JPS59120701A - Rotary machine - Google Patents
Rotary machineInfo
- Publication number
- JPS59120701A JPS59120701A JP57229294A JP22929482A JPS59120701A JP S59120701 A JPS59120701 A JP S59120701A JP 57229294 A JP57229294 A JP 57229294A JP 22929482 A JP22929482 A JP 22929482A JP S59120701 A JPS59120701 A JP S59120701A
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- stationary
- rotary
- steam
- implanted
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-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
- F01D1/04—Non-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 traversed by the working-fluid substantially axially
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【発明の詳細な説明】 従来の回転機械は,第1図に図示するように。[Detailed description of the invention] A conventional rotating machine is shown in Figure 1.
回転体動Raf:植設した回転軸(同転ロータ)bか中
心部にあり,同軸bは軸受Cl 、 C2を介して支持
体dに軸支されている。そして、回転軸bを中心とし,
て、静翼リンクeを植設したケーゾングfが環装されて
いる。なお、gは出力軸7hは図ij\省略の蒸気源か
ら供給される人力蒸気。Rotating body motion Raf: The installed rotating shaft (co-rotating rotor) b is located at the center, and the coaxial shaft b is supported by the support body d via bearings Cl and C2. Then, centering on the rotation axis b,
A casing f with a stator vane link e installed is mounted on the ring. In addition, the output shaft 7h is manually powered steam supplied from a steam source (not shown in the figure).
lは排気ダクトjから排出される排気,には静止部から
植出されたソール材である。1 is the sole material extruded from the stationary part of the exhaust gas discharged from the exhaust duct j.
このような従来の回転機械においては,漏洩損失が生じ
るという欠点があった。Such conventional rotating machines have the drawback of leakage losses.
本発明は,静止翼が植設された静止軸等の静止部材を中
心に,回転体動翼を植設し/ζ回転体が環装され,」一
記回転体かさらに静止チャンバーで環装されていること
を特徴とし,その目的とするところは,外周側を密閉構
造に出来るのて,外周側での漏洩損失を減少せし5め−
まだ,離爪散型の回転機械を提供するものである。In the present invention, rotary rotor blades are installed around a stationary member such as a stationary shaft in which stationary blades are installed. The purpose of this is to reduce leakage loss on the outer periphery by making the outer periphery a sealed structure.
However, it still provides a rotary machine that can be separated into pieces.
以下,本発明のρイま1〜い一実施例を第2図乃至第5
図で図示する実施例を用いて詳述する。Hereinafter, the first to first embodiments of the present invention will be explained with reference to FIGS. 2 to 5.
A detailed explanation will be given using an example illustrated in the drawings.
第2図乃至第5図において2 1は静1F軸,2a。In FIGS. 2 to 5, 21 is the static 1F axis, 2a.
2bは静止軸lK植込まれた静翼,3は回転軸で。2b is the stator blade embedded in the stationary shaft lK, and 3 is the rotating shaft.
同回転軸3は分割環状体3a,3b,:(c,3dで連
結構造体となっている。4a 、 4bは回転軸3を軸
支する軸受,5a,5b,5cid分割榎状体3J’,
3c 、 3dに円周方向に植込thた回転体動翼,
6,は回転軸3とカノズリング部7a,7bでボルト等
により連結された出力軸,8はノズル,二.点鎖線で表
示され・た領域、8.aはノズル室、 8bはノズル8
件静止軸】とを連結する支柱、9は静止部から植:
・11:・
出され永し′ニル材、1’Oa□、・ii□Obは回転
軸□3の・夙□1周、iリ □・に環装さ・、れだ外
−シンク・で、、イランジj、、la、llbでボルト
等により連結されている。12は蒸気導入管Iす、13
1ト気ダク□、ト、□4a、14□、□4o、□4d。The rotating shaft 3 has a connecting structure with split annular bodies 3a, 3b, (c, 3d). 4a and 4b are bearings that pivotally support the rotating shaft 3, and 5a, 5b, and 5cid split annular bodies 3J' ,
3c, 3d rotary rotor blades implanted in the circumferential direction,
6, an output shaft connected to the rotating shaft 3 by bolts or the like at the nozzle ring portions 7a, 7b; 8, a nozzle; 2. The area indicated by the dotted chain line, 8. a is the nozzle chamber, 8b is the nozzle 8
The column connecting the stationary shaft with the stationary shaft, 9 is installed from the stationary part:
・11:・ The long-drawn aluminum material, 1'Oa□, ・ii□Ob is ringed in the i-ri □, one rotation of the rotating shaft □3, and the sink is outside the ledge. ,,Iranjij,,la,llb are connected by bolts or the like. 12 is the steam introduction pipe I, 13
1 tokidaku□, □4a, 14□, □4o, □4d.
14e、14f 、44gはケーシング10a、10b
の支持台。14e, 14f, 44g are casings 10a, 10b
support stand.
15ハケーシング10aとノズル8とを連結するボ□1
ルトである・ 、、:
第4図および第!5 甲憾+幹:j止軸1および回転軸
8の組立てプロカスの例を示したものである。15 is a bolt that connects the casing 10a and the nozzle 8. ,,: Figure 4 and Figure ! 5. Armor + Trunk: This is an example of assembly procedure for the stop shaft 1 and rotating shaft 8.
1□1
第4図は静止軸1に回転軸、の1・部すなわち分割環状
体3aをセットシた状態で1次に動翼5aの植込まれだ
分割環状体3bを公害li環状体3aに結合するプロセ
スを示している。1 □ 1 Figure 4 shows the first part of the rotary shaft 1, that is, the divided annular body 3a, set on the stationary shaft 1, and the rotor blade 5a is embedded in the divided annular body 3b to the pollution-prone annular body 3a. It shows the process of combining.
第5図は、さらに静止軸lに静翼2aを植込むプロセス
を示している。このように、順次回転部と静止部とを交
互に組合せて行くに
のように構成された実施例においては2図不省略のボイ
ラ等から蒸気等の高エネルギー流体を蒸気導入管12か
らノズル室8aへ導き、つ酢、:、′
・いて動翼! a 4” 5b 、 5cに噴射し、高
エネルギー流□
”−静翼2b→動翼5cと流れること、によって1、回
転軸3を回転させ、流体エネル臀−を回転エネルギーに
変換し、出力軸6から回転エネルギを取り出す。FIG. 5 further shows the process of implanting the stationary blade 2a on the stationary shaft l. In this embodiment, in which the rotating part and the stationary part are sequentially combined, high-energy fluid such as steam is supplied from the boiler (not shown in Figure 2) to the nozzle chamber through the steam introduction pipe 12. Lead to 8a, Tsuzuzu:,' ・Moving blade! A 4'' is injected into 5b and 5c, and the high-energy flow □'' flows from stationary blade 2b to rotor blade 5c, thereby rotating the rotating shaft 3, converting fluid energy into rotational energy, and rotating the output shaft. The rotational energy is extracted from 6.
このように、動R5a 、 sb 、 5cが外周にな
っている回転軸3に植え込捷れているため7動漬5・。In this way, since the movable shafts R5a, sb, and 5c are inserted into the rotating shaft 3, which is the outer periphery, and are twisted, the movable shaft 5.
5b、5cの遠心応力は各部とも基本的には圧縮応力ど
なるので、万一飛散状態が発生したケ、シても、従来構
造にくらべ、て、、、、4魅!に、≦、、い、、へいう
利点がある。、t、た、外、周側す:なわちノズル8゜
回転軸3.出力軸6によって密閉構造にすることが出来
るので、外周側での漏洩損失艇減少出来るようになる。The centrifugal stress of 5b and 5c is basically compressive stress in each part, so even if a scattering condition occurs, it will be 4 times lower than the conventional structure! There is an advantage that ≦,,i,,. , t, outside, circumferential side: that is, nozzle 8° rotation axis 3. Since the output shaft 6 allows a sealed structure, leakage loss on the outer circumferential side can be reduced.
以上、実施例で詳述したように2本発明によ。As described above in detail in the examples, two aspects of the present invention have been described.
れば、動翼が外周り、ングを構成する回転軸に植え込ま
れているため、動翼の遠心応力は、各部とも基本的には
圧縮応力となるので、万一飛散状態が発生したと−ても
、従来構造にくら□べて飛散しにくいという利点がある
。Since the rotor blades are installed around the outer circumference of the rotating shaft that constitutes the ring, the centrifugal stress of the rotor blades is basically compressive stress in each part, so in the unlikely event that a flying condition occurs, -It has the advantage of being less likely to scatter compared to conventional structures.
また、外周側は密閉構造畿することが出来るので、外周
側での雫洩損失が従来のものに比べて減少出来るという
利点もある。Furthermore, since the outer circumferential side can have a sealed structure, there is an advantage that leakage loss on the outer circumferential side can be reduced compared to the conventional one.
なお1本発明は実施例においてはタービンを用いて説明
したが、その他の高松機械にも適用出来るものである。Note that although the present invention has been explained using a turbine in the embodiment, it can also be applied to other Takamatsu machines.
第1図は従来のタービンの縦断面図、第2図乃至第5図
は本発明に係る実施例を示すもので。
第2図は縦断面図、第3甲はノズル部−大口。
第4図および第5図は組立説明図である。
1・・・静止軸、 2a、2b・・・静翼、3・・・
回転軸、3a。
3b 、 3a 、 3d−−−分割環状体、 4a
、4.b □−・軸受、 5a、5b。
5c・・・回転体動翼、6・・・出力軸、−7a、、7
b・・・カンプリング部、8・・・ノズル、 8a・・
・ノズル室、9・・・シール、 LOa、10b・・
ケーシング、 lla、1lb−フランジ、12・・・
蒸気導入管、13・・・排気ダク) 、’14”a。
14b、14c、14d、14e、14f、14g=・
支持台、 i”s−:”:ボルト。:・・。
漂4図FIG. 1 is a longitudinal sectional view of a conventional turbine, and FIGS. 2 to 5 show embodiments of the present invention. Figure 2 is a longitudinal sectional view, and Figure 3 is the nozzle part - large mouth. FIGS. 4 and 5 are assembly explanatory views. 1... Stationary shaft, 2a, 2b... Stationary blade, 3...
Rotating shaft, 3a. 3b, 3a, 3d---split ring body, 4a
,4. b □-・Bearing, 5a, 5b. 5c... Rotating body rotor blade, 6... Output shaft, -7a, 7
b... Compling part, 8... Nozzle, 8a...
・Nozzle chamber, 9...Seal, LOa, 10b...
Casing, lla, 1lb-flange, 12...
Steam introduction pipe, 13...exhaust duct), '14''a. 14b, 14c, 14d, 14e, 14f, 14g=.
Support stand, i”s-:”: Bolt. :... Drifting 4
Claims (1)
体動翼を植設した回転体が環装され。 L配回転体がさらに静止チャンバーで環装されているこ
とを特徴とする回転機械。[Scope of Claims] A rotary body having a rotary blade installed thereon is ring-mounted around a stationary member such as a stationary shaft having a stationary blade installed therein. A rotating machine characterized in that the L rotating body is further surrounded by a stationary chamber.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57229294A JPS59120701A (en) | 1982-12-27 | 1982-12-27 | Rotary machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57229294A JPS59120701A (en) | 1982-12-27 | 1982-12-27 | Rotary machine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS59120701A true JPS59120701A (en) | 1984-07-12 |
Family
ID=16889872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57229294A Pending JPS59120701A (en) | 1982-12-27 | 1982-12-27 | Rotary machine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59120701A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5253977A (en) * | 1990-12-14 | 1993-10-19 | Technicatome Societe Technique Pour L'energie Atomique | Multistage pump for two-phase effluents |
GB2554490A (en) * | 2016-09-23 | 2018-04-04 | Intelligent Power Generation Ltd | An axial turbine |
-
1982
- 1982-12-27 JP JP57229294A patent/JPS59120701A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5253977A (en) * | 1990-12-14 | 1993-10-19 | Technicatome Societe Technique Pour L'energie Atomique | Multistage pump for two-phase effluents |
GB2554490A (en) * | 2016-09-23 | 2018-04-04 | Intelligent Power Generation Ltd | An axial turbine |
GB2554477A (en) * | 2016-09-23 | 2018-04-04 | Intelligent Power Generation Ltd | An axial turbine |
GB2554490B (en) * | 2016-09-23 | 2019-02-20 | Intelligent Power Generation Ltd | An axial turbine |
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