US1412257A - Turbine - Google Patents

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Publication number
US1412257A
US1412257A US396208A US39620820A US1412257A US 1412257 A US1412257 A US 1412257A US 396208 A US396208 A US 396208A US 39620820 A US39620820 A US 39620820A US 1412257 A US1412257 A US 1412257A
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Prior art keywords
jet
buckets
wheel
turbine
nozzle
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US396208A
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Gustav B Petsche
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B1/00Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on blades or like rotors, e.g. Pelton wheels; Parts or details peculiar thereto
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/24Rotors for turbines
    • F05B2240/241Rotors for turbines of impulse type
    • F05B2240/2411Pelton type
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Definitions

  • My invention relates to turbine wheels in which a fluid jet of high velocity is used as the impelling means and it hasofor its main object to provide aturbine construction having in connection with means for converting the pressure of a fluid into' velocity a nozzle extension of decreasing sectional area extending around the wheel and having a narrow slot like op'eningthrough which the fluid issues into the buckets in a narrow jet, the buckets being of the jetreversing type and set with their jet receiving edges approximately tangential to the narrowv jet.
  • Figure l is a side elevation of a. Pelton wheel turbine provided with my improvement, a portion of the casing being removed to Show the side of the" wheel. and the nozzle and nozzle extension being shown in section.
  • Figure 2 is an elevation of the construction shown in Fig; 1 taken as on the section line .22 of Fig. 1. I i
  • Figure 3 is a plan viewtakenas on the section line 3 3 of Fig. l.
  • Figure i is a somewhat enlarged detailed view showing one ofthe buckets of the wheel and illustratingthemotion of the jet over the buckets.
  • Figure 5 is a view taken on the section line 5-5 of Fig. at the section being continued through he nozzle extension and showing the angle with which the jet portion comes in contact with the bucket.
  • Figure 6 is a sectional view taken as on the line 6-6.of Fig. 5 and illustrating the travel of the fluid over the face of the bucket.
  • F igure? is a view illustratinga modification been; bucket arrangement with reference to the opening of'the nozzle extension which is of special utility where narrow and very high velocity jetsare employed.
  • Figure 8 is a plan view of a turbine of the Pelton wheel type set horizontally and provided with my nozzle extension and with a bucket arrangement which is of a special dicated at D nozzle extension.
  • FIG. 10 is a diagrammatic view illus tra'ting the arrangement of the buckets in the wheel shown in Figs. 8 and 9.
  • a Flgs. 1 and 2; is'the casing of the Pelton wheel;
  • B is'thesha-ft' OftllG wheel;
  • C a
  • the curved faces of the buckts are indicated at D D see Fig. 4.; and the buckets are formed with the. top portions as in- E indicates the nozzle by.
  • E. F indicates my nozzle extension which extends from the nozzle It around the wholeor any desired part of the wheel and isfformedzwith gradually .contracted area so that the high velocity j'et entering. from the nozzle will directed by the curved form of the extension in'ward toward the wheel and will issue through the opening 01'' slot on the inner face-of the extension. In my construction this slot is made narrow so that the jet issuing through it will be narrow;
  • the turbine wheel here shown contrary to the Pelton wheel type is set horizontally, the wheel being indicated at C.
  • the buckets are so shaped and attached to the wheel that the water issuing from the nozzle extension indicated at f and through the narrow opening or slot 7 will enter at the top of the buckets and after passing over their curved faces, leave them at the bottom.
  • These specially formed buckets are indicated at I, I and are dia grammatically shown in operative position with regard to the slot 7 in Fig. 10.
  • the size of the jet is regulated by a shutter or swinging gate J which is a well known device for regulatiFng flow and takes the place of nozzle E in It will be obvious for the reason that my construction provides for the impact of the narrow high velocity jet upon any desired number of buckets attached to thewheel that it is practical for me to make a wheel with a smaller number of buckets than in the usual construction for the given power and also that I am enabled to use a wheel of smaller diameter and revolve it with higher speed which is of manifest advantage esspecially where this turbine is to be used for generating electric power and where the wheel and the generator are mounted on the same shaft.
  • a very notable advantage of my construct-ion is that when the wheel is to' be used under a partial load the size of: the jet is cut down proportionately.
  • the high velocity jet does not come in contact with the first buckets registering with the opening of the nozzle extension but owing to the contraction of the nozzle extension the jet does come in contact with the final buckets and always impinges upon them at the proper angle and with full velocity, acting, therefore, with high efiiciency on a smaller number of buckets.
  • jet receiving edge as definin not the mathematical edge of the bucket but that portion otthe concave bucket adjacent to the mathematical edge against which the jet first impinges.
  • a nozzle extension For receiving and guiding the fiuid from said means extending around the wheel with gradually contracting areaand having a narrow slot like opening registering with the tangential jet receiving edges of the buckets and through which opening the nozzle extension delivers high velocity fluid tangentially into the buckets.

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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)

Description

G. B. PETS'CHE.
TURBINE.
APPLICATION FILED JULY 14.1920.
Patented Apr. 11, 1922 I [MENTOR 4;, /3 PM 4; '4 Tranusr TURBINE.
Application filed M 14;
To'allwlwmit may concern. v 7
Be it known that I, GUSTAV B. Pnrs'orrn, a citizen ofthe United States of America and resident of Yonkers, in the county of lVestchesteran'd State. of New York, have invented a'certain new and useful Improvement in Turbines, of which thefollo'wing is a true and exact description, reference being had to the accompanying drawings, which form a part thereof. 7 I
My invention relates to turbine wheels in which a fluid jet of high velocity is used as the impelling means and it hasofor its main object to provide aturbine construction having in connection with means for converting the pressure of a fluid into' velocity a nozzle extension of decreasing sectional area extending around the wheel and having a narrow slot like op'eningthrough which the fluid issues into the buckets in a narrow jet, the buckets being of the jetreversing type and set with their jet receiving edges approximately tangential to the narrowv jet.
Referencebeing now had to the drawings in which my invention is illustrated.
Figure l is a side elevation of a. Pelton wheel turbine provided with my improvement, a portion of the casing being removed to Show the side of the" wheel. and the nozzle and nozzle extension being shown in section.
Figure 2 is an elevation of the construction shown in Fig; 1 taken as on the section line .22 of Fig. 1. I i
Figure 3 is a plan viewtakenas on the section line 3 3 of Fig. l.
,Figure i is a somewhat enlarged detailed view showing one ofthe buckets of the wheel and illustratingthemotion of the jet over the buckets.
Figure 5 is a view taken on the section line 5-5 of Fig. at the section being continued through he nozzle extension and showing the angle with which the jet portion comes in contact with the bucket.
Figure 6 is a sectional view taken as on the line 6-6.of Fig. 5 and illustrating the travel of the fluid over the face of the bucket.
F igure? is a view illustratinga modification been; bucket arrangement with reference to the opening of'the nozzle extension which is of special utility where narrow and very high velocity jetsare employed.
Figure 8 is a plan view of a turbine of the Pelton wheel type set horizontally and provided with my nozzle extension and with a bucket arrangement which is of a special dicated at D nozzle extension.
Specification of Letters Patent. Patntie d 1920. seriarno. 396,208. i
In this view the turbine wheel is not see -tioned but the section is taken through the nozzle extension on the line' 88 of F F gure 9 1s a sectlonal view taken as o the hue 9"9 of Fig. 8 and i Figure 10 is a diagrammatic view illus tra'ting the arrangement of the buckets in the wheel shown in Figs. 8 and 9. A Flgs. 1 and 2; is'the casing of the Pelton wheel; B is'thesha-ft' OftllG wheel; C, a
wheel'which is formed, as shown, with pro- Ijecti'ng bucket holding armsgC reinforced by shoulders as indicated at C3. D indicates the buckets whi'eh are secured to the arms C V and which, as shown-in Figs. 1, 2 arr-d3, are."
of the usual type ofejet reversing, buckets made double with a single dividing edge as These buckets are made indicated at D preferably with projecting ribs D on' their 1 back, seeFig. 5, which extend into'slotsa C on the arms 6 and are secured in place by screws. The curved faces of the buckts are indicated at D D see Fig. 4.; and the buckets are formed with the. top portions as in- E indicates the nozzle by.
means of, which the pressure ofthc'fluidis converted into velocity, the nozzle made regulable as by an ad ustable cone or snnilar device indicated at E. F indicates my nozzle extension which extends from the nozzle It around the wholeor any desired part of the wheel and isfformedzwith gradually .contracted area so that the high velocity j'et entering. from the nozzle will directed by the curved form of the extension in'ward toward the wheel and will issue through the opening 01'' slot on the inner face-of the extension. In my construction this slot is made narrow so that the jet issuing through it will be narrow;
'at the same angle and will cont-inuein'con- It will be observed that V whatever portlon of the narrow high velocity tact with the bucket at that-same angle, av in Fig. 5, so long as the bucket. remains in com munication with the slot or, opening ofthe j The jet reversing bucket or buckets are so located that their jet receiv in ed estbv which I mean that )orti'on of I the concave face of the bucket-against which the jet first impinges, are approximately tangent to the narrow jet issuing from the slot.
In the modification of my invention shown in Figs. 8 and 9, the turbine wheel here shown contrary to the Pelton wheel type is set horizontally, the wheel being indicated at C. The buckets are so shaped and attached to the wheel that the water issuing from the nozzle extension indicated at f and through the narrow opening or slot 7 will enter at the top of the buckets and after passing over their curved faces, leave them at the bottom. These specially formed buckets are indicated at I, I and are dia grammatically shown in operative position with regard to the slot 7 in Fig. 10. In the construction shown in Fig. 8 the size of the jet is regulated by a shutter or swinging gate J which is a well known device for regulatiFng flow and takes the place of nozzle E in It will be obvious for the reason that my construction provides for the impact of the narrow high velocity jet upon any desired number of buckets attached to thewheel that it is practical for me to make a wheel with a smaller number of buckets than in the usual construction for the given power and also that I am enabled to use a wheel of smaller diameter and revolve it with higher speed which is of manifest advantage esspecially where this turbine is to be used for generating electric power and where the wheel and the generator are mounted on the same shaft. A very notable advantage of my construct-ion is that when the wheel is to' be used under a partial load the size of: the jet is cut down proportionately. In this case, as indicated for instance in Fig. 8, the high velocity jet does not come in contact with the first buckets registering with the opening of the nozzle extension but owing to the contraction of the nozzle extension the jet does come in contact with the final buckets and always impinges upon them at the proper angle and with full velocity, acting, therefore, with high efiiciency on a smaller number of buckets.
I have heretofore referred to that'portion of the concave jet reversing buckets against which the jet first impinges as the jet receiving edges of the buckets, and in my claims I use the term jet receiving edge as definin not the mathematical edge of the bucket but that portion otthe concave bucket adjacent to the mathematical edge against which the jet first impinges.
Having now described my invention, what I claim as new and desire to secure by Letters Patent, is:
1. In combination with a turbine wheel having jet reversing buckets extending radially from the wheel with their jet receiving edges located so as to be approximately tangential to the plane of the impelling jet, means for converting the pressure of a fluid into velocity, a nozzle extension For receiving and guiding the fiuid from said means extending around the wheel with gradually contracting areaand having a narrow slot like opening registering with the tangential jet receiving edges of the buckets and through which opening the nozzle extension delivers high velocity fluid tangentially into the buckets.
2. In combination with a turbine wheel having jet reversing buckets extending radially from the wheel with their jet receiving edges located so as to be approximately tangential to the plane of the impelling jet, said buckets extending alternately in opposite directions and having their tangential jet receiving edges located to register with the narrow slot like opening from the nozzle extension, means for converting the pressure of a fluid into velocity a nozzle extension for receiving and guiding the fluid from said means extending around the wheel with gradually contracting area and having a narrow slot like opening registering with the tangential jct'receiving edges of the buckets and throu h which 0 Jenin the nozzle extension delivers high velocity fluid tangentially into the buckets.
GUSTAV B. PETSCI-IE.
US396208A 1920-07-14 1920-07-14 Turbine Expired - Lifetime US1412257A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3479124A (en) * 1966-09-22 1969-11-18 Koninkl Mas Fab Stork Nv Turbine
US3883265A (en) * 1973-09-12 1975-05-13 Stork Koninklijke Maschf Turbine
US4177005A (en) * 1975-09-06 1979-12-04 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft (M.A.N.) Variable-throat spiral duct system for rotary stream-flow machines
US4295788A (en) * 1980-03-10 1981-10-20 Terry Corporation Turbine wheel and nozzle arrangement
RU2298652C2 (en) * 2004-09-27 2007-05-10 Общество с ограниченной ответственностью "Турбо-Веста" Method of control centripetal turbine with vaneless guide assembly
WO2018185004A3 (en) * 2017-04-03 2019-01-03 Grohe Ag RADIATOR, IN PARTICULAR FOR A SANITARY BREAD HEAD, WITH A RUNNING BUCKET THEREFORE INSTALLED AND EQUIPPED TO SHARE A WATER SPREAD AND DISCONNECT PARTIAL FLOWS

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3479124A (en) * 1966-09-22 1969-11-18 Koninkl Mas Fab Stork Nv Turbine
US3883265A (en) * 1973-09-12 1975-05-13 Stork Koninklijke Maschf Turbine
US4177005A (en) * 1975-09-06 1979-12-04 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft (M.A.N.) Variable-throat spiral duct system for rotary stream-flow machines
US4295788A (en) * 1980-03-10 1981-10-20 Terry Corporation Turbine wheel and nozzle arrangement
RU2298652C2 (en) * 2004-09-27 2007-05-10 Общество с ограниченной ответственностью "Турбо-Веста" Method of control centripetal turbine with vaneless guide assembly
WO2018185004A3 (en) * 2017-04-03 2019-01-03 Grohe Ag RADIATOR, IN PARTICULAR FOR A SANITARY BREAD HEAD, WITH A RUNNING BUCKET THEREFORE INSTALLED AND EQUIPPED TO SHARE A WATER SPREAD AND DISCONNECT PARTIAL FLOWS
CN110678613A (en) * 2017-04-03 2020-01-10 高仪股份公司 Jet former with working vanes for dividing and diverting the water flow, especially for sanitary shower heads
US11311893B2 (en) 2017-04-03 2022-04-26 Grohe Ag Jet former, in particular for a sanitary shower head, comprising a rotor blade that is configured and designed to divide a flow of water into parts and partial flows

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