US3639080A - Francis-type runner - Google Patents
Francis-type runner Download PDFInfo
- Publication number
- US3639080A US3639080A US84078A US3639080DA US3639080A US 3639080 A US3639080 A US 3639080A US 84078 A US84078 A US 84078A US 3639080D A US3639080D A US 3639080DA US 3639080 A US3639080 A US 3639080A
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- US
- United States
- Prior art keywords
- blade
- runner
- point
- ring
- crown
- 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
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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
-
- 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
- ABSTRACT V The length of the entrance edge of each blade on the side of the crown ring is made longer than that on the side of the shroud ring; and the runner satisfies the ll'ollowing three condi- 1101182 '5 s 350 .yll s where D G 2 D S 9 an angle between the centerline of the runner and a line connecting the points at which the entrance edge of the blade contacts with the crown and shroud rings respectively;
- -y c an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the crown ring and the normal to the tangent at said contact point to the curved surface of the blade;
- y s an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the shroud ring and the normal to the tangent at said contact point to the curved surface of the blade;
- D c an outer diameter of the blade at a point where the blade contacts with the crown ring
- D s an outer diameter of the blade at a point where the blade contacts with the shroud ring.
- the present invention relates to a Francis-type turbine and more specifically a Francis-type runner. More particularly the present invention relates to the contour of the entrance of a Francis-type runner.
- a Francis-type runner comprises a crown ring, a shroud ring and a plurality of blades between them.
- the efficiency of a turbine employing such Francis-type runner does not correspond to the designed effieiency in some cases so that the operation control of the turbine is much adversely affected.
- the present invention provides an improved Francistype runner in which the length of the entrance edge of the blade on the side of the crown ring is made longer than that on the side of the shroud ring; and the Francis-type runner is designed to satisfy the following relations:
- y c an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the crown ring and normal to the tangent at said contact point to the curved surface of the blade;
- FIG. la is a fragmentary sectional view of a Francis-type runner in accordance with the present invention.
- FIG. I bis a side view thereof
- FIG. lc is a horizontal sectional view thereof
- FIG. 2 is a graph illustrating the effieiency of a Franeis-type runner vs. the speed
- FIG. 3 is a graph illustrating the output thereof vs. the guide vane opening.
- FIG. 2 illustrates a test result of a Francis-type turbine in which the efficiency is plotted against the speed for each of several guide vane openings. It is seen that the turbine has two efficiency curves at each one of guide vane openings G G within certain ranges of the speed. This will be described in more detail with reference to the curve for the guide vane opening G...
- the efficiency curve suddenly changes from the point b on the high-efficiency curve to the point r: on the low-efficiency curve.
- the efficiency is gradually increased or decreased accordingly, but when the point e is reached, the efficiency suddenly changes from the point e on the Iow-efficiency curve to the pointf on the highfrequency curve.
- FIG. 3 the output of the turbine at the speed m in FIG. 2 is plotted against the guide vane opening.
- the extensive experiments conducted by the inventor showed that the blade entrance angle 6 indicated in FIG. lb is an important factor in design.
- the angle 6 is an angle between the centerline of the runner and the line connecting the points x and y where entrance edge of the blade 3 contacts with the crown ring and the shroud ring respectively. It is seen that the point x is located left relative to the point y, that is the length of the blade 3 on the side of the crown ring is longer than that on the side of the shroud ring 2. It should be noted that the point x is the vertex of the angle 6.
- the experiments showed that the angle between 15 and 35 is effective for preventing the swirls.
- D,c D s where D c an outer diameter of the blade at a point where it makes contact with the crown ring; and D s an outer diameter of the blade at a point where it makes contact with the shroud ring. Furthermore, it is more advantageous to satisfy the following condition: 71 Yr where y c an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the crown ring and the normal to the tangent at said contact point to the curved surface of the blade; and
- the swirls may be prevented in the passage so that the designed efficiency having no double-efficiency-curve" may be attained.
- I. Francis-type runner comprising a crown ring, a shroud ring and a plurality of blades interconnected therebetween, in which the length of the entrance edge of each blade on the side of said crown ring is longer than that on the side of said shroud ring; and said runner satisfies the following relations:
- D,c an outer diameter of said each blade at a point where said each blade contacts with said crown ring
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Hydraulic Turbines (AREA)
Abstract
The length of the entrance edge of each blade on the side of the crown ring is made longer than that on the side of the shroud ring; and the runner satisfies the following three conditions: 15 DEG </= theta </=35 DEG gamma 1c</= gamma 1s D1 c</= D1s WHERE theta = AN ANGLE BETWEEN THE CENTERLINE OF THE RUNNER AND A LINE CONNECTING THE POINTS AT WHICH THE ENTRANCE EDGE OF THE BLADE CONTACTS WITH THE CROWN AND SHROUD RINGS RESPECTIVELY; gamma 1 C = AN ANGLE BETWEEN THE LINE PASSING THROUGH THE CENTER OF THE RUNNER AND A POINT AT WHICH THE ENTRANCE EDGE OF THE BLADE CONTACTS WITH THE CROWN RING AND THE NORMAL TO THE TANGENT AT SAID CONTACT POINT TO THE CURVED SURFACE OF THE BLADE; gamma 1S = AN ANGLE BETWEEN THE LINE PASSING THROUGH THE CENTER OF THE RUNNER AND A POINT AT WHICH THE ENTRANCE EDGE OF THE BLADE CONTACTS WITH THE SHROUD RING AND THE NORMAL TO THE TANGENT AT SAID CONTACT POINT TO THE CURVED SURFACE OF THE BLADE; D1c = an outer diameter of the blade at a point where the blade contacts with the crown ring; and D1s = an outer diameter of the blade at a point where the blade contacts with the shroud ring.
Description
United States Patent Yamahe [54] FRANCIS-TYPE RUNNER [72] inventor: Masahiro Yamabe, Hitachi, Japan [73] Assignee: Hitachi, Ltd'., Tokyo, Japan [22] Filed: Oct. 26, 1970 [21] Appl. No.: 84,078
[52] U.S.Cl ..4l6/186,416/188 [51] Int. Cl ..F0ld 5/04 [581 FieldotSearch ..416/186,181,185, 179,213 A, 416/241 A, 187,183,192, 188
[56] References Cited UNITED STATES PATENTS 3,224,078 12/1965 Mayne ..4l6/l86 3,224,079 12/1965 Dybvig ..416/186 FOREIGN PATENTS OR APPLICATIONS 691,676 3/1930 France ..416/186 Primary Examiner-Edgar W. Geoghegan Assistant ExaminerClemens Schimikowski Attorney-Craig, Antonelli, Stewart & Hill 1 1 Feb. 1, 1972 [5 7] ABSTRACT V The length of the entrance edge of each blade on the side of the crown ring is made longer than that on the side of the shroud ring; and the runner satisfies the ll'ollowing three condi- 1101182 '5 s 350 .yll s where D G 2 D S 9 an angle between the centerline of the runner and a line connecting the points at which the entrance edge of the blade contacts with the crown and shroud rings respectively;
-y c= an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the crown ring and the normal to the tangent at said contact point to the curved surface of the blade;
y,s an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the shroud ring and the normal to the tangent at said contact point to the curved surface of the blade;
D c= an outer diameter of the blade at a point where the blade contacts with the crown ring; and
D s= an outer diameter of the blade at a point where the blade contacts with the shroud ring.
1 Claims, 5 Drawing Figures PATENTED FEB I I972 F/G. lb
F/G. la
INVENTOR OPEN/N6 0F GU/DEl/A/VE M QQQQR int 3: KQ RBDRDQ MASAHI HO YAMA BE RPM CY Ej skewed.
ATTORNEYS FRANCIS-TYPE RUNNER BACKGROUND OF THE INVENTION The present invention relates to a Francis-type turbine and more specifically a Francis-type runner. More particularly the present invention relates to the contour of the entrance of a Francis-type runner.
In general, a Francis-type runner comprises a crown ring, a shroud ring and a plurality of blades between them. The efficiency of a turbine employing such Francis-type runner does not correspond to the designed effieiency in some cases so that the operation control of the turbine is much adversely affected.
SUMMARY OF THE INVENTION The present invention was made to overcome this problem. In brief, the present invention provides an improved Francistype runner in which the length of the entrance edge of the blade on the side of the crown ring is made longer than that on the side of the shroud ring; and the Francis-type runner is designed to satisfy the following relations:
where an angle between the centerline of the runner and a line connecting the points at which the entrance edge of the blade contacts with the crown and shroud rings respectivcly;
y c an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the crown ring and normal to the tangent at said contact point to the curved surface of the blade;
032 an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the shroud ring and the normal to the tangent at said contact point to the curved surface of the blade;
0,0 an outer diameter of the blade at a point where the blade contacts with the crown ring; and
l),s an outer diameter of the blade at a point where the blade contacts with the shroud ring.
The present invention will become more apparent from the following description of the preferred embodiment thereof taken in conjunction with the accompanying drawing.
BRIEF DESCRIPTION OF THE INVENTION FIG. la is a fragmentary sectional view of a Francis-type runner in accordance with the present invention;
FIG. Ibis a side view thereof;
FIG. lc is a horizontal sectional view thereof;
FIG. 2 is a graph illustrating the effieiency of a Franeis-type runner vs. the speed; and
FIG. 3 is a graph illustrating the output thereof vs. the guide vane opening.
DESCRIPTION OF THE PREFERRED EMBODIMENT FIG. 2 illustrates a test result of a Francis-type turbine in which the efficiency is plotted against the speed for each of several guide vane openings. It is seen that the turbine has two efficiency curves at each one of guide vane openings G G within certain ranges of the speed. This will be described in more detail with reference to the curve for the guide vane opening G... When the speed n is gradually increased from the point a on the curve G the efficiency curve suddenly changes from the point b on the high-efficiency curve to the point r: on the low-efficiency curve. When the turbine speed is increased or decreased between the points d and e, the efficiency is gradually increased or decreased accordingly, but when the point e is reached, the efficiency suddenly changes from the point e on the Iow-efficiency curve to the pointf on the highfrequency curve.
In FIG. 3 the output of the turbine at the speed m in FIG. 2 is plotted against the guide vane opening. These phenomena are observed also in the field units.
The cause of these phenomena is that the flowing water is separated from the runner blades on the side of the crown ring at the runner entrance so that the swirls are superposed upon each other in the passage defined by the runner blades, crown ring and the shroud ring. Because of these swirls the flow rate or the work done by the runner is changed so that the turbine exhibits a high efficiency in some cases or low efficiency in other cases.
These swirls are caused by the contour of the runner entrance. Therefore, it is desired to change the contour of the runner entrance in such a manner that the entering flow will not be separated from the runner blades at the entrance. The extensive experiments conducted by the inventor showed that the blade entrance angle 6 indicated in FIG. lb is an important factor in design. The angle 6 is an angle between the centerline of the runner and the line connecting the points x and y where entrance edge of the blade 3 contacts with the crown ring and the shroud ring respectively. It is seen that the point x is located left relative to the point y, that is the length of the blade 3 on the side of the crown ring is longer than that on the side of the shroud ring 2. It should be noted that the point x is the vertex of the angle 6. The experiments showed that the angle between 15 and 35 is effective for preventing the swirls.
In addition, it was found out that the following relation must be satisfied:
D,c D s where D c an outer diameter of the blade at a point where it makes contact with the crown ring; and D s an outer diameter of the blade at a point where it makes contact with the shroud ring. Furthermore, it is more advantageous to satisfy the following condition: 71 Yr where y c an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the crown ring and the normal to the tangent at said contact point to the curved surface of the blade; and
'y,s an angle between the line passing through the center of the runner and a point at which the entrance edge of the blade contacts with the shroud ring and the normal to the tangent at said contact point to the curved surface of the blade. In the conventional runner, 6 l5 while 'y s 'y c so that the flow is easily separated from the blade.
According to the present invention, when the abovedescribed conditions 15 0 35 D c D, and
71 71 are satisfied, the swirls may be prevented in the passage so that the designed efficiency having no double-efficiency-curve" may be attained.
What is claimed is:
I. Francis-type runner comprising a crown ring, a shroud ring and a plurality of blades interconnected therebetween, in which the length of the entrance edge of each blade on the side of said crown ring is longer than that on the side of said shroud ring; and said runner satisfies the following relations:
'Yi Yr D c D s where 0 an angle between the center line of said runner and a line connecting the points at which the entrance edge of said each blade contacts with said crown ring and said shroud ring respectively;
normal to the tangent at said contact point to the curved surface of said each blade;
D,c= an outer diameter of said each blade at a point where said each blade contacts with said crown ring; and
D,s an outer diameter of said each blade at a point where said each blade contacts with said shroud ring.
UNITED (STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,639,080 Dated February 1, 1972 Inventor(s) Masahiro Yamabe It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Title Page, left column, line 15, which now reads:
"691, 676 3/1930 France. .416/186" should read as follows:
-October 27, 1969 v Japan. 85244/69- Signed and sealed this 11th day of July 1972.
(SEAL) Attest:
EDWARD M. FLET CHER, JR R0 BERT GOTT SC HAL K Atte stin g Offic er Commi ss ioner of Paten ts FORM PO-lOSO (10-69) USCOMM-DC 60376-P89 a u.s GOVERNMENT PRINTING OFFICE I969 o--3ss-a:4
Claims (1)
1. Francis-type runner comprising a crown ring, a shroud ring and a plurality of blades interconnected therebetween, in which the length of the entrance edge of each blade on the side of said crown ring is longer than that on the side of said shroud ring; and said runner satisfies the following relations: 15* < OR = theta < OR = 35* gamma 1c < OR = gamma 1s D1c < OR = D1s where theta an angle between the center line of said runner and a line connecting the points at which the entrance edge of said each blade contacts with said crown ring and said shroud ring respectively; gamma 1c an angle between the line passing through the center of said runner and a point at which the entrance edge of said each blade contacts with said crown ring and the normal to the tangent at said contact point to the curved surface of said each blade; gamma 1s an angle between the line passing through the center of said runner and a point at which the entrance edge of said each blade contacts with said shroud ring and the normal to the tangent at said contact point to the curved surface of said each blade; D1c an outer diameter of said each blade at a point where said each blade contacts with said crown ring; and D1s an outer diameter of said each blade at a point where said each blade contacts with said shroud ring.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US8407870A | 1970-10-26 | 1970-10-26 |
Publications (1)
Publication Number | Publication Date |
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US3639080A true US3639080A (en) | 1972-02-01 |
Family
ID=22182754
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US84078A Expired - Lifetime US3639080A (en) | 1970-10-26 | 1970-10-26 | Francis-type runner |
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US (1) | US3639080A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874819A (en) * | 1972-05-12 | 1975-04-01 | Hitachi Ltd | Francis type runner for pump turbine |
US3964841A (en) * | 1974-09-18 | 1976-06-22 | Sigma Lutin, Narodni Podnik | Impeller blades |
US4108570A (en) * | 1976-02-04 | 1978-08-22 | Hitachi, Ltd. | Francis-type runner for pump-turbine |
US4389160A (en) * | 1979-02-02 | 1983-06-21 | Edison International, Inc. | High speed centrifugal pump and method for operating same at reduced noise levels |
US4479757A (en) * | 1982-09-30 | 1984-10-30 | Dominion Engineering Works Limited | Blade configurations for Francis-type turbine runners |
US4533294A (en) * | 1980-09-25 | 1985-08-06 | Dresser Industries, Inc. | High speed centrifugal pump and method for operating same at reduced noise levels |
US5832606A (en) * | 1996-09-17 | 1998-11-10 | Elliott Turbomachinery Co., Inc. | Method for preventing one-cell stall in bladed discs |
US6135716A (en) * | 1996-08-02 | 2000-10-24 | Ge Energy (Norway) As | Runner for Francis-type hydraulic turbine |
US20050013691A1 (en) * | 2003-06-16 | 2005-01-20 | Kabushiki Kaisha Toshiba | Francis turbine |
US20050042104A1 (en) * | 2003-06-16 | 2005-02-24 | Kabushiki Kaisha Toshiba | Francis turbine |
AT412495B (en) * | 2002-09-26 | 2005-03-25 | Va Tech Hydro Gmbh & Co | WHEEL OF A HYDRAULIC MACHINE |
AT412496B (en) * | 2002-09-26 | 2005-03-25 | Va Tech Hydro Gmbh & Co | WHEEL OF A HYDRAULIC MACHINE |
US20050089404A1 (en) * | 2003-08-11 | 2005-04-28 | Kabushiki Kaisha Toshiba | Francis turbine |
US20050214115A1 (en) * | 2002-07-26 | 2005-09-29 | Helmut Keck | Hydraulic machine rotor |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR691676A (en) * | 1930-01-07 | 1930-10-24 | Sulzer Ag | Rotary pump, in particular boiler feed pump |
US3224079A (en) * | 1964-12-28 | 1965-12-21 | Ruth D Mayne | Method for manufacture of turbine type blower wheels |
US3224078A (en) * | 1963-09-30 | 1965-12-21 | Ruth D Mayne | Method of making a turbine type blower wheel |
-
1970
- 1970-10-26 US US84078A patent/US3639080A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR691676A (en) * | 1930-01-07 | 1930-10-24 | Sulzer Ag | Rotary pump, in particular boiler feed pump |
US3224078A (en) * | 1963-09-30 | 1965-12-21 | Ruth D Mayne | Method of making a turbine type blower wheel |
US3224079A (en) * | 1964-12-28 | 1965-12-21 | Ruth D Mayne | Method for manufacture of turbine type blower wheels |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874819A (en) * | 1972-05-12 | 1975-04-01 | Hitachi Ltd | Francis type runner for pump turbine |
US3964841A (en) * | 1974-09-18 | 1976-06-22 | Sigma Lutin, Narodni Podnik | Impeller blades |
US4108570A (en) * | 1976-02-04 | 1978-08-22 | Hitachi, Ltd. | Francis-type runner for pump-turbine |
US4389160A (en) * | 1979-02-02 | 1983-06-21 | Edison International, Inc. | High speed centrifugal pump and method for operating same at reduced noise levels |
US4533294A (en) * | 1980-09-25 | 1985-08-06 | Dresser Industries, Inc. | High speed centrifugal pump and method for operating same at reduced noise levels |
US4479757A (en) * | 1982-09-30 | 1984-10-30 | Dominion Engineering Works Limited | Blade configurations for Francis-type turbine runners |
US6135716A (en) * | 1996-08-02 | 2000-10-24 | Ge Energy (Norway) As | Runner for Francis-type hydraulic turbine |
US5832606A (en) * | 1996-09-17 | 1998-11-10 | Elliott Turbomachinery Co., Inc. | Method for preventing one-cell stall in bladed discs |
US20050214115A1 (en) * | 2002-07-26 | 2005-09-29 | Helmut Keck | Hydraulic machine rotor |
US7210908B2 (en) | 2002-07-26 | 2007-05-01 | Va Tech Hydro Gmbh | Hydraulic machine rotor |
AT412495B (en) * | 2002-09-26 | 2005-03-25 | Va Tech Hydro Gmbh & Co | WHEEL OF A HYDRAULIC MACHINE |
AT412496B (en) * | 2002-09-26 | 2005-03-25 | Va Tech Hydro Gmbh & Co | WHEEL OF A HYDRAULIC MACHINE |
US20050013691A1 (en) * | 2003-06-16 | 2005-01-20 | Kabushiki Kaisha Toshiba | Francis turbine |
US7128534B2 (en) | 2003-06-16 | 2006-10-31 | Kabushiki Kaisha Toshiba | Francis turbine |
US7198470B2 (en) | 2003-06-16 | 2007-04-03 | Kabushiki Kaisha Toshiba | Francis turbine |
US20050042104A1 (en) * | 2003-06-16 | 2005-02-24 | Kabushiki Kaisha Toshiba | Francis turbine |
US20050089404A1 (en) * | 2003-08-11 | 2005-04-28 | Kabushiki Kaisha Toshiba | Francis turbine |
US7195459B2 (en) * | 2003-08-11 | 2007-03-27 | Kabushiki Kaisha Toshiba | Francis turbine |
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