US2381187A - Fluid coupling - Google Patents

Fluid coupling Download PDF

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Publication number
US2381187A
US2381187A US402373A US40237341A US2381187A US 2381187 A US2381187 A US 2381187A US 402373 A US402373 A US 402373A US 40237341 A US40237341 A US 40237341A US 2381187 A US2381187 A US 2381187A
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Prior art keywords
impeller
turbine
blades
fluid
vanes
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Expired - Lifetime
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US402373A
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Swift John Frederick
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Hydraulic Brake Co
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Hydraulic Brake Co
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Priority to US402373A priority Critical patent/US2381187A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D33/00Rotary fluid couplings or clutches of the hydrokinetic type
    • F16D33/18Details
    • F16D33/20Shape of wheels, blades, or channels with respect to function

Definitions

  • This invention relates to fluid couplings, and more particularly to an impeller and a turbine, and the relationship of one tothe other.
  • the absolute path of fluid flow in the circuit of the coupling providcd by the impeller and associated turbine is the resultant of the rotary motion of the impeller and the turbine and the relative motion vided by the blades of the impeller itself and the.
  • vanes of the turbine itself is usually smooth and continuous. However, there is an abrupt discontinuity at the clearances between the impeller and the turbine, introducing serious objections in the way of velocity changes, vibrations, and
  • An object of the invention is to provide a fluid coupling including an impeller and a turbine providing in conJunction with one another a fluid circuit, and blades on the impeller and vanes on the turbine of such contour and relationship as to insure continuous flow of the fluid through the circuit.
  • Another object of the invention is to provide blades for the impeller and vanes for the turbine of such contour and relation to one another that fluid channels provided by the vanes on the turbine, when the coupling is running at normal speeds and loads, conform to the theoretical flow of the fluid through the fluid circuit.
  • Another object of the invention is to provide a fluid coupling including an impeller and a turbine having blades and vanes, respectively, of substantially the same contour but arranged in oppositely disposed relation so that the adjacent blades of the impeller and the vanes 01' the turbine are tipped 'off radially in opposite senses in order that the passages of the impeller and the turbine completely overlap.
  • FIG. 1 is a vertical sectional view of a fluid coupling embodying the invention
  • Fig. 2 is a fragmentary view of the impeller
  • Fig. 3 is a fragmentary view of the turbine.
  • Fig. 4 is an enlarged view of a blade corresponding to the blades and vanes incorporated in the impeller and turbine, respectively.
  • a driving shaft having a flange l2 provided with a concentrically disposed recess ll.
  • a housing l8 preferably fabricated in two parts 18 and 2! suitably joined together has concentrically disposed hubs 22 and 2
  • the hub 22 is bolted or otherwise secured to the flange l2, and the hub 2
  • a driven shaft 28 is supported for rotation coaxially with relation to the driving shaft. As shown, the driven shaft extends through the ring 26 and housing [6 into the recess H in the driving shaft, and is journaled on a bearing III fitted in the hub 22. A fluid seal 32 also fitted in the hub 22 embraces the driven shaft to inhibit seepage of fluid from the housing to the bearing.
  • the part l8 of the housing I6 constitutes the outer shroud of an impeller indicated generally at '34, and arranged on the inner wall 'of the part l8 are blades 36 supporting an inner shroud ll.
  • a turbine indicated generally at 40 is mounted on the driven shaft 28 'within the housing in oppositely disposed relation to the impeller 24.
  • ] includes a hub 42 keyed or otherof the turbine are substantially alike, but are arranged in oppositely disposed relation.
  • This arrangement of the blades on the impeller and turbine is of paramount importance, particularly the relationship of the blades on the impeller to the vanes of the turbine, because it is due to such arrangement that the fluid in the circuit flowsacross the clearances between'the impeller and turbine without velocity changes introducing ob jectional vibrations and eddy currents;
  • the ad- .lacent blades of .the impeller and vanes of the turbine are tipped ofl radially in the opposite senses so that the passages through the impeller and turbine completely overlap, and this overlapping of the passages promotes continuous flow oi the fluid across the clearances between the impcller and the turbine, thus minimizing the setting up of velocity changes, eddy currents, vibration impulses, and obiectional noises.
  • the fluid flow follows the optimum path for smoothness in operation of the coupling.
  • a fluid coupling comprising an impeller having blades twisted throughout their lengths with their inlet and Outlet edges tipped in Opposite directions, and a turbine associated with the impeller having vanes twisted throughout their lengths with their inlet and outlet edges tipped in opposite directions and being in oppositely disposed relation to the impeller blades.
  • a fluid coupling comprising an impeller hav ing blades twisted throughout their lengths with their inlet and outlet edges inclined in opposite directions, and a turbine opposed to the impeller having blades twisted throughout their lengths with their inlet and outlet edges inclined in 0D- posite directions. the edges of the impeller blades and turbine vanes crossing one another.
  • a fluid coupling comprising an impeller, a turbine opposed to the impeller in spaced relation providing small clearance, blades on the impeller curved and twisted throughout their lengths with their inlet and outlet edges inclined in opposite directions, and vanes on the turbine curved and twisted throughout their lengths with their inlet and outlet edges inclined in opposite directions, the edges of the vanes crossing the adiacent edges of the blades.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Turbines (AREA)

Description

g- 7, 1 J. F. SWIFT 2,381,187
FLUID COUPLING Filed July 14, 1941 INVENTOR.
d/PEDEF/CA Ju /Fr ATTORNEY Patented Aug.
UNITED STATES PATENT OFFICE Hydraulic Brake Company, Detroit, corporation of California Mich, 2.
Application July 14, 1941, Serial No. 402,373
3 Claims. (.01. Bil-54) This invention relates to fluid couplings, and more particularly to an impeller and a turbine, and the relationship of one tothe other.
Generally in fluid couplings, the absolute path of fluid flow in the circuit of the coupling providcd by the impeller and associated turbine is the resultant of the rotary motion of the impeller and the turbine and the relative motion vided by the blades of the impeller itself and the.
vanes of the turbine itself is usually smooth and continuous. However, there is an abrupt discontinuity at the clearances between the impeller and the turbine, introducing serious objections in the way of velocity changes, vibrations, and
eddy currents as the blades of the impeller pass the vanes of the turbine, and the instant invention aims to overcome these objections.
An object of the invention is to provide a fluid coupling including an impeller and a turbine providing in conJunction with one another a fluid circuit, and blades on the impeller and vanes on the turbine of such contour and relationship as to insure continuous flow of the fluid through the circuit.
Another object of the invention is to provide blades for the impeller and vanes for the turbine of such contour and relation to one another that fluid channels provided by the vanes on the turbine, when the coupling is running at normal speeds and loads, conform to the theoretical flow of the fluid through the fluid circuit.
Another object of the invention is to provide a fluid coupling including an impeller and a turbine having blades and vanes, respectively, of substantially the same contour but arranged in oppositely disposed relation so that the adjacent blades of the impeller and the vanes 01' the turbine are tipped 'off radially in opposite senses in order that the passages of the impeller and the turbine completely overlap.
Other objects and advantages of the invention will appear from the following description taken in connection with the drawing forming a part of this specification, and in which- Fig. 1 is a vertical sectional view of a fluid coupling embodying the invention;
Fig. 2 is a fragmentary view of the impeller;
Fig. 3 is a fragmentary view of the turbine; and
Fig. 4 is an enlarged view of a blade corresponding to the blades and vanes incorporated in the impeller and turbine, respectively.
Referring to the drawing for more specific details of the invention, In represents a driving shaft having a flange l2 provided with a concentrically disposed recess ll. A housing l8 preferably fabricated in two parts 18 and 2! suitably joined together has concentrically disposed hubs 22 and 2|. The hub 22 is bolted or otherwise secured to the flange l2, and the hub 2|, has suitably secured therein a ring 26.
A driven shaft 28 is supported for rotation coaxially with relation to the driving shaft. As shown, the driven shaft extends through the ring 26 and housing [6 into the recess H in the driving shaft, and is journaled on a bearing III fitted in the hub 22. A fluid seal 32 also fitted in the hub 22 embraces the driven shaft to inhibit seepage of fluid from the housing to the bearing.
The part l8 of the housing I6 constitutes the outer shroud of an impeller indicated generally at '34, and arranged on the inner wall 'of the part l8 are blades 36 supporting an inner shroud ll.
A turbine indicated generally at 40 is mounted on the driven shaft 28 'within the housing in oppositely disposed relation to the impeller 24.
The turbine 4|] includes a hub 42 keyed or otherof the turbine are substantially alike, but are arranged in oppositely disposed relation. This arrangement of the blades on the impeller and turbine is of paramount importance, particularly the relationship of the blades on the impeller to the vanes of the turbine, because it is due to such arrangement that the fluid in the circuit flowsacross the clearances between'the impeller and turbine without velocity changes introducing ob jectional vibrations and eddy currents;
It is to be observed that the blades of the impeller and the vanes of the turbine are twisted throughout their lengths, as most clearly shown,
so as to conform to the theoretical flow of the fluid through the circuit. Then, too, the ad- .lacent blades of .the impeller and vanes of the turbine are tipped ofl radially in the opposite senses so that the passages through the impeller and turbine completely overlap, and this overlapping of the passages promotes continuous flow oi the fluid across the clearances between the impcller and the turbine, thus minimizing the setting up of velocity changes, eddy currents, vibration impulses, and obiectional noises.
In a normal operation, actuation of the impeller 34 results in energization of the fluid in the housing is, and the energy 0! the fluid is absorbed by the turbine Iii, resulting in rotation thereof.
When the fluid is energized by the impeller, it passes through the channels provided by the blades of the impeller and the vanes of the turbine across the clearances between the blades of the impeller and the vanes oi the turbine. and,
due to the particular conformation of the blades of the impeller and the vanes of the turbine and of the relationship of the blades to the vanes, the fluid flow follows the optimum path for smoothness in operation of the coupling.
While this invention has been described in connection with certain specific embodiments, the principle involved is susceptible oi. numerous other applications that will readily occur to persons skilled in the art. The invention is, therefore, to be limited only as indicated by the scope oi the appended claim Having thus described the various features or the invention. what I claim as new and desire to secure by Letters Patent is:
l. A fluid coupling comprising an impeller having blades twisted throughout their lengths with their inlet and Outlet edges tipped in Opposite directions, and a turbine associated with the impeller having vanes twisted throughout their lengths with their inlet and outlet edges tipped in opposite directions and being in oppositely disposed relation to the impeller blades.
2. A fluid coupling comprising an impeller hav ing blades twisted throughout their lengths with their inlet and outlet edges inclined in opposite directions, and a turbine opposed to the impeller having blades twisted throughout their lengths with their inlet and outlet edges inclined in 0D- posite directions. the edges of the impeller blades and turbine vanes crossing one another.
3. A fluid coupling comprising an impeller, a turbine opposed to the impeller in spaced relation providing small clearance, blades on the impeller curved and twisted throughout their lengths with their inlet and outlet edges inclined in opposite directions, and vanes on the turbine curved and twisted throughout their lengths with their inlet and outlet edges inclined in opposite directions, the edges of the vanes crossing the adiacent edges of the blades.
JOHN FREDERICK SWIF'I'.
US402373A 1941-07-14 1941-07-14 Fluid coupling Expired - Lifetime US2381187A (en)

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2460587A (en) * 1942-11-09 1949-02-01 Gustav Hanke Airplane drive
US2589863A (en) * 1946-12-06 1952-03-18 Orpheus F Quartullo Gasoline-electric drive for vehicles
US2663148A (en) * 1953-12-22 Blading for hydraulic torque
US2663149A (en) * 1950-12-30 1953-12-22 Borg Warner Rotary turbine-type hydraulic torque converter
US2768711A (en) * 1951-10-12 1956-10-30 Clayton Manufacturing Co Hydro-kinetic apparatus
US2772538A (en) * 1952-07-12 1956-12-04 Fred E Ullery Blade formations for turbo-machines
US2785636A (en) * 1953-12-28 1957-03-19 Gen Motors Corp Fluid coupling
US2870875A (en) * 1951-10-12 1959-01-27 Clayton Manufacturing Co Hydro-kinetic brake device
US3002356A (en) * 1956-05-02 1961-10-03 Twin Disc Clutch Co Power transmission
US3016709A (en) * 1953-01-21 1962-01-16 Lysholm Alf Single stage turbine hydraulic torque converter
US3167917A (en) * 1960-09-07 1965-02-02 Alexander M Alexandrescu Hydraulic coupling
US20170108101A1 (en) * 2015-10-19 2017-04-20 Aisin Seiki Kabushiki Kaisha Torque converter and manufacturing method thereof
CN108223612A (en) * 2016-12-14 2018-06-29 福伊特专利有限公司 Fluid coupling
WO2021048644A1 (en) * 2019-09-10 2021-03-18 Suprichakorn Staporn Fluid coupling for a continuous variable transmission
US11085497B1 (en) * 2020-10-09 2021-08-10 David Johnson Fluid coupling with partially curved impeller vanes

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663148A (en) * 1953-12-22 Blading for hydraulic torque
US2460587A (en) * 1942-11-09 1949-02-01 Gustav Hanke Airplane drive
US2589863A (en) * 1946-12-06 1952-03-18 Orpheus F Quartullo Gasoline-electric drive for vehicles
US2663149A (en) * 1950-12-30 1953-12-22 Borg Warner Rotary turbine-type hydraulic torque converter
US2768711A (en) * 1951-10-12 1956-10-30 Clayton Manufacturing Co Hydro-kinetic apparatus
US2870875A (en) * 1951-10-12 1959-01-27 Clayton Manufacturing Co Hydro-kinetic brake device
US2772538A (en) * 1952-07-12 1956-12-04 Fred E Ullery Blade formations for turbo-machines
US3016709A (en) * 1953-01-21 1962-01-16 Lysholm Alf Single stage turbine hydraulic torque converter
US2785636A (en) * 1953-12-28 1957-03-19 Gen Motors Corp Fluid coupling
US3002356A (en) * 1956-05-02 1961-10-03 Twin Disc Clutch Co Power transmission
US3167917A (en) * 1960-09-07 1965-02-02 Alexander M Alexandrescu Hydraulic coupling
US20170108101A1 (en) * 2015-10-19 2017-04-20 Aisin Seiki Kabushiki Kaisha Torque converter and manufacturing method thereof
US10495203B2 (en) * 2015-10-19 2019-12-03 Aisin Seiki Kabushiki Kaisha Torque converter and manufacturing method thereof
CN108223612A (en) * 2016-12-14 2018-06-29 福伊特专利有限公司 Fluid coupling
WO2021048644A1 (en) * 2019-09-10 2021-03-18 Suprichakorn Staporn Fluid coupling for a continuous variable transmission
US11085497B1 (en) * 2020-10-09 2021-08-10 David Johnson Fluid coupling with partially curved impeller vanes

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