US2026436A - Control device for impulse turbines - Google Patents
Control device for impulse turbines Download PDFInfo
- Publication number
- US2026436A US2026436A US702246A US70224633A US2026436A US 2026436 A US2026436 A US 2026436A US 702246 A US702246 A US 702246A US 70224633 A US70224633 A US 70224633A US 2026436 A US2026436 A US 2026436A
- Authority
- US
- United States
- Prior art keywords
- water
- control device
- scroll case
- jet
- impulse
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/146—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by throttling the volute inlet of radial machines or engines
-
- 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
- F03B15/00—Controlling
- F03B15/02—Controlling by varying liquid flow
-
- 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
- the jet escaping through the orifice has the proper axial and tangential ve-v locity-components without it being necessary to provide guide blades in the interior of the case.
- This jet then impinges on the buckets of a runner disposed in front of the orifice and causes it to rotate with a uniform speed.
- the control of the flow is effected by contracting the cross section of the inlet pipe by a needle-shaped deviceor the like.
- a similar regula ing device is known for reaction turbines, but itsworking is quite different from that of the present invention.
- reaction turbines where the scroll case runs always full of water, the thickness of the water jet imparting the runner leaves the same and the angles of attack change, whilst in impulse turbines with an annular jet with free internal cylindric surface and formed by diversing of the water over a circular overrunning edge at the regulation with a control device about the present invention the angles of attack rest independent-from the degree of regulation and only the wall thickness of the annular jet varies.
- the angles of attack rest independent-from the degree of regulation and only the wall thickness of the annular jet varies.
- Fig. l of the drawings is a longitudinal sec- 5 tion and Fig. 2 is a section on the axis through the spiral casing of a turbine with a normal flow of water passing through it.
- Fig. 3 shows the same view as l with the control device in a part gate position.
- Figs. 4 and 5 represent the i0 longitudinal section of other examples of execution.
- the turbine consists in a spiral- -casing l with an orifice in the side wall the edge of which is the circular weir 2 over which the 15 jet escapes.
- the water entering by the inlet pipe 3 form in the casing a real whirl or vortex.
- the flowing over on the circular weir 2 forms a rotating jet of annular cross section 4, which has both axial 20 and tangential velocity components. This jet then impinges on the runner buckets placed in front of the orifice.
- Fig. 1 and efflcient streamlined rotatable control device 5 is situated in 25 the first part of the scroll case, and can be considered as a part of the spiral case giving the necessary variable feature that will influence the characteristics of the water whirling round in the case.
- control device 5 If the control device 5 is situated so as not to alter materially the flow distribution that obtains in the plain scroll case (Fig. 1), the flow characteristics will remain as it would be in the plain scroll case and with a proper design the annular jet 4 will have a constant thickness.
- the flow in the spiral-casing will be influenced in such a manner, as to cause the annular jet to escape from the casing along 40 the circular weir 2 with different thicknesses 4', 4", without changing materially the axial and tangential velocity components and the angle of the jet defined thereby.
- These devices are on the waterside formed as a part of the spiral and can be actuated by any arrangement 8. They influence the whirling water and the annular jet in the same manner as the streamlined vane shown in Fig. 3.
- the scope of the invention covers also the arrangement of the control device at the beginning of the spiral path of the water in the scroll case with other types of construction than those of Figs. 1 to 5.
- a sliding regulating device could be arranged or others.
- a scroll case provided with a circular opening in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface, with a regulating device located in the interior of the scroll case in the first part of the spiral path of the water.
- a scroll case provided with a circular opening in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface
- a regulating device located in the interior of the scroll case in the first part of the spiral path of the water, said regulating device being a streamlined vane washed by the water on both sides.
- a scroll case provided with a circular opening 5 in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface
- a regulating device located in the interior of the scroll case in the first part of the spiral path of the water, said regulating device being in the form or a flap hinged on the scroll case.
- a scroll case provided with a circular opening in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface
- a regulating device located in the interior of the scroll case in the first part of the spiral path of the water, said regulating device being in the form of a flexible elastic sheet forming a part of the internal scroll wall or the scroll case.
Description
1935- i M. REIFFENSTEIN 2,025,436
CONTROL DEVICE FOR IMPULSE TURBINES Filed Dec. 15, 1955 2 s t -sh t 1 DecQ 1935- M. IEIFFENSTEIN 2,026,436
CONTROL DEVICE FOR IMPULSE TURBINES Filed Dec. 1a, 1953 2 Sheets-Sheet 2 Patented Dec. 31, 1935 UNITED STATES PATENT OFFICE 2,026,436 CONTROL DEVICE FOR IMPULSE TURBINES Manfred Reifienstein, Vienna,'Austria Application December 13, 1933, Serial No. 702,246 In Austria January 4, 1933 4 Claims; (01. 253-124) In certain hydraulic impulse-turbines known to the art of the type having a spiral case, the runner is actuated by a jet of annular cross section. This annular jet is formed by the overflowing of a rotating mass of water over the edge of a circular orifice located in one of the walls of the scroll case. The jet escaping through the orifice has the proper axial and tangential ve-v locity-components without it being necessary to provide guide blades in the interior of the case. This jet then impinges on the buckets of a runner disposed in front of the orifice and causes it to rotate with a uniform speed. In a turbine of this type as known in the art, the control of the flow is effected by contracting the cross section of the inlet pipe by a needle-shaped deviceor the like. By this method, however, even when streamlined arrangements are employed, the control is effected chiefly by a throttling action on the water which is unfavorable for maintaining efliciency at part gates.
A perfect control, without losses, would be possible only by means of a scroll case variable in its whole shape. It has been found according to the invention that it is sumcient to vary the shape of a part of the scroll case to influence the whole flow therein. The flow through the orifice is not then perfectly symmetrical around the axis of the turbine but theory and experience have proved that the variations in thickness of the annular ring of water issuing from the orifice has no bad effect on the efliciency of the machine. It is sufiicient in practice to' use a device, situated not at the inlet proper of the scroll case but in the interior of the case itself in the first part of the spiral path of the water so as to influence both the incoming water and the water already whirling round in the case imparting to the fiow the proper directions. The effect is as if the curvature of the whole scroll case itself has been altered. That is, the control is effected by guiding and not by throttling.
A similar regula ing device is known for reaction turbines, but itsworking is quite different from that of the present invention. In reaction turbines where the scroll case runs always full of water, the thickness of the water jet imparting the runner leaves the same and the angles of attack change, whilst in impulse turbines with an annular jet with free internal cylindric surface and formed by diversing of the water over a circular overrunning edge at the regulation with a control device about the present invention the angles of attack rest independent-from the degree of regulation and only the wall thickness of the annular jet varies. Thus it is possible to maintain very good efliciencyat part gates.
In Figs. 1 to 5 several modes of execution of the present invention are represented.
Fig. l of the drawings is a longitudinal sec- 5 tion and Fig. 2 is a section on the axis through the spiral casing of a turbine with a normal flow of water passing through it. Fig. 3 shows the same view as l with the control device in a part gate position. Figs. 4 and 5 represent the i0 longitudinal section of other examples of execution.
In all examples the turbine consists in a spiral- -casing l with an orifice in the side wall the edge of which is the circular weir 2 over which the 15 jet escapes.
The water entering by the inlet pipe 3 form in the casing a real whirl or vortex. The flowing over on the circular weir 2 forms a rotating jet of annular cross section 4, which has both axial 20 and tangential velocity components. This jet then impinges on the runner buckets placed in front of the orifice.
In the example, of Fig. 1 and efflcient streamlined rotatable control device 5 is situated in 25 the first part of the scroll case, and can be considered as a part of the spiral case giving the necessary variable feature that will influence the characteristics of the water whirling round in the case.
If the control device 5 is situated so as not to alter materially the flow distribution that obtains in the plain scroll case (Fig. 1), the flow characteristics will remain as it would be in the plain scroll case and with a proper design the annular jet 4 will have a constant thickness.
If the control device is moved to the position shown in Fig. 3, the flow in the spiral-casing will be influenced in such a manner, as to cause the annular jet to escape from the casing along 40 the circular weir 2 with different thicknesses 4', 4", without changing materially the axial and tangential velocity components and the angle of the jet defined thereby.
In the example shown in Figs. 4 and 5, a part 4 On the wall of the spiral-casing l'a flap 6 .is articulated with the center of rotation at I (Fig. 4) or an elastic flexible sheet 9 is provided for (Fig. 5). These devices are on the waterside formed as a part of the spiral and can be actuated by any arrangement 8. They influence the whirling water and the annular jet in the same manner as the streamlined vane shown in Fig. 3.
The scope of the invention covers also the arrangement of the control device at the beginning of the spiral path of the water in the scroll case with other types of construction than those of Figs. 1 to 5. For instance a sliding regulating device could be arranged or others.
Having thus fully described the invention what is claimed as new and desired to be secured by Letters Patent is:-
1. In an impulse turbine the combination of a scroll case provided with a circular opening in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface, with a regulating device located in the interior of the scroll case in the first part of the spiral path of the water.
2. In an impulse turbine the combination of a scroll case provided with a circular opening in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface, with a regulating device located in the interior of the scroll case in the first part of the spiral path of the water, said regulating device being a streamlined vane washed by the water on both sides.
3. In an impulse turbine the combination of a scroll case provided with a circular opening 5 in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface, with a regulating device located in the interior of the scroll case in the first part of the spiral path of the water, said regulating device being in the form or a flap hinged on the scroll case.
4. In an impulse turbine the combination of a scroll case provided with a circular opening in at least one side wall formed as a circular weir and opening to substantially atmospheric pressure to provide a rotating annular jet having a free inner surface, with a regulating device located in the interior of the scroll case in the first part of the spiral path of the water, said regulating device being in the form of a flexible elastic sheet forming a part of the internal scroll wall or the scroll case.
MANFRED REIFF'ENSTEIN.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT2026436X | 1933-01-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2026436A true US2026436A (en) | 1935-12-31 |
Family
ID=3689665
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US702246A Expired - Lifetime US2026436A (en) | 1933-01-04 | 1933-12-13 | Control device for impulse turbines |
Country Status (1)
Country | Link |
---|---|
US (1) | US2026436A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3149820A (en) * | 1961-06-28 | 1964-09-22 | Silencer Mfg Inc | Gas turbine speed control |
US3313518A (en) * | 1966-02-25 | 1967-04-11 | Garrett Corp | Turbine control |
WO2009043781A2 (en) * | 2007-09-26 | 2009-04-09 | Continental Automotive Gmbh | Rotor housing comprising a variably adjustable flow channel |
-
1933
- 1933-12-13 US US702246A patent/US2026436A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3149820A (en) * | 1961-06-28 | 1964-09-22 | Silencer Mfg Inc | Gas turbine speed control |
US3313518A (en) * | 1966-02-25 | 1967-04-11 | Garrett Corp | Turbine control |
WO2009043781A2 (en) * | 2007-09-26 | 2009-04-09 | Continental Automotive Gmbh | Rotor housing comprising a variably adjustable flow channel |
WO2009043781A3 (en) * | 2007-09-26 | 2010-11-18 | Continental Automotive Gmbh | Spiral-shaped rotor housing comprising a variably adjustable flow channel |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2944786A (en) | Super and subsonic vaneless nozzle | |
US5441384A (en) | Hydraulic turbine and guide gate apparatus and runner apparatus therefor | |
US3076480A (en) | Fluid conduits | |
US3411451A (en) | Centrifugal pump inlet elbow | |
US1771711A (en) | Split guide blade for centrifugal pumps | |
US3743436A (en) | Diffuser for centrifugal compressor | |
US2026436A (en) | Control device for impulse turbines | |
US3384022A (en) | Centrifugal pump | |
US2614747A (en) | Gaseous flow regulator | |
US1096057A (en) | Water and wind engine. | |
US1606887A (en) | Hydraulic ttjreine | |
JPS5944482B2 (en) | axial turbine | |
US2944729A (en) | Induction and discharge means for effective camber control | |
US1276154A (en) | Exhaust connecting branch for turbines. | |
US3138317A (en) | Surge control mechanism for turbomachinery | |
US1748892A (en) | Hydraulic process and apparatus | |
US2064313A (en) | Hydraulic power apparatus | |
US1728435A (en) | Hydraulic turbine | |
US807025A (en) | Regulating-nozzle. | |
US444938A (en) | Thomas w | |
US1948478A (en) | Hydraulic turbine | |
US1803220A (en) | Water turbine | |
CN109763928B (en) | Guide vane and fluid machine | |
JP2017031923A (en) | Runner and hydraulic machine | |
US3368493A (en) | Guide vane arrangement |