US1154648A - Fluid-pressure turbine. - Google Patents
Fluid-pressure turbine. Download PDFInfo
- Publication number
- US1154648A US1154648A US87557414A US1914875574A US1154648A US 1154648 A US1154648 A US 1154648A US 87557414 A US87557414 A US 87557414A US 1914875574 A US1914875574 A US 1914875574A US 1154648 A US1154648 A US 1154648A
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- Prior art keywords
- bucket
- fluid
- disks
- wheel
- pressure turbine
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- 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.)
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- 239000012530 fluid Substances 0.000 description 29
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 3
- 230000002441 reversible effect Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000002184 metal Substances 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D5/00—Pumps with circumferential or transverse flow
Definitions
- PatentedSept. 28, 1915 are PatentedSept. 28, 1915.
- This invention relates to turbines adapted to be operated by steam or other fluid pressure,-and more particularly to that type of turbine in which the Wheel or rotatable part, is composed of a series of thin plates or vanes rigidly secured together with narrow spaces between the same, and mounted to turn with the shaft, the object being to pro- 4 vide additional deflecting surfaces against which'the steam may impinge, and thereby increase the efliciency of the turbine.
- a large number of spacing pieces in the form of buckets or other shapes are rigidly secured between the plates of the Wheel, and so arranged, with reference to location and shape that the steam or other fluid as it is delivered in jets from nozzles directed tangentially passes through the narrow spaces between the plates, against which it operates by adhesion, and impinges against the surfaces.
- the bucket pieces may be substantially crescent shaped with the outer surface concave and the inner surface convex, or both surfaces formed of planes meeting together at an obtuse angle at the center, and may be arranged in radial rows between the plates of the wheel, the buckets of adjacent rows being staggered, or arranged according to any other preferred design, as desired.
- radial arrangement of the aforesaid shaped buckets is particularly adapted for reversible turbines, the surfaces being so disposed that the steam in passing in either direction through the wheel will be deflected repeatedly from one surface to another, that is be tween the inner or outer surfaces, or both inner and outer surfaces of the buckets.
- any desired number of plates with the interposed bucket spacing pieces may be connected up together in this manner, and any number of fluid pressure nozzles of any suitable shape may be arranged around the wheel.
- the series of plates may be divided up into a plurality of sections by stationary walls extending between said sections, each of which may be provided with a separate nozzle or set of nozzles.
- Figure 1 is a longitudinal section of the upper half of a turbine embodying my improvement; Fig. 2, a transverse section of the same; Fig. 3, a longitudinal section. showing a slight modification; Fig. 4, an end elevation of the same; Fig. 5, a transverse section of a portion of the same upon a larger scale, and showing the modified form of buckets; and Fig. 6, a plan of a portion of the rotatable element comprising the disks and bucket pieces.
- the wheel is built up of two sets of plates or disks, 6, there being, in this instance, four plates in each set, rigidly bolted together and mounted on the shaft, 7, within the casing 11.
- the plates are preferably formed of thin metal, and are separated by narrow spaces within which are rigidly secured the bucket distance pieces, 8, which are formed substantially crescent-shaped and arranged in radial rows, the adjacent rows being staggered, as shown.
- the shape and arrangement of these bucket distance pieces may be changed to suit different conditions, the object being that the steam shall impinge with a glancing blow and be repeatedly deflected from the surface of one bucket to the surface of another until substantially all of the energy is absorbed from the steam at the time it reaches the exhaust at the center of the wheel.
- the bucket pieces, 8 are more shallow and the outer surface, instead of being concave, is formed'of two substantially plane'surfaces inclined at an obtuse
- the under surface is similarly formed, thus making two tapered wihgs'extending in opposite directions from the apex of the bucket piece and adapted to give a gentle deflection tothe incoming steamas it passes from one bucket. to another, whereby substantially all shock is eliminated.
- the buckets of the successive radial rows should be spaced with a progressive pitch from'theperiphery toward the center of the wheel whereby the steam travels from the injecting nozzle in a spiral path fro-m one bucket to the nextdown through the wheel totlie outlet.
- the Wings upon the side opposite'the inlet may b'ecut away, as indieated at 8, o thatthe steam from the inlet' nozzl'e.
- any desired number of circumferential rows or rings of bucket pieces maybe employ'edto most efliciently utilize the energy from the steam, and in order'to'take out the final inertia, the last bucket engaged by the steam in the various spiral'paths may be provided with a curved pock'tfS", for deflectingthe steam backward or in'th'e o'ppositedirection as it discharges to the exhaust through the center of the wheel.
- longitudinal ribs, 5 may be provided at intervals, which will serve to deflect the steam into the bucket system of thewheeL sure'fis admitted through the nozzle or nozzles for drivingthe'wheel, it passes through the' 'n'a'rrow spaces between the disks, ,6, and
- a fluid pressure turbine the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces betweenthe same, and bucket pieces secured in radial rows between said disks ⁇ f 5.
- a'fluid pressureturbine the combination'of a casing, arOtatable shaft, a plurality of disks rigidly secured together and mounted upon said shaft, a tangential'noa 'zle for delivering fluid through the spaces between'the dis nd. a plurality of rows bucket piecesrigidly secured in the spaces between said disks, and having inclined Sue faces for deflectingthe fluidlfrom'one bucket 6.
- a fluid pressure turbine the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, bucket pieces having oppositely tapering wings secured between said disks, and tangential nozzles for delivering fluid to the buckets, the outer buckets having one wing cut away.
- a fluid pressure turbine the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, and bucket pieces secured between said disks and having inclined surfaces for deflecting the fluid from one bucket to another, the inner buckets being provided with curved pockets for the final deflection of the fluid.
- a fluid pressure turbine the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, bucket pieces secured between said disks and having inclined surfaces for deflecting the fluid from one bucket to another, and tangential nozzles located in the planes of the respective disks for delivering fluid into the spaces at both sides thereof.
- a fluid pressure turbine the combination of a cylindrical casing having longitudinal ribs upon its inner surface, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, and bucket pieces secured between said disks and having inclined surfaces for deflecting the fluid from one bucket to another.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
C. J. MELLIN.
FLUID PRESSURE TURBINE. APPLICATION FILED DEC. 5. 1914.
1,154,64. PatentedSept. 28, 1915.
3 SHEETS-SHEET 1.
-FIG 1:'8 I I4 8 FIG- 2.-
COLUMBIA PLANOGRAPH- cm. WASHINGTON, D c.
. lVlELLIN FLUID PRESSURE TURBINE.
APPLICATION FILED DEC. 5
Patented Sept. 28, 1915.
3 SHEETSSHEE12.
-FIG 3:-
WITNESSES C. J. IVIELLIN.
FLUID PRESSURE TURBINE.
APPLICATION FILED DEC. 5. 1914.
PatentedSept. 28, 1915.
3 SHEETS-SHEET 3.
CARL J'. MELLIN, OF S CI-IENECTADY, NEW YORK.
FLUID-PRESSURE TURBINE.
Specification of Letters Patent.
Patented Sept. 28, 1915.
Application filed December 5, 1914. Serial No. 875,574.
To all whom it may concern Be it known that I, CARL J. MELLIN, a citizen of the United States, residing at Schenectady, in the county of Schenectady and State of New York, have invented a certain new and useful Improvement in Fluid- Pressure Turbines, of which improvement the following is a specification.
This invention relates to turbines adapted to be operated by steam or other fluid pressure,-and more particularly to that type of turbine in which the Wheel or rotatable part, is composed of a series of thin plates or vanes rigidly secured together with narrow spaces between the same, and mounted to turn with the shaft, the object being to pro- 4 vide additional deflecting surfaces against which'the steam may impinge, and thereby increase the efliciency of the turbine.
According to my improvement, a large number of spacing pieces in the form of buckets or other shapes are rigidly secured between the plates of the Wheel, and so arranged, with reference to location and shape that the steam or other fluid as it is delivered in jets from nozzles directed tangentially passes through the narrow spaces between the plates, against which it operates by adhesion, and impinges against the surfaces.
of the bucket spacing pieces at such an angle as to be deflected from one to another on the general spiral course of the fluid from the nozzles, until it ultimately escapes at the outlet at the center of the wheel. Inthis way the fluid is not abruptly checked at any one bucket, which might produce more or less shock, but is gradually retarded on its course, as it is deflected from one surface to another, whereby the energy of the fluid is gradually absorbed, thus allowing a slower speed of the wheel, but at the same time taking up substantially all of the energy of the steam or other fluid by the time it reaches the exhaust at the center ofthe Wheel. 7,
The bucket pieces may be substantially crescent shaped with the outer surface concave and the inner surface convex, or both surfaces formed of planes meeting together at an obtuse angle at the center, and may be arranged in radial rows between the plates of the wheel, the buckets of adjacent rows being staggered, or arranged according to any other preferred design, as desired. The
radial arrangement of the aforesaid shaped buckets is particularly adapted for reversible turbines, the surfaces being so disposed that the steam in passing in either direction through the wheel will be deflected repeatedly from one surface to another, that is be tween the inner or outer surfaces, or both inner and outer surfaces of the buckets.
Any desired number of plates with the interposed bucket spacing pieces may be connected up together in this manner, and any number of fluid pressure nozzles of any suitable shape may be arranged around the wheel. When a large number of such plates are built up together for producing a turbine of high power, the series of plates may be divided up into a plurality of sections by stationary walls extending between said sections, each of which may be provided with a separate nozzle or set of nozzles.
In the accompanying drawings: Figure 1 is a longitudinal section of the upper half of a turbine embodying my improvement; Fig. 2, a transverse section of the same; Fig. 3, a longitudinal section. showing a slight modification; Fig. 4, an end elevation of the same; Fig. 5, a transverse section of a portion of the same upon a larger scale, and showing the modified form of buckets; and Fig. 6, a plan of a portion of the rotatable element comprising the disks and bucket pieces. I
According to the construction shown in Figs. 1 and 2 of the drawings, the wheel is built up of two sets of plates or disks, 6, there being, in this instance, four plates in each set, rigidly bolted together and mounted on the shaft, 7, within the casing 11. The plates are preferably formed of thin metal, and are separated by narrow spaces within which are rigidly secured the bucket distance pieces, 8, which are formed substantially crescent-shaped and arranged in radial rows, the adjacent rows being staggered, as shown. The shape and arrangement of these bucket distance pieces may be changed to suit different conditions, the object being that the steam shall impinge with a glancing blow and be repeatedly deflected from the surface of one bucket to the surface of another until substantially all of the energy is absorbed from the steam at the time it reaches the exhaust at the center of the wheel.
here a plurality of sets of disks are employed, there may be one or more stationary sets, and the bucket pieces may also be 13, for driving the wheel either in a forangle to each other.
ward or a reverse direction. I
In the modification shown'in Figs. 3 to G inclusive, the bucket pieces, 8 are more shallow and the outer surface, instead of being concave, is formed'of two substantially plane'surfaces inclined at an obtuse The under surface is similarly formed, thus making two tapered wihgs'extending in opposite directions from the apex of the bucket piece and adapted to give a gentle deflection tothe incoming steamas it passes from one bucket. to another, whereby substantially all shock is eliminated.
The buckets of the successive radial rows should be spaced with a progressive pitch from'theperiphery toward the center of the wheel whereby the steam travels from the injecting nozzle in a spiral path fro-m one bucket to the nextdown through the wheel totlie outlet. In the outer circumferential ro'w of buckets the Wings upon the side opposite'the inlet may b'ecut away, as indieated at 8, o thatthe steam from the inlet' nozzl'e. will notbethrown out against the casing,'but will be deflected into the bucket system 'of the wheel; Any desired number of circumferential rows or rings of bucket pieces maybe employ'edto most efliciently utilize the energy from the steam, and in order'to'take out the final inertia, the last bucket engaged by the steam in the various spiral'paths may be provided with a curved pock'tfS", for deflectingthe steam backward or in'th'e o'ppositedirection as it discharges to the exhaust through the center of the wheel.
s As indieatedin'Figs. 3 and 4, several sets of forward and reversejet nozzles, 13 and 13*, may be placed around the periphery of "the wheel and they may also be located in "such positions that each nozzle is in the plane ofone '01"; the supporting disks of "the wheel, so. as to discharge intothe two bucket channels upon bothside's of the disk, and by arranging the successive set-s'of forward and reverse nozzles alternately, the same bucket channels are used whenrfunning in either direction.
In order to prevent a free circulation of sienna-mend the inner surface of the casing, longitudinal ribs, 5, may be provided at intervals, which will serve to deflect the steam into the bucket system of thewheeL sure'fis admitted through the nozzle or nozzles for drivingthe'wheel, it passes through the' 'n'a'rrow spaces between the disks, ,6, and
to another.
WVhen the steam or other fluid under'presrepeated deflections of the steam upon the surfacesofthe buckets assist in gradually absorbing the energy from the steam and greatly increase the efliciency' of the turbine. The construction shown in Figs. 1 and 2 isidentical with'that of my prior pending application Serial No. 871,400,'flled November 10, 191 1., which is a renewal of original applicationSer. No. 708,812, filed July 11, 1912.
I claim as my invention and desire to secure by Letters ,Patent:
1. In a fluid pressure turbine, the combination of a casing, a tangential admission nozzle for the fluid, a plurality ofrotatable disks rigidly secured together with narrow spaces betwee'n'the same and having a central exhaust outlet, and bucket distance pieces having-deflecting surfaces rigidly secured between said disks. "i 2. In a fluid pressure turbine,'the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, and distance pieces secured between said disks and having surfaces'disposed at'an angle to the direction ofth'e fluidfor deflecting thesame to other surfaces.
In a
fluid pressure turbine, the combination of a casing, aplurality ofrotatable between said disks and having outer inclined surfaces and" inner inclined surfaces adapted to deflect the fluid. I
4c. In a fluid pressure turbine, the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces betweenthe same, and bucket pieces secured in radial rows between said disks} f 5. In a'fluid pressureturbine, the combination'of a casing, arOtatable shaft, a plurality of disks rigidly secured together and mounted upon said shaft, a tangential'noa 'zle for delivering fluid through the spaces between'the dis nd. a plurality of rows bucket piecesrigidly secured in the spaces between said disks, and having inclined Sue faces for deflectingthe fluidlfrom'one bucket 6. In a fluidpre'ssure turbine, the combiiiation of casing, 'a plurality of rotatable disks rigidly secured "together with narrow spaces'between the same, and a plurality of rows of bucket pieces secured between said disks, said buckets being formed'with'oppositely tapering wings having inclined surfaces for deflecting the fluid from one bucket to another.
7. In a fluid pressure turbine, the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, bucket pieces having oppositely tapering wings secured between said disks, and tangential nozzles for delivering fluid to the buckets, the outer buckets having one wing cut away.
8. In a fluid pressure turbine, the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, and bucket pieces secured between said disks and having inclined surfaces for deflecting the fluid from one bucket to another, the inner buckets being provided with curved pockets for the final deflection of the fluid.
9. In a fluid pressure turbine, the combination of a casing, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, bucket pieces secured between said disks and having inclined surfaces for deflecting the fluid from one bucket to another, and tangential nozzles located in the planes of the respective disks for delivering fluid into the spaces at both sides thereof.
10. In a fluid pressure turbine, the combination of a cylindrical casing having longitudinal ribs upon its inner surface, a plurality of rotatable disks rigidly secured together with narrow spaces between the same, and bucket pieces secured between said disks and having inclined surfaces for deflecting the fluid from one bucket to another.
CARL J. MELLIN.
Witnesses:
W. R. IVARNER, A. S. FOWLER.
Copies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents, Washington, D. C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US87557414A US1154648A (en) | 1914-12-05 | 1914-12-05 | Fluid-pressure turbine. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US87557414A US1154648A (en) | 1914-12-05 | 1914-12-05 | Fluid-pressure turbine. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1154648A true US1154648A (en) | 1915-09-28 |
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ID=3222712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US87557414A Expired - Lifetime US1154648A (en) | 1914-12-05 | 1914-12-05 | Fluid-pressure turbine. |
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| Country | Link |
|---|---|
| US (1) | US1154648A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3880549A (en) * | 1973-11-19 | 1975-04-29 | Stork Koninklijke Maschf | Turbine |
| US4066381A (en) * | 1976-07-19 | 1978-01-03 | Hydragon Corporation | Turbine stator nozzles |
| US20130142638A1 (en) * | 2010-05-28 | 2013-06-06 | Teruhiko Ohbo | Radial flow steam turbine |
-
1914
- 1914-12-05 US US87557414A patent/US1154648A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3880549A (en) * | 1973-11-19 | 1975-04-29 | Stork Koninklijke Maschf | Turbine |
| US4066381A (en) * | 1976-07-19 | 1978-01-03 | Hydragon Corporation | Turbine stator nozzles |
| US20130142638A1 (en) * | 2010-05-28 | 2013-06-06 | Teruhiko Ohbo | Radial flow steam turbine |
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