、簡単な構造でランチ羽根の高圧面側から低圧面
側への流水の漏れ流れを抑制し、水車効率を高め、ラン
チ羽根外周部出口のキャビテーション特性を向上させ、
ランチ羽根ないしディスチャージリングの損傷を防止す
ることができる。As described above, the present invention provides a launch vane for a propeller water turbine which is formed as a plate-like body with an airfoil cross section, by providing an elongated recess in the longitudinal direction of the airfoil on the outer peripheral end surface of the runner blade. This structure suppresses leakage of flowing water from the high-pressure side of the launch blade to the low-pressure side, increases turbine efficiency, and improves cavitation characteristics at the outlet of the outer circumference of the launch blade.
Damage to the launch blade or discharge ring can be prevented.
第1図および第2図は横軸プロペラ水車のランナ羽根要
部の従来例を示すもので、第1図はその構成図、第2図
は第1図のB−B断面図、第3図および第4図は本発明
の実施例を示し、第3図はランナ羽根要部の平面図、第
4図はそのC−C断 6−
面図である。
11 ランナ羽根、lla・・・高圧面側、12b・・
低圧面側、12・・・凹所。Figures 1 and 2 show a conventional example of the main part of the runner blade of a horizontal propeller water turbine. Figure 1 is its configuration, Figure 2 is a sectional view taken along line B-B in Figure 1, and Figure 3 4 shows an embodiment of the present invention, FIG. 3 is a plan view of the main part of the runner blade, and FIG. 4 is a sectional view taken along the line C--C. 11 Runner blade, lla...high pressure side, 12b...
Low pressure side, 12... recess.
Claims (1)
ランナ羽根において、該ランナ羽根の外周端面に、該ラ
ンチ羽根の高圧面側から低圧面側への流水の漏れ流れを
抑制する凹所を前記翼形に沿って1弥ことを特徴とする
プロペラ水車のランチ羽根。1) In a runner blade of a propeller water turbine formed as a plate-shaped body having a wing-shaped cross section, a recess is provided on the outer peripheral end face of the runner blade to suppress leakage of flowing water from the high-pressure side to the low-pressure side of the launch blade. A launch blade of a propeller water turbine, characterized in that: a launch blade of a propeller water wheel is formed along the airfoil shape.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59008848A JPS60153478A (en) | 1984-01-20 | 1984-01-20 | Runner vane for propeller turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59008848A JPS60153478A (en) | 1984-01-20 | 1984-01-20 | Runner vane for propeller turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS60153478A true JPS60153478A (en) | 1985-08-12 |
Family
ID=11704163
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP59008848A Pending JPS60153478A (en) | 1984-01-20 | 1984-01-20 | Runner vane for propeller turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60153478A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006210318A (en) * | 2004-12-27 | 2006-08-10 | Nissan Motor Co Ltd | Battery pack |
JP2016017415A (en) * | 2014-07-04 | 2016-02-01 | 株式会社東芝 | Axial-flow water turbine |
JP2016037875A (en) * | 2014-08-06 | 2016-03-22 | 東京電力株式会社 | Fluid machine |
JP2019007374A (en) * | 2017-06-21 | 2019-01-17 | 株式会社東芝 | Runner of movable blade water turbine, discharge ring of movable blade water turbine, and movable blade water turbine |
JP2019199801A (en) * | 2018-05-14 | 2019-11-21 | 株式会社東芝 | Runner vane and axial flow hydraulic machine |
-
1984
- 1984-01-20 JP JP59008848A patent/JPS60153478A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006210318A (en) * | 2004-12-27 | 2006-08-10 | Nissan Motor Co Ltd | Battery pack |
JP2016017415A (en) * | 2014-07-04 | 2016-02-01 | 株式会社東芝 | Axial-flow water turbine |
JP2016037875A (en) * | 2014-08-06 | 2016-03-22 | 東京電力株式会社 | Fluid machine |
JP2019007374A (en) * | 2017-06-21 | 2019-01-17 | 株式会社東芝 | Runner of movable blade water turbine, discharge ring of movable blade water turbine, and movable blade water turbine |
JP2019199801A (en) * | 2018-05-14 | 2019-11-21 | 株式会社東芝 | Runner vane and axial flow hydraulic machine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP4148872B2 (en) | Casing, compressor, turbine and combustion turbine engine including such casing | |
US3861826A (en) | Cascade diffuser having thin, straight vanes | |
KR100254284B1 (en) | Turbine spray nozzle and turbine rotary blade for axial-flow type turbo machine | |
US4248566A (en) | Dual function compressor bleed | |
US8133032B2 (en) | Rotor blades | |
US6338609B1 (en) | Convex compressor casing | |
US3999883A (en) | Variable turbomachine stator | |
US20100232936A1 (en) | Variable stator vane contoured button | |
JPH09105310A (en) | Flow orientation control element for gas-turbine engine and axial compressor | |
US3832089A (en) | Turbomachinery and method of manufacturing diffusers therefor | |
JP2005023935A (en) | Method and apparatus for assembling gas turbine engine | |
US10378360B2 (en) | Fan root endwall contouring | |
EP1260674B1 (en) | Turbine blade and turbine | |
JPH04232304A (en) | Cooling blade type moving blade | |
JP5964263B2 (en) | Rotor cascade of axial flow turbine and axial flow turbine | |
CA1064828A (en) | Variable camber vane for a gas turbine engine | |
US2846137A (en) | Construction for axial-flow turbomachinery | |
CN111720175A (en) | Impeller machinery movable vane top seal structure | |
US11649798B2 (en) | Reversible pump turbine and guide vane for the reversible pump turbine | |
US8777564B2 (en) | Hybrid flow blade design | |
US10221859B2 (en) | Turbine engine compressor blade | |
US20210372288A1 (en) | Compressor stator with leading edge fillet | |
CN207554113U (en) | Aero-turbine rotor assembly and its blade | |
JPS60153478A (en) | Runner vane for propeller turbine | |
US6632069B1 (en) | Step of pressure of the steam and gas turbine with universal belt |