US1405090A - Semidouble-flow steam turbine - Google Patents
Semidouble-flow steam turbine Download PDFInfo
- Publication number
- US1405090A US1405090A US187961A US18796117A US1405090A US 1405090 A US1405090 A US 1405090A US 187961 A US187961 A US 187961A US 18796117 A US18796117 A US 18796117A US 1405090 A US1405090 A US 1405090A
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- Prior art keywords
- steam
- turbine
- exhaust
- semidouble
- steam turbine
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- 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
- F01D1/023—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 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
Definitions
- the space enclosed by the two uppermost internal guide walls and the top of the exhaust casing (hereinafter called the duct)r of the improved construction described in said application is utilized as a conduit for conducting the whole or a portion of the steam from an intermediate stage of the turbine to the low pressure stage or stages through which the steam flows in the opposite direction or in both directions to the exhaust.
- Fig. 1 is a central, vertical longitudinal section and Fig. 2 a half section taken on the line II-.II of Fig. 1 of an exhaust casing of the kind described in said application adapted for use with a semi-double-tlow turbine in ac- 'exhaust casing d6'.
- FIGS. 3 and 4 are views similar to Figs. 1 and 2 snowing a modified construction f'or use with a semi-double-flow turbine of a differif ent type to that illustrated-in Fig. 1.
- the tur'- bine therein illustrated' is of the type in which a portion only of thev steam is conducted from an intermediate stage Ato one half of the divided low pressure stage through which it flows inv4 the opposite direction to the exhaust.
- the turbinecylinderv is indicated at 5, the exhaust casing at, and the exhaust outlet at 7;
- the internal guide walls are indicated by the numeral 8 andy the curved guides' for defie'cting the steam leaving the last rows of moving blades from an axial into an approximately radial direction of flow by the reference number 9.
- a central transverse web 10 is preferably also provided between the guide walls 8 for a purpose hereinafter described.
- a steam distributing chamber 15 communicates with the other end of the duct 12 and distributes the steam passing through said duct to the guide blades or nozzles 16 of that half of the divided 'low pressure stage of the turbine through which the steam flows in the opposite direction to the exhaust.
- the distributing chamber 15 is similar in shape to that of the collecting chamber 11 shown in section in Figure 2, both ofV saidchambers gradually increasing in cross-sectional area as they approach the duct 12.
- the steam leaving the final rows of moving blades 17, 18 of the divided low pressure stage ofthe turbine will be deflected by the guides 9 into an approximately radial direction of flow, and is divided into segmental portions by the internal guide walls 8 and conducted away to the exhaust in the manner described in said application.
- the central division wall 10 between said guide walls preventsy the The steam abstracted steam Which flows Ylrom the moving ⁇ blades 17 and 18 in opposite directions from intermingling and setting up Whirls and eddies which are objectionable as resulting in a loss of eiiiciency.
- the division 1vall 10 is, hovvever, not essential especially if the curved guides 9 are properly designed so as to defleet the steam into an approximately radial direction, to ensure which additional intermediate curved guides or battles may advantageously be provided.
- a divided-HOW, lowpressure stage comprising energy-abstracting portions through Which steam flows in opposite directions, curved Walls for segmentally dividing the steam discharged from each portion and :tor conducting it in the same general direction, and means cooperating With the Walls to prevent inter ⁇ mixture of steam discharged from the portions, thereby7 avoiding eddying and whirling.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
K. BAUMANN.
SEMIDOUBLE FLOW STEAM TURBINE.
APPLICAHQN FILED AUG.24. 1917.
Patented Jan. 31, 1922.
Q3 SHEETS-SHEET l.
Patented Jan. 31, 1922.
3 SHEETS-SHEET 2.
0 INVENTOR y K. BAUMANN. SEIVIIDOUBLE FLOW STEAM T'URBINE.
APPLICATION FILED AUG.24, 1917. l
Patented Jan. 31, 1922.
3 SHEETS- SHEET 3.
INVENTQRA UiIEn STATES PATENT OFFICE.
'KARL BAUMANN, or URivIsToN, ENGLAND, AssIcrNoR To THE. BRITISH wEsTINc;d HoUsE ELECTRIC AND MANUFACTURING COMPANY LIMITED, A COMPANY ORGANIZED- UNDER THE LAws 0E GREAT BRITAIN.
SEMIDOUBLE-FLOW STEAM TURBINE.
Specification'of Letters-Patent.
Patented Jan. 31, 1922..`
Application filed August 24, 1917. Serial N0. 187,961.
sure stage or stages of the turbine are so arranged that the steam flows through them in opposite directions to the exhaust. Turbines of this kind are commonly called semidouble-flow turbines.
In my application Serial No. 187,963, filed August 24, 1917, there is described an improved construction of turbine exhaust casing and the present invention consists in a modified construction of the turbine exhaust casing set forth in'said application, for use with semi-double-flow turbines.
Asis well known in one form of turbine of this type one or more pipes or conduits have to be provided for conducting a portion of the steam from an intermediate stage to that part of the divided low pressure stage or stages in which the steam flows in the opposite direction to that in which the steam flows through the high pressure stages of the turbine. In another form of semidouble-flow turbine the whole of the steam from an intermediate stage of the turbine is conducted thrpugh one or more pipes or conduits to the low pressure stage or stages through which the steam flows in opposite directions to the exhaust.
According to the "present invention the space enclosed by the two uppermost internal guide walls and the top of the exhaust casing (hereinafter called the duct)r of the improved construction described in said application is utilized as a conduit for conducting the whole or a portion of the steam from an intermediate stage of the turbine to the low pressure stage or stages through which the steam flows in the opposite direction or in both directions to the exhaust.
In the accompanying drawings Fig. 1 is a central, vertical longitudinal section and Fig. 2 a half section taken on the line II-.II of Fig. 1 of an exhaust casing of the kind described in said application adapted for use with a semi-double-tlow turbine in ac- 'exhaust casing d6'.
cordance ywith the present invention; Figs.
3 and 4; are views similar to Figs. 1 and 2 snowing a modified construction f'or use with a semi-double-flow turbine of a differif ent type to that illustrated-in Fig. 1. Referring now to Figs'. 1 andI 2 the tur'- bine therein illustrated' is of the type in which a portion only of thev steam is conducted from an intermediate stage Ato one half of the divided low pressure stage through which it flows inv4 the opposite direction to the exhaust. The turbinecylinderv is indicated at 5, the exhaust casing at, and the exhaust outlet at 7; The internal guide walls are indicated by the numeral 8 andy the curved guides' for defie'cting the steam leaving the last rows of moving blades from an axial into an approximately radial direction of flow by the reference number 9. A central transverse web 10 is preferably also provided between the guide walls 8 for a purpose hereinafter described.
Surrounding the intermediate stage ofthe I turbine from which a portion ofthe'steam is abstracted is a steam collecting chamber l*11 which communicates. with the duct 12 formed between the uppermost internal guidewalls. 8 and theupper portion of the from .this intermediate stage passes fromjthe outer portions of the rowof vmoving blades 18 through openings Min the turbine cylinder into the collecting chamber 11. Y
A steam distributing chamber 15 communicates with the other end of the duct 12 and distributes the steam passing through said duct to the guide blades or nozzles 16 of that half of the divided 'low pressure stage of the turbine through which the steam flows in the opposite direction to the exhaust. The distributing chamber 15 is similar in shape to that of the collecting chamber 11 shown in section in Figure 2, both ofV saidchambers gradually increasing in cross-sectional area as they approach the duct 12. The steam leaving the final rows of moving blades 17, 18 of the divided low pressure stage ofthe turbine will be deflected by the guides 9 into an approximately radial direction of flow, and is divided into segmental portions by the internal guide walls 8 and conducted away to the exhaust in the manner described in said application. The central division wall 10 between said guide walls preventsy the The steam abstracted steam Which flows Ylrom the moving` blades 17 and 18 in opposite directions from intermingling and setting up Whirls and eddies which are objectionable as resulting in a loss of eiiiciency. The division 1vall 10 is, hovvever, not essential especially if the curved guides 9 are properly designed so as to defleet the steam into an approximately radial direction, to ensure which additional intermediate curved guides or battles may advantageously be provided.
The turbine illustrated in Figure 3 is of the kind in Which the Whole ot the steam leaving a row of moving bladesv of an intermediate stage is led tol a divided low pressure stage through Which the steam flows in opposite directions to the exhaust. ln the turbine of this type the Whole of the steam leaving the moving blades 13 passes into'the collecting chamber 11 and Hows through the duct 12 to the guide blades or nozzles 16, 16a of the divided low pressure stage. The distributing chamber 15 is, in this construction, located centrally within the exhaust casing- 6 having on the outer periphery of its lower half a portion 19 which is somewhat triangular in section as seen in Fig. 3. The lower portions of some of the internal guide Walls 8 are carried through the triangular portion 19 of the distributing chamber 15 for the purpose of maintaining said chamber in position Within the exhaust casing 6. That portion of the exhaust casing 6 which is not occupied by the distributing chamber 15 or duct 12 is preferably provided with a division Wall 2O which extends as shown in Figure 4L from theJ outerperiphery of the triangular portion 19 to the side of the exhaust casing, being carried down to near the exhaust outlet 7.` This division Wall 2O per-' forms the same function as the central division VWall 10 shown in the construction illustrated in Figure 1.
claim, as my invention:
l. ln an .axial itlovv steam turbine having a divided low pressure stage "through which the steam ilows in opposite axial directions, a casing provided with partitions 'forming separate inlet and exhaust chambers ior each division osaid stage. y
2. ln steam turbine, a divided-flow, loW- pressure stage comprising energy-abstract- .ing portions through which steam 'flows in ing steam discharged from the portions fromV an. axial to substantially a radial direction, and Walls for segmentally dividing the steam discharged 'from each portion. i
4. In a steam turbine, a divided-HOW, lowpressure stage comprising energy-abstracting portions through Which steam flows in opposite directions, curved Walls for segmentally dividing the steam discharged from each portion and :tor conducting it in the same general direction, and means cooperating With the Walls to prevent inter` mixture of steam discharged from the portions, thereby7 avoiding eddying and whirling.
In testimony whereof I have hereunto subscribed my'name this tenth day of July, 1917.
KARL BAUMANN,
Witnesses:
FREDERICK NixoN, WILFRED MORRIS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US187961A US1405090A (en) | 1917-08-24 | 1917-08-24 | Semidouble-flow steam turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US187961A US1405090A (en) | 1917-08-24 | 1917-08-24 | Semidouble-flow steam turbine |
Publications (1)
Publication Number | Publication Date |
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US1405090A true US1405090A (en) | 1922-01-31 |
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Application Number | Title | Priority Date | Filing Date |
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US187961A Expired - Lifetime US1405090A (en) | 1917-08-24 | 1917-08-24 | Semidouble-flow steam turbine |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3973404A (en) * | 1974-01-23 | 1976-08-10 | Hitachi, Ltd. | Low pressure turbine installation |
US4464902A (en) * | 1981-03-05 | 1984-08-14 | M.A.N. Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | Plural turbochargers having a common exhaust housing |
US5246338A (en) * | 1991-05-28 | 1993-09-21 | Mitsubishi Jukogyo Kabushiki Kaisha | Mixed gas turbine |
EP1992789A1 (en) * | 2007-05-18 | 2008-11-19 | ABB Turbo Systems AG | Exhaust gas turbine casing comprising a support element |
EP2690253A1 (en) * | 2012-07-27 | 2014-01-29 | Siemens Aktiengesellschaft | Low pressure turbine |
-
1917
- 1917-08-24 US US187961A patent/US1405090A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3973404A (en) * | 1974-01-23 | 1976-08-10 | Hitachi, Ltd. | Low pressure turbine installation |
US4464902A (en) * | 1981-03-05 | 1984-08-14 | M.A.N. Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | Plural turbochargers having a common exhaust housing |
US5246338A (en) * | 1991-05-28 | 1993-09-21 | Mitsubishi Jukogyo Kabushiki Kaisha | Mixed gas turbine |
EP1992789A1 (en) * | 2007-05-18 | 2008-11-19 | ABB Turbo Systems AG | Exhaust gas turbine casing comprising a support element |
WO2008142044A2 (en) * | 2007-05-18 | 2008-11-27 | Abb Turbo Systems Ag | Turbine housing |
WO2008142044A3 (en) * | 2007-05-18 | 2009-11-19 | Abb Turbo Systems Ag | Gas outlet housing of an exhaust turbine with a support element |
EP2690253A1 (en) * | 2012-07-27 | 2014-01-29 | Siemens Aktiengesellschaft | Low pressure turbine |
WO2014016272A1 (en) * | 2012-07-27 | 2014-01-30 | Siemens Aktiengesellschaft | Low-pressure turbine |
CN104508243A (en) * | 2012-07-27 | 2015-04-08 | 西门子公司 | Low-pressure turbine |
CN104508243B (en) * | 2012-07-27 | 2016-05-11 | 西门子公司 | low-pressure turbine |
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