JPH0373721B2 - - Google Patents

Info

Publication number
JPH0373721B2
JPH0373721B2 JP60050713A JP5071385A JPH0373721B2 JP H0373721 B2 JPH0373721 B2 JP H0373721B2 JP 60050713 A JP60050713 A JP 60050713A JP 5071385 A JP5071385 A JP 5071385A JP H0373721 B2 JPH0373721 B2 JP H0373721B2
Authority
JP
Japan
Prior art keywords
outer casing
inner casing
casing
vane ring
pressure end
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 - Lifetime
Application number
JP60050713A
Other languages
Japanese (ja)
Other versions
JPS60212604A (en
Inventor
Jei Miraa Ruisu
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of JPS60212604A publication Critical patent/JPS60212604A/en
Publication of JPH0373721B2 publication Critical patent/JPH0373721B2/ja
Granted 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • 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
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • 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
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

【発明の詳細な説明】 本発明は、蒸気タービンに関し、特に内側ケー
シング及び羽根リングを有する蒸気タービンに関
するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to steam turbines, and more particularly to steam turbines having an inner casing and vane rings.

従来の蒸気タービンは、外側ケーシングと、該
外側ケーシング内に配設され外側ケーシングから
支持された内側ケーシングと、該内側ケーシング
内に支持された羽根リングとを備えて製作されて
いる。内側ケーシング内に羽根リングを支持する
ことにより、外側ケーシングが最も高い圧力及び
温度にさらされるのを避けることができる。しか
し、羽根リングと外側ケーシングとの間に内側ケ
ーシングを配置すると、外側ケーシングが羽根リ
ング及び内側ケーシングの双方を収容しなければ
ならないので、外側ケーシングが比較的に大径に
なり、好ましいことではない。
Conventional steam turbines are constructed with an outer casing, an inner casing disposed within and supported from the outer casing, and a vane ring supported within the inner casing. By supporting the vane ring within the inner casing, exposure of the outer casing to the highest pressures and temperatures can be avoided. However, if the inner casing is placed between the vane ring and the outer casing, the outer casing will have a relatively large diameter, which is not desirable, since the outer casing must accommodate both the vane ring and the inner casing. .

従つて、本発明の目的は、外側ケーシングが最
も高い圧力及び温度にさらされるのを避けるとい
う内側ケーシングの利点を保持しながら、タービ
ン直径を大巾に縮小することである。
It is therefore an object of the present invention to significantly reduce the turbine diameter while retaining the advantage of the inner casing of avoiding exposing the outer casing to the highest pressures and temperatures.

この目的を達成するために、本発明は、水平割
りの円筒状外側ケーシングと、部分的に該外側ケ
ーシング内に配設されて該外側ケーシングから支
持された水平割りの円筒状内側ケーシングと、部
分的に前記外側ケーシング内に且つ部分的に前記
内側ケーシング内に配設されると共に、タービン
ロータを囲む末広形の羽根リングとを備え、該羽
根リングは、同羽根リングの低圧端部が前記内側
ケーシングから軸方向に突出し、相対的に小径の
同羽根リングの高圧端部のみが前記内側ケーシン
グ内に配設されており、前記低圧端部が、前記外
側ケーシングまで半径方向外方に延びて、同外側
ケーシングに直接支持された一体の支持腕を備え
ている蒸気タービンを提供している。
To this end, the present invention comprises a horizontally split cylindrical outer casing, a horizontally split cylindrical inner casing partially disposed within and supported from the outer casing; a divergent vane ring disposed generally within the outer casing and partially within the inner casing and surrounding a turbine rotor, the vane ring having a low pressure end within the inner casing; only a high pressure end of a relatively small diameter vane ring projecting axially from the casing is disposed within the inner casing, and the low pressure end extends radially outwardly to the outer casing; A steam turbine is provided having an integral support arm supported directly on the outer casing.

このように羽根リングの小径の高圧端部のみを
内側ケーシング内に配置することにより、内側ケ
ーシングを比較的に小径とすることができ、内側
及び外側ケーシングの直径及び肉厚及をもつと小
さくすることができる。また、羽根リングの低圧
端部では蒸気の圧力及び温度が相対的に低下して
いるため、外側ケーシングが最も高い圧力及び温
度にさらされるのを避けるという内側ケーシング
の利点も損なわれない。
By arranging only the small-diameter high-pressure end of the vane ring inside the inner casing in this way, the inner casing can be made relatively small in diameter, making the diameter and wall thickness of the inner and outer casings smaller. be able to. Also, because the steam pressure and temperature are relatively reduced at the low pressure end of the vane ring, the advantage of the inner casing to avoid exposing the outer casing to the highest pressures and temperatures is not compromised.

本発明は、添付図面に例示したその好適な実施
例に関する以下の説明から一層容易に明らかとな
ろう。
The invention will become more readily apparent from the following description of preferred embodiments thereof, illustrated in the accompanying drawings.

第1図及び第2図には先行技術が記載されてお
り、そこに示された蒸気タービン103は、本発
明に従つて構成された第3図及び第4図に示すタ
ービン3と同一の作動温度、圧力及び蒸気量で設
計されている。先行技術における100台の参照番
号は、第3図及び第4図において100を引いた参
照番号で示された諸部分に類似するものを表して
いる。
The prior art is described in FIGS. 1 and 2, in which the steam turbine 103 shown is operationally identical to the turbine 3 shown in FIGS. 3 and 4 constructed in accordance with the present invention. It is designed with temperature, pressure and steam amount. Reference numerals in the 100 range in the prior art represent similar parts to those designated by the reference numeral 100 minus 100 in FIGS. 3 and 4.

本発明の好適な実施例による蒸気タービン3
は、ボルト7によつて相互に結合された水平割り
の円筒外側ハウジング又はケーシング5と、ボル
ト11によつて相互に結合されて外側ケーシング
5内に配設され、支持体13によつて外側ケーシ
ング5から支持された、水平割りの円筒状内側ケ
ーシング9とを備える。内側ケーシング9内に部
分的に配設され外側ケーシング5内に部分的に配
設されているのは長手方向にスプリツトされた羽
根リング15であつて、これもボルト17により
相互に結合されている。図示のように末広形の該
羽根リング15は、相対的に大径の同羽根リング
15の低圧端部が内側ケーシング9から軸方向に
突出し、相対的に小径の同羽根リング15の高圧
端部のみが内側ケーシング9内に配置されてお
り、低圧端部が、外側ケーシング5まで半径方向
外方に延びて、同外側ケーシング5に直接支持さ
れた一体の支持腕19を備えている。また、羽根
リング15は円周方向に延びる複数の溝21を有
しており、該溝21が固定羽根23の環状列を受
けて入れている。
Steam turbine 3 according to a preferred embodiment of the invention
are arranged within the outer casing 5 and are connected to each other by bolts 11 with horizontally split cylindrical outer housings or casings 5 connected to each other by bolts 7 and by supports 13 to the outer casing. 5 and a horizontally split cylindrical inner casing 9 . Disposed partly in the inner casing 9 and partly in the outer casing 5 are longitudinally split vane rings 15, which are also interconnected by bolts 17. . As shown in the drawing, the blade ring 15 has a wide-end shape, with the low-pressure end of the blade ring 15 having a relatively large diameter protruding in the axial direction from the inner casing 9, and the high-pressure end of the blade ring 15 having a relatively small diameter protruding from the inner casing 9 in the axial direction. is located within the inner casing 9 and has an integral support arm 19 whose low pressure end extends radially outwards to the outer casing 5 and is supported directly thereon. The vane ring 15 also has a plurality of circumferentially extending grooves 21 which receive annular rows of fixed vanes 23 therein.

回転羽根27の複数の環状列を有するタービン
ロータ25は羽根リング15内に配設されてお
り、回転羽根27の列は指状になつて固定羽根2
3の列の間に入つている。
A turbine rotor 25 having a plurality of annular rows of rotating blades 27 is disposed within the blade ring 15, and the rows of rotating blades 27 are arranged in the form of fingers to form fixed blades 2.
It is between the 3 columns.

ノズルブロツク29及びノズル室31は、羽根
リング15の一端において内側ケーシング9内に
配設され、羽根通路へ蒸気が流れるようにしてい
る。また、内側ケーシング9内にはダミーリング
33が配設されており、該ダミーリング33がタ
ービンロータ25上の一体型バランスデイスク3
5と協働して、蒸気によつて生じ回転する羽根及
びロータに作用するスラストをバランスさせてい
る。
A nozzle block 29 and a nozzle chamber 31 are arranged within the inner casing 9 at one end of the vane ring 15 to allow steam to flow into the vane passage. Further, a dummy ring 33 is disposed inside the inner casing 9, and the dummy ring 33 is connected to the integrated balance disk 3 on the turbine rotor 25.
5 to balance the thrust generated by the steam and acting on the rotating blades and rotor.

内側ケーシング9よりもむしろ外側クーシング
5から羽根リングの低圧端部を支持することによ
つて、羽根リングに作用する抵抗モーメントを増
大して応力を軽減する利点がある。羽根リング1
5の支持領域は、材料に対する要求を下げ且つ許
容応力を増大するより低い温度領域に移り、ま
た、内側及び外側ケーシング全体の直径、壁厚並
びにボルト締結要求を減少させ、更に、羽根リン
グからの負荷が外側ケーシングに直接伝達される
ので内側ケーシング支持体サイズを減少させ、こ
のようにして材料、製造及び取扱い上の節約をも
たらす。
By supporting the low pressure end of the vane ring from the outer casing 5 rather than the inner casing 9, there is the advantage of increasing the moment of resistance acting on the vane ring and reducing stress. feather ring 1
The support area of 5 moves to a lower temperature area which lowers the demands on the material and increases the allowable stresses, and also reduces the overall diameter, wall thickness and bolting requirements of the inner and outer casings, and further reduces the stress from the vane ring. Loads are transferred directly to the outer casing, reducing inner casing support size, thus providing savings in material, manufacturing and handling.

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

第1図は、種々の上側リングは除いてあるが上
側ケーシングは取り付けてある先行技術の蒸気タ
ービンを一部断面で示す平面図、第2図は、第1
図の線−に沿つて示す部分断面図、第3図
は、本発明に従つて構成された、上側ケーシング
及び種々の上側リングを部分的に取り除いた、蒸
気タービンの部分平面図、第4図は、第3図の線
−に沿つて示す部分断面図である。 3……蒸気タービン、5……外側ケーシング、
9……内側ケーシング、15……羽根リング、1
9……支持腕、25……タービンロータ。
1 is a plan view, partially in section, of a prior art steam turbine with the various upper rings removed but the upper casing installed; FIG.
FIG. 3 is a partial plan view of a steam turbine constructed in accordance with the present invention, with the upper casing and various upper rings partially removed, FIG. 4; 3 is a partial sectional view taken along line - in FIG. 3; FIG. 3...Steam turbine, 5...Outer casing,
9...Inner casing, 15...Blade ring, 1
9...Support arm, 25...Turbine rotor.

Claims (1)

【特許請求の範囲】[Claims] 1 水平割りの円筒状外側ケーシング5と、部分
的に該外側ケーシング5内に配設されて該外側ケ
ーシング5から支持された水平割りの円筒状内側
ケーシング9と、部分的に前記外側ケーシング5
内に且つ部分的に前記内側ケーシング内に配設さ
れると共に、タービンロータ25を囲む末広形の
羽根リング15とを備え、該羽根リング15は、
同羽根リング15の低圧端部が前記内側ケーシン
グ9から軸方向に突出し、相対的に小径の同羽根
リング15の高圧端部のみが前記内側ケーシング
9内に配置されており、前記低圧端部が、前記外
側ケーシング5まで半径方向外方に延びて、同外
側ケーシング5に直接支持された一体の支持腕1
9を備えている蒸気タービン。
1 a horizontally split cylindrical outer casing 5 , a horizontally split cylindrical inner casing 9 partially disposed within the outer casing 5 and supported from the outer casing 5 , and partially the outer casing 5
a diverging vane ring 15 disposed within and partially within the inner casing and surrounding the turbine rotor 25, the vane ring 15 comprising:
A low-pressure end of the vane ring 15 protrudes axially from the inner casing 9, only a high-pressure end of the vane ring 15 having a relatively small diameter is disposed within the inner casing 9, and the low-pressure end , an integral support arm 1 extending radially outwardly to and directly supported by the outer casing 5;
Steam turbine with 9.
JP60050713A 1984-03-23 1985-03-15 Steam turbine Granted JPS60212604A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US59298384A 1984-03-23 1984-03-23
US592983 1984-03-23

Publications (2)

Publication Number Publication Date
JPS60212604A JPS60212604A (en) 1985-10-24
JPH0373721B2 true JPH0373721B2 (en) 1991-11-22

Family

ID=24372871

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60050713A Granted JPS60212604A (en) 1984-03-23 1985-03-15 Steam turbine

Country Status (6)

Country Link
EP (1) EP0156619B1 (en)
JP (1) JPS60212604A (en)
KR (1) KR930008675B1 (en)
DE (1) DE3565299D1 (en)
ES (1) ES8607476A1 (en)
IN (1) IN162366B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4661043A (en) * 1985-10-23 1987-04-28 Westinghouse Electric Corp. Steam turbine high pressure vent and seal system
US7497658B2 (en) * 2005-11-11 2009-03-03 General Electric Company Stacked reaction steam turbine stator assembly
US7722314B2 (en) * 2006-06-22 2010-05-25 General Electric Company Methods and systems for assembling a turbine
CN204984506U (en) * 2015-09-08 2016-01-20 阿尔斯通技术有限公司 Steam turbine with modularization male part
CN114458615B (en) * 2021-12-14 2023-11-21 泸州懋威科技有限公司 Compact turbine engine compressor bearing structure

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE724321C (en) * 1936-03-01 1942-08-24 Karl Roeder Dr Ing Guide vane carriers, subdivided in at least one axis plane and containing several rings, in particular for overpressure steam turbines
DE858251C (en) * 1938-03-03 1952-12-04 Karl Dr-Ing Roeder Guide vane or seal carrier, in which the carrier, which is divided at least in one axial plane, is held together by holding bodies
US2304994A (en) * 1941-06-20 1942-12-15 Westinghouse Electric & Mfg Co Turbine cylinder cooling
GB662371A (en) * 1948-07-17 1951-12-05 Westinghouse Electric Int Co Improvements in or relating to steam turbine apparatus
FR1157588A (en) * 1955-09-22 1958-05-30 Bbc Brown Boveri & Cie Gas or steam turbine for high pressures and temperatures
GB1024844A (en) * 1962-02-12 1966-04-06 Pametrada Improvements in or relating to steam turbines
CH426882A (en) * 1963-07-15 1966-12-31 Licentia Gmbh Axial reheating steam turbine
AT242716B (en) * 1963-11-18 1965-10-11 Elin Union Ag Steam turbine with controlled steam extraction
DE1426826A1 (en) * 1964-02-17 1969-01-23 Licentia Gmbh Live steam supply with multi-flow, highly stressed double-casing turbine

Also Published As

Publication number Publication date
EP0156619B1 (en) 1988-09-28
DE3565299D1 (en) 1988-11-03
JPS60212604A (en) 1985-10-24
KR930008675B1 (en) 1993-09-11
KR850007838A (en) 1985-12-09
IN162366B (en) 1988-05-14
ES541438A0 (en) 1986-05-16
EP0156619A1 (en) 1985-10-02
ES8607476A1 (en) 1986-05-16

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