US3176960A - Hydraulic turbines or pumps - Google Patents
Hydraulic turbines or pumps Download PDFInfo
- Publication number
- US3176960A US3176960A US271304A US27130463A US3176960A US 3176960 A US3176960 A US 3176960A US 271304 A US271304 A US 271304A US 27130463 A US27130463 A US 27130463A US 3176960 A US3176960 A US 3176960A
- Authority
- US
- United States
- Prior art keywords
- rotor
- throat ring
- pumps
- spherical
- hydraulic
- 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
Links
Images
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
- F03B3/12—Blades; Blade-carrying rotors
- F03B3/14—Rotors having adjustable blades
-
- 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
- F03B11/02—Casings
-
- 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
Definitions
- This invention relates to hydraulic turbines, pumps, and the like, having variable-pitch rotor blades, and has particular reference to variable-pitch hydraulic machines of the type set forth in which blade-tip clearance is maintained constant at all pitch settings by use of a spherical throat ring and blade tips machined to a spherical envelope.
- the throat ring is divided in its median plane in order to permit assembly of the rotor into the throat ring.
- the bottom half of the spherical throat ring is embedded in concrete, the rotor is lowered into position and, then, the top half of the spherical throat ring is lowered over the rotor, seated on the bottom half, and bolted in place.
- This construction is expensive and lacks the rigidity of the completely grouted-in throat ring.
- Another object of the invention is to provide a new and improved method of the type set forth for assembling the rotor into, or removing it from, a one-piece throat ring.
- Another object of the invention is to provide a new and improved grouted-in throat ring for hydraulic turbines, pumps, and the like.
- Another object of the invention is to provide a new and improved throat ring for hydraulic turbines, pumps, and the like, with a rotor or runner assembled therein.
- FIG. 1 is a diametral vertical sectional View of a hydraulic turbine of the variable-pitch propeller type having a throat ring of cylindrical form above, and of spherical form below, the median plane of the runner;
- FIG. 2 is a fragmentary radial vertical section of a hydraulic machine with variable-pitch rotor blades running in a spherical throat ring;
- FIG. 3 is an isometric view of a fragmentary portion of the spherical throat ring showing a form of the invention in relation thereto.
- head-cover extension 13 guides the water through the annular space between runner hub 15 and throat ring 16, in which annular space runner blades 14 rotate. The water is then discharged by Way of draft tube 20.
- Runner assembly or rotor 27 is attached to shaft 17, which shaft 17 is journaled in guide bearings 18 and 19.
- Throat ring 16 is of one-piece construction and is permanently embedded in concrete foundation 21 prior to installation of rotor 27. Said throat ring is characterized by having a spherical bore 24.
- the maximum diameter 22 of rotor 27 is greater than the bore 24 of threat ring 16 above median plane 22A.
- slots 28, see FIGS. 2 and 3 are formed in throat ring 16, one of said slots 23 being formed for each one of the rotor blades 14, such that the tips of said rotor blades may pass axially through the constricted portion of throat ring 16 on their way to median plane 22A.
- a filler piece or other closure member 29 is provided for each of said slots 28, a filler piece or other closure member 29 is provided. Said filler pieces are fixed into slots 28 after rotor 27 has been located in its operating position at median plane 22A.
- such method comprises providing slots 28 in the constricted portion of throat ring 16, said slots being of such number as to correspond to the number of rotor blades 14, and passing the rotor or runner assembly 27 through such constricted portion of said throat ring by passing the tips of said rotor blades through said slots.
- slots 28 are then filled in by filler pieces or other closure members 29.
- a hydraulic machine comprising a rotor having variable pitch rotor blades and a stator having a single piece spherical throat ring embedded in concrete and surrounding said rotor blades, said rotor blades having tip ends corresponding in contour with the internal surface of said throat ring such that a constant clearance is maintained between the tips of said blades and said throat ring at all pitch settings, a constricted portion in said throat ring of lesser diameter than the overall tip diameter of said rotor blades, said throat ring being provided with a plurality of slots extending substantially parallel to the axis of rotation of said rotor along the constricted portion of the throat ring at least to the median plane of said throat ring, each slot being dimensioned to permit the passage of a rotor blade whereby the rotor may be installed or FOREIGN PATENTS removed from the stator, and filler means for closing 1,104,025 1/55 France;
Description
April 1965 R. s. SPROULE 3,176,960
HYDRAULIC TURBINES 0R PUMPS Filed April 8, 1963 3 Sheets-Sheet 1 INVENTOR. "ZOBE'ET S. SF'EOULE ATTO PNEY P 1965 R. s. SPROULE 3,176,960
HYDRAULIC TUR BINES OR PUMPS Filed April 8, 1965 3 Sheets-Sheet 2 20 Fig.2. 13; 3.1
INVENTOR.
ROBERT S. SPEOULE A TTOPNE K April 6, 1965 R. s. SPROULE 3,176,960
HYDRAULIC TURBINES OR PUMPS Filed April 8, 1965 3 Sheets-Sheet 5 INVENTOR ROBERT S- SPEOULE.
United States Patent,
3,176,960 HYDRAULIC TURBINES 0R PUMPS Robert S. Sproule, Montreal, Quebec, Canada, assignor to Dominion Engineering Works, Limited Filed Apr. 8, 1963, Ser. No. 271,304 1 Claim. (Cl. 253-148) This invention relates to hydraulic turbines, pumps, and the like, having variable-pitch rotor blades, and has particular reference to variable-pitch hydraulic machines of the type set forth in which blade-tip clearance is maintained constant at all pitch settings by use of a spherical throat ring and blade tips machined to a spherical envelope.
In contemporary machines of the type set forth, the throat ring is divided in its median plane in order to permit assembly of the rotor into the throat ring. In large vertical machines, the bottom half of the spherical throat ring is embedded in concrete, the rotor is lowered into position and, then, the top half of the spherical throat ring is lowered over the rotor, seated on the bottom half, and bolted in place. This construction is expensive and lacks the rigidity of the completely grouted-in throat ring.
An attempted compromise has been to make the throat ring cylindrical down to the median plane and spherical below this plane, the entire one-piece throat ring being embedded in concrete. This form of construction allows axial assembly of the rotor into the throat ring, but results in large gaps between the blade tips and the cylindrical portion of the throat ring when the blades are in coarse pitch. These gaps permit leakage which lowers the efi'iciency of the machine.
It is an object of the present invention to provide a new and improved method for axially assembling the rotor or runner assembly into, or removing it from, a hydraulic machine having a grouted-in throat ring.
Another object of the invention is to provide a new and improved method of the type set forth for assembling the rotor into, or removing it from, a one-piece throat ring.
Another object of the invention is to provide a new and improved grouted-in throat ring for hydraulic turbines, pumps, and the like.
Another object of the invention is to provide a new and improved throat ring for hydraulic turbines, pumps, and the like, with a rotor or runner assembled therein.
Other objects and advantages of the invention will be apparent from the following description, taken in connection with the accompanying drawings. It will be understood that changes may be made in the details of construction and arrangement of parts shown and described, as the preferred form of the invention has been given by way of illustration only.
Referring to the drawings:
FIG. 1 is a diametral vertical sectional View of a hydraulic turbine of the variable-pitch propeller type having a throat ring of cylindrical form above, and of spherical form below, the median plane of the runner;
FIG. 2 is a fragmentary radial vertical section of a hydraulic machine with variable-pitch rotor blades running in a spherical throat ring; and
FIG. 3 is an isometric view of a fragmentary portion of the spherical throat ring showing a form of the invention in relation thereto.
Referring more particularly to the drawings, wherein similar reference characters designate corresponding parts throughout, water flows, in the operation of the hydraulic machine shown, through spiral casing 19 from ice penstock or other water supply source,-and is directed by fixed stay vanes 11 and adjustable wicket gates 12.
With particular reference to FIG. 2, head-cover extension 13 guides the water through the annular space between runner hub 15 and throat ring 16, in which annular space runner blades 14 rotate. The water is then discharged by Way of draft tube 20. Runner assembly or rotor 27 is attached to shaft 17, which shaft 17 is journaled in guide bearings 18 and 19.
The maximum diameter 22 of rotor 27 is greater than the bore 24 of threat ring 16 above median plane 22A. In order to make axial introduction of runner assembly or rotor 27 into throat ring 16 possible, slots 28, see FIGS. 2 and 3, are formed in throat ring 16, one of said slots 23 being formed for each one of the rotor blades 14, such that the tips of said rotor blades may pass axially through the constricted portion of throat ring 16 on their way to median plane 22A.
For each of said slots 28, a filler piece or other closure member 29 is provided. Said filler pieces are fixed into slots 28 after rotor 27 has been located in its operating position at median plane 22A.
In installations where it is desirable to install rotor 27 from below the median plane, slots 28 and filler pieces 29 would, of course, be appropriately located.
With more particular regard to the new and improved method provided by me for axially assembling the rotor or runner assembly 27 into, or removing it from, the completely grouted-in, one-piece throat ring 16, such method comprises providing slots 28 in the constricted portion of throat ring 16, said slots being of such number as to correspond to the number of rotor blades 14, and passing the rotor or runner assembly 27 through such constricted portion of said throat ring by passing the tips of said rotor blades through said slots. After rotor 27 has been installed in its appropriate position, slots 28 are then filled in by filler pieces or other closure members 29.
It will be understood that, although the invention has been illustrated and described in relation to a hydraulic turbine, its application is not limited to such but, rather, is equally applicable to other hydraulic machines in which blade-tip clearance is maintained constant at all pitch settings by use of a spherical throat ring and blade tips machined to a spherical envelope.
The operation of the device is believed to be apparent from the foregoing.
From the foregoing, it Will be seen that I have provided new and improved means and method for accomplishing all of the objects and advantages of the invention.
I claim:
A hydraulic machine comprising a rotor having variable pitch rotor blades and a stator having a single piece spherical throat ring embedded in concrete and surrounding said rotor blades, said rotor blades having tip ends corresponding in contour with the internal surface of said throat ring such that a constant clearance is maintained between the tips of said blades and said throat ring at all pitch settings, a constricted portion in said throat ring of lesser diameter than the overall tip diameter of said rotor blades, said throat ring being provided with a plurality of slots extending substantially parallel to the axis of rotation of said rotor along the constricted portion of the throat ring at least to the median plane of said throat ring, each slot being dimensioned to permit the passage of a rotor blade whereby the rotor may be installed or FOREIGN PATENTS removed from the stator, and filler means for closing 1,104,025 1/55 France;
said slots when the rotor is installed in the stator. 348,032 5/31 Great Britain References Cited by the Examiner V a UNITED STATES PATENTS 1, 77,04 pp I u Exiaminer' KARL'J. ALBRECHT, Primary Examiner.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US271304A US3176960A (en) | 1963-04-08 | 1963-04-08 | Hydraulic turbines or pumps |
GB10689/64A GB1011718A (en) | 1963-04-08 | 1964-03-13 | Hydraulic turbines or pumps |
US50046365 USRE26095E (en) | 1963-04-08 | 1965-10-06 | Hydraulic turbines or pumps |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US271304A US3176960A (en) | 1963-04-08 | 1963-04-08 | Hydraulic turbines or pumps |
Publications (1)
Publication Number | Publication Date |
---|---|
US3176960A true US3176960A (en) | 1965-04-06 |
Family
ID=23035018
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US271304A Expired - Lifetime US3176960A (en) | 1963-04-08 | 1963-04-08 | Hydraulic turbines or pumps |
US50046365 Expired USRE26095E (en) | 1963-04-08 | 1965-10-06 | Hydraulic turbines or pumps |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US50046365 Expired USRE26095E (en) | 1963-04-08 | 1965-10-06 | Hydraulic turbines or pumps |
Country Status (2)
Country | Link |
---|---|
US (2) | US3176960A (en) |
GB (1) | GB1011718A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3386155A (en) * | 1963-07-01 | 1968-06-04 | Dominion Eng Works Ltd | Method of fitting seal rings to blades |
US3945760A (en) * | 1974-10-29 | 1976-03-23 | Westinghouse Electric Corporation | Outer cylinder for a low pressure turbine apparatus |
US3982840A (en) * | 1974-12-19 | 1976-09-28 | Societe Anonyme Automobiles Citroen | Universal joint with assembly feature |
US4022543A (en) * | 1975-10-21 | 1977-05-10 | Aktiebolaget Karlstads Mekaniska Werkstad | Apparatus for facilitating removal of a marine propeller blade |
US4150914A (en) * | 1976-12-20 | 1979-04-24 | Ab Karlstads Mekaniska Werkstad | Propeller blades |
US4566166A (en) * | 1984-10-03 | 1986-01-28 | Allis-Chalmers Corporation | Method for manufacturing a stay ring bearing stationary guide vanes for a nongated turbine |
US4784569A (en) * | 1986-01-10 | 1988-11-15 | General Electric Company | Shroud means for turbine rotor blade tip clearance control |
WO2001057364A1 (en) * | 2000-02-07 | 2001-08-09 | General Electric Company | Frangible cover for turbofan engine blade removal and access |
US20040052634A1 (en) * | 2001-01-17 | 2004-03-18 | Bjorn Lindberg | Energy generating system |
JP2007016711A (en) * | 2005-07-08 | 2007-01-25 | Toshiba Corp | Stay ring and water turbine having the same |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5954474A (en) | 1996-03-28 | 1999-09-21 | Voith Hydro, Inc. | Hydro-turbine runner |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB348032A (en) * | 1930-02-04 | 1931-05-04 | James Herbert Wainwright Gill | Improvements in or relating to rotors for axial flow hydraulic machines |
US1877048A (en) * | 1928-07-05 | 1932-09-13 | Harry E Popp | Adjustable vane hydraulic turbine |
FR1104025A (en) * | 1954-04-02 | 1955-11-15 | Neyrpic Ets | Improvements to turbine blade orientation control devices |
-
1963
- 1963-04-08 US US271304A patent/US3176960A/en not_active Expired - Lifetime
-
1964
- 1964-03-13 GB GB10689/64A patent/GB1011718A/en not_active Expired
-
1965
- 1965-10-06 US US50046365 patent/USRE26095E/en not_active Expired
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1877048A (en) * | 1928-07-05 | 1932-09-13 | Harry E Popp | Adjustable vane hydraulic turbine |
GB348032A (en) * | 1930-02-04 | 1931-05-04 | James Herbert Wainwright Gill | Improvements in or relating to rotors for axial flow hydraulic machines |
FR1104025A (en) * | 1954-04-02 | 1955-11-15 | Neyrpic Ets | Improvements to turbine blade orientation control devices |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3386155A (en) * | 1963-07-01 | 1968-06-04 | Dominion Eng Works Ltd | Method of fitting seal rings to blades |
US3945760A (en) * | 1974-10-29 | 1976-03-23 | Westinghouse Electric Corporation | Outer cylinder for a low pressure turbine apparatus |
US3982840A (en) * | 1974-12-19 | 1976-09-28 | Societe Anonyme Automobiles Citroen | Universal joint with assembly feature |
US4022543A (en) * | 1975-10-21 | 1977-05-10 | Aktiebolaget Karlstads Mekaniska Werkstad | Apparatus for facilitating removal of a marine propeller blade |
US4150914A (en) * | 1976-12-20 | 1979-04-24 | Ab Karlstads Mekaniska Werkstad | Propeller blades |
US4566166A (en) * | 1984-10-03 | 1986-01-28 | Allis-Chalmers Corporation | Method for manufacturing a stay ring bearing stationary guide vanes for a nongated turbine |
US4784569A (en) * | 1986-01-10 | 1988-11-15 | General Electric Company | Shroud means for turbine rotor blade tip clearance control |
WO2001057364A1 (en) * | 2000-02-07 | 2001-08-09 | General Electric Company | Frangible cover for turbofan engine blade removal and access |
US6375410B2 (en) | 2000-02-07 | 2002-04-23 | General Electric Company | Frangible cover for turbofan engine blade removal and access |
US20040052634A1 (en) * | 2001-01-17 | 2004-03-18 | Bjorn Lindberg | Energy generating system |
US7011501B2 (en) * | 2001-01-17 | 2006-03-14 | Water Crossing, Inc. | Energy generating system |
JP2007016711A (en) * | 2005-07-08 | 2007-01-25 | Toshiba Corp | Stay ring and water turbine having the same |
Also Published As
Publication number | Publication date |
---|---|
USRE26095E (en) | 1966-10-11 |
GB1011718A (en) | 1965-12-01 |
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