JPS59185802A - Three-flow exhaust turbine - Google Patents

Three-flow exhaust turbine

Info

Publication number
JPS59185802A
JPS59185802A JP5981883A JP5981883A JPS59185802A JP S59185802 A JPS59185802 A JP S59185802A JP 5981883 A JP5981883 A JP 5981883A JP 5981883 A JP5981883 A JP 5981883A JP S59185802 A JPS59185802 A JP S59185802A
Authority
JP
Japan
Prior art keywords
exhaust turbine
exhaust
turbine section
flow
axle
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
JP5981883A
Other languages
Japanese (ja)
Inventor
Masayoshi Tateno
立野 政義
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.)
Fuji Electric Co Ltd
Original Assignee
Fuji Electric Co Ltd
Fuji Electric Manufacturing Co 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 Fuji Electric Co Ltd, Fuji Electric Manufacturing Co Ltd filed Critical Fuji Electric Co Ltd
Priority to JP5981883A priority Critical patent/JPS59185802A/en
Publication of JPS59185802A publication Critical patent/JPS59185802A/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
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/023Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines the working-fluid being divided into several separate flows ; several separate fluid flows being united in a single flow; the machine or engine having provision for two or more different possible fluid flow paths

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To reduce the number of parts and simplify manufacture by forming a two-flow exhaust turbine and a single-flow exhaust turbine by means of a common axle and support the axle between two trubines without using a bearing. CONSTITUTION:A two-flow exhaust turbine 21 and a single-flow exhaust turbine 22, formed by means of a common axle 25, are supported by means of bearings 26, 27 at both ends of said axle. Any bearing or coupling is not provided between two rotors 23, 24. Thus, the number of parts can be reduced and manufacture can also be simplified.

Description

【発明の詳細な説明】 〔発明の属する技術分野〕 本発明は3つの排気流系統を有したタービンに関する。[Detailed description of the invention] [Technical field to which the invention pertains] The present invention relates to a turbine with three exhaust flow systems.

〔従来技術とその問題点〕[Prior art and its problems]

蒸気タービン等のタービンにおいては、排気系統はこれ
までは普通1流、2I&、あるいは4流のものが用いら
れている。これら排気系統は復水タービンにお℃・では
復水器に接続されるものである。
In turbines such as steam turbines, the exhaust system has conventionally been one-flow, two-flow, or four-flow exhaust system. These exhaust systems are connected to the condensing turbine and the condenser at °C.

また、作動流体の流量が多く2流では排気断面積  ゛
が小さくタービン性能が悪く、かつ4流では排気断面積
が太きすぎて不経済であるような場合、2流として排気
2断面積を太きくしようとしてもこれに対応できる大き
な低圧部を作ることが現在の技術では困難であるため、
3流の排気系統が採用される場合がある。
In addition, when the flow rate of the working fluid is large and the 2nd flow has a small exhaust cross-sectional area and the turbine performance is poor, and the 4th flow has an exhaust cross-sectional area that is too large and is uneconomical, the 2nd-flow exhaust cross-sectional area may be used as the 2nd flow. Even if we try to make it thicker, it is difficult with current technology to create a large low-pressure part that can accommodate this.
A third-stream exhaust system may be used.

この場合に従来用いられている3流排気のタービンは第
1図に示す如き構成て1あり、これば蒸気タービンを例
にとっている。1は2流排気タ一ビン部を示し、ロータ
2と、その車軸3と、ロータを覆うケーシング4と、車
軸を支持する軸受5゜6とを有している。軸受は基礎(
図示せず)により支持される。ケーシングに設けられて
いる蒸気入ロアより供給された蒸気は2つのローク’H
fi分に各々作用し矢印で示すように高圧部より低圧部
に向って流れロータを回転させ、各々の排気路8.。
In this case, a three-stream exhaust turbine conventionally used has a configuration as shown in FIG. 1, and a steam turbine is taken as an example. Reference numeral 1 designates a second-flow exhaust turbine section, which includes a rotor 2, an axle 3 thereof, a casing 4 covering the rotor, and bearings 5 and 6 supporting the axle. Bearings are the foundation (
(not shown). The steam supplied from the steam input lower installed in the casing is passed through two rows'H.
fi, the flow rotor is rotated from the high pressure section to the low pressure section as shown by the arrow, and each exhaust passage 8. .

9より排出される。これら排気路は図示しない復水器に
連通している。タービンはさらに1流排気タービン部1
1を有し、これはロータ12と、その車軸13と、ケー
シング14とを有している。
It is discharged from 9. These exhaust passages communicate with a condenser (not shown). The turbine further includes a first-stream exhaust turbine section 1.
1, which has a rotor 12, its axle 13 and a casing 14.

車軸13は一方の端においてカップリング15により前
記2流排気タ一ビン部の車軸3の軸端に結合され、また
他方の端部において基礎に支持された軸受16により軸
支されている。ケーシングに設けられている蒸気入口1
”7より供給される蒸気は矢印で示すように単一のロー
タ部分を高圧部から低圧部に流れ、復水器に連通する排
気路18より排出される。
The axle 13 is connected at one end by a coupling 15 to the shaft end of the axle 3 of the second flow exhaust turbine section, and is supported at the other end by a bearing 16 supported on the foundation. Steam inlet 1 provided in the casing
The steam supplied from "7" flows through the single rotor section from the high pressure section to the low pressure section as shown by the arrow, and is discharged through the exhaust passage 18 which communicates with the condenser.

上述の如き構成においては、2流排気タ一ビン部と1流
排気タービン部とを各々別体として作りこれらを結合す
るため、2流排気のものに較ベケーシング、車軸、軸受
等の部品点数が多くなり製造コストカ高くなり、また2
つのタービン部の間に軸受及びカップリングを要するた
めタービンの全長が長くなるという短所を有していた。
In the above-mentioned configuration, the second-stream exhaust turbine section and the first-stream exhaust turbine section are made separately and are combined, so the number of parts such as the casing, axle, and bearings is reduced compared to the second-stream exhaust turbine section. This increases the manufacturing cost, and also increases the production cost.
Since bearings and couplings are required between the two turbine parts, the overall length of the turbine becomes long.

〔発明の目的〕 本発明の目的は上述の短所を解消し、2流排気のものに
較ぜコスト及び大きさを実質的増大させることがたい3
流排気めタービンを提供することである。
[Object of the Invention] It is an object of the present invention to overcome the above-mentioned disadvantages and to avoid a substantial increase in cost and size compared to two-flow exhaust systems.
It is an object of the present invention to provide a flow exhaust turbine.

〔発明の要点〕[Key points of the invention]

本発明は、2流排気タ一ビン部と1流排気タービン部の
車軸を共通の軸により形成し、この軸を2つのタービン
部間に軸受を用いることなく軸支したものである。
In the present invention, the axles of the second-stream exhaust turbine section and the first-stream exhaust turbine section are formed by a common shaft, and this shaft is supported between the two turbine sections without using a bearing.

〔発明の実施例〕[Embodiments of the invention]

第2図は本発明の1つの実施例である蒸気タービン7示
すもので、2流排気タ一ビン部21と1流排気タービン
部22とを有する。2流排気タ一ビン部のロータ23と
1流排気タービン部のロータ24とは共通の車軸25を
有しこれは両端において軸受26.27により軸支され
ている。2つのロータ23及び24の間には軸受やカッ
プリングが存在せず、このためケーシング28は2つの
ロータに対し共通の構造とすることが可能となって見・
る。ケーシング28に設けられた蒸気供給路は途中で2
つに分れ、2流排気タ一ビン部の入口29及び1流排気
タービン部の入口31に各々蒸気を供給する。各々の入
口29.31より供給された蒸気は矢印で示すように各
ロータ23,24に作用し図示しない復水器に接続され
た排気路32,33.。
FIG. 2 shows a steam turbine 7 according to one embodiment of the present invention, which has a second-stream exhaust turbine section 21 and a first-stream exhaust turbine section 22. As shown in FIG. The rotor 23 of the second-stream exhaust turbine section and the rotor 24 of the first-stream exhaust turbine section have a common axle 25, which is supported at both ends by bearings 26, 27. There are no bearings or couplings between the two rotors 23 and 24, so the casing 28 can have a common structure for the two rotors.
Ru. The steam supply path provided in the casing 28 has two
The steam is divided into two parts, and the steam is supplied to the inlet 29 of the second-stream exhaust turbine section and the inlet 31 of the first-stream exhaust turbine section, respectively. The steam supplied from each inlet 29, 31 acts on each rotor 23, 24 as shown by the arrows, and exhaust passages 32, 33, 32, 32, 32, 32, 32, 32, 31, 31, 31, 24, 32, 31, 31, 31, 31, 31, 24, 31, 31, 31, 31, 31, 31, 35, 35, 25, 24, 24, 24, 24, 24, 22, 22, 2, , , , , , , , , , , , , , , , , , , , , , , , , , , , tion por por , t’s steam, Which is supplied from each inlet port 29, 31, acts on each rotor 23, 24, as indicated by the arrows. .

34より排出される。It is discharged from 34.

第3図は本発明の他の実施例の蒸気タービンを示づ−も
ので、第2図に示す構成要素と同じ性質の構成要素には
同じ符号を付してその説明を省略する。従って以下に特
に述べる魚身外は第2図の例と同じである。この例にお
いては、1流排気タービン部220ロータ41は第2図
の例とは逆向きになっており、1流排気タービン部22
の排気路と2流排気タ一ビン部21の一方の排気路とは
共通の排気路42となっている。
FIG. 3 shows a steam turbine according to another embodiment of the present invention, and components having the same properties as those shown in FIG. 2 are given the same reference numerals and their explanations will be omitted. Therefore, the parts other than the fish body described below are the same as the example shown in FIG. 2. In this example, the first-stream exhaust turbine section 220 rotor 41 is oriented in the opposite direction from the example shown in FIG.
The exhaust path and one exhaust path of the second-flow exhaust turbine section 21 form a common exhaust path 42.

〔発明の効果〕〔Effect of the invention〕

上述のように本発明によれば2IN、排気タービン部及
び1流排気タービン部の間に軸受もカップリングも存在
せず、またケーシングも共通の構成にできろため、従来
のものに較べ部品数が少く、また製作が簡単になりコス
ト低下が可能であり、また全長も短いものとすることが
できる。
As mentioned above, according to the present invention, there are no bearings or couplings between the 2IN, exhaust turbine section, and first-stream exhaust turbine section, and the casing can also have a common configuration, so the number of parts is reduced compared to the conventional one. This makes it possible to reduce the manufacturing cost and reduce the overall length.

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

第1図は従来の3流排気のタービンの構成説明図;第2
図は本発明の1つの実施例であろ3流排気のタービンの
構成説明図;第3図は本発明の他の実施例である3流排
気のタービンの構成説明図。 3・・・2流排気タ一ビン部の車軸、 13・・・1流排気タービン部の車軸、21・・・2流
排気ター−ビン部、 22・・・1流排気タービン部、 25・・・共通の車軸。 特許出願人  富士電機製造株式会社 第1図 第2図 第3図′ 32           4z
Figure 1 is an explanatory diagram of the configuration of a conventional three-stream exhaust turbine;
The figure is an explanatory diagram of the configuration of a three-stream exhaust turbine, which is one embodiment of the present invention; FIG. 3 is an explanatory diagram of the configuration of a three-stream exhaust turbine, which is another embodiment of the present invention. 3... Axle of second flow exhaust turbine section, 13... Axle of first flow exhaust turbine section, 21... Second flow exhaust turbine section, 22... First flow exhaust turbine section, 25. ...Common axle. Patent applicant: Fuji Electric Manufacturing Co., Ltd. Figure 1 Figure 2 Figure 3' 32 4z

Claims (1)

【特許請求の範囲】 1)2流排気タ一ビン部と1流排気タービン部とを有し
た3流排気のタービンにおいて、2流排気タ一ビン部の
車軸と1流排気タービン部の車軸とを共通の軸により形
成し、該軸を両軸端で軸支する構成としたことを特徴と
する3流排気のタービン。 2、特許請求の範囲第1項記載のタービンにおいて、ロ
ータを覆うケーシングを共通の構成で一体化したことを
特徴とする3流排気のター ビン。
[Scope of Claims] 1) In a third-stream exhaust turbine having a second-stream exhaust turbine section and a first-stream exhaust turbine section, an axle of the second-stream exhaust turbine section and an axle of the first-stream exhaust turbine section. A three-stream exhaust turbine, characterized in that the two are formed by a common shaft, and the shaft is pivotally supported at both shaft ends. 2. A three-stream exhaust turbine according to claim 1, characterized in that the casing covering the rotor is integrated with a common configuration.
JP5981883A 1983-04-05 1983-04-05 Three-flow exhaust turbine Pending JPS59185802A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5981883A JPS59185802A (en) 1983-04-05 1983-04-05 Three-flow exhaust turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5981883A JPS59185802A (en) 1983-04-05 1983-04-05 Three-flow exhaust turbine

Publications (1)

Publication Number Publication Date
JPS59185802A true JPS59185802A (en) 1984-10-22

Family

ID=13124181

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5981883A Pending JPS59185802A (en) 1983-04-05 1983-04-05 Three-flow exhaust turbine

Country Status (1)

Country Link
JP (1) JPS59185802A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015533981A (en) * 2012-09-11 2015-11-26 コンセプツ・イーティーアイ・インコーポレーテッド Overhang turbine and generator system with turbine cartridge

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015533981A (en) * 2012-09-11 2015-11-26 コンセプツ・イーティーアイ・インコーポレーテッド Overhang turbine and generator system with turbine cartridge
US10069378B2 (en) 2012-09-11 2018-09-04 Concepts Nrec, Llc ORC turbine and generator, and method of making a turbine

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