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US1510086A - Arrangement at hubs for turbine, pump, or propeller wheels with turnable vanes - Google Patents

Arrangement at hubs for turbine, pump, or propeller wheels with turnable vanes Download PDF

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Publication number
US1510086A
US1510086A US624937A US62493723A US1510086A US 1510086 A US1510086 A US 1510086A US 624937 A US624937 A US 624937A US 62493723 A US62493723 A US 62493723A US 1510086 A US1510086 A US 1510086A
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United States
Prior art keywords
vane
pivot
vanes
hub
bearing
Prior art date
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Expired - Lifetime
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US624937A
Inventor
Englesson John Elov
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Individual
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Filing date
Publication date
Priority to DEE28602D priority Critical patent/DE394525C/en
Priority to GB4476/23A priority patent/GB208434A/en
Priority to FR562287D priority patent/FR562287A/en
Application filed by Individual filed Critical Individual
Priority to US624937A priority patent/US1510086A/en
Application granted granted Critical
Publication of US1510086A publication Critical patent/US1510086A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H3/00Propeller-blade pitch changing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H3/00Propeller-blade pitch changing
    • B63H3/02Propeller-blade pitch changing actuated by control element coaxial with propeller shaft, e.g. the control element being rotary
    • B63H3/04Propeller-blade pitch changing actuated by control element coaxial with propeller shaft, e.g. the control element being rotary the control element being reciprocatable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H3/00Propeller-blade pitch changing
    • B63H3/06Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical
    • B63H3/08Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid
    • B63H3/081Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid actuated by control element coaxial with the propeller shaft
    • B63H3/082Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid actuated by control element coaxial with the propeller shaft the control element being axially reciprocatable
    • 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
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12Blades; Blade-carrying rotors
    • F03B3/14Rotors having adjustable blades
    • F03B3/145Mechanisms for adjusting the blades
    • 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
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/76Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
    • 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

  • the vane is pivoted upon a journal or pivot of relatively small diameter and is t-urnable about the axis of this pivot.
  • the outer extremities of the vane base are supported upon an annular ring bearing.
  • this pivot may be made of very small diameter and because of this the friction is reduced greatly and the work required to turn the vane about the pivot axis is very small.
  • the base of the vane is made relatively very broad and its extremities are sup ported upon the separate ring bearing atxa relatively large distance from the axis of rotation, i.
  • Fig. 1 is a longitudinal sectional view
  • Fig. 2 is a cross sectional view through the middle'of the hub of Fig. 1.
  • Fig. 3 is a longitudinal sectional view of another form of my invention.
  • a hollow hub body 1 is supported on a hollow main shaft 1 in which there is a connecting rod 3.
  • This rod is movable longitudinally in bearings 4 and 5 formed by the body 1, and such longitudinal movement imparts the turning'motion to the vanes as will be described hereinafter.
  • Each ofvanes 7 is supported by two bearpivot alone.
  • journal or pivot 9 which is integral with the hub body and about whose axis the vane is turnable.
  • the other is a ring bearing 10, separate and distinct from pivot 9.
  • This ring may be fastened either to the hub as shown at 12 and be movable in a groove 2 in the vane base, or it may be fastened to the latter and move in a corresponding channel in the hub body.
  • suitable packing ring 13 is fitted around the vane base.
  • a flange 6 on the connecting rod 3 engages a spider 8 so that movement up and down of rod 3 imparts a similar motion to the spider 8.
  • agroove 15 which engages a small journal 17 on the vane base through a loose sleeve 16 fitted around journal 17".
  • the spider 8 is moved For each vane, the spider carup or down by means of rod. 3 and carries with it the journals 17', Pivots 9 being fixed, the vanes will turn around the axes of these pivots.
  • a special feature of my design are" clearance spaces 11 (between the inside surfaces of rings 10 andthe bases of the corresponding grooves 2), and 11 (between the butt ends of pivots 9 and thebases of their bearings in the vanes).
  • the space at 11 insures the taking up of all forces in a direction perpendicular to the axis of pivot 9 by the The space at the end of the latter allows all forces parallel to the axis of. pivot 9 to be taken up by the bearing surface of ring 10. These latter forces are due to be taken care of by the ordinary running fit of the vane on this pivot, and by placing the bearing 10 at a relatively very large distance from the center of the pivot, substantially all forces parallel to the axis of pivot 9 will be borne by this hearing 10.
  • the smallness of ivot 9 reduces the work required to turn t e vanes; the breadth of the vane base and its support at its extremities by ring bearing 10 assures a firm and staunch anchorage of the vane.
  • the lubrication of the vane bearings is accomplished by forcing oil undebropressure through channels 14 in the hub' y 1.
  • the pivot 9 is made spherical in shape.
  • center of the sphere must of course lie in the lane of the ring bearing 10.
  • a rotary Vane having-its bearing in the periphery, and means coaxially disposed with respect to the vane to only prevent transverse play thereof, whereby all forces directed against the vanes other than those being in a transverse direction with respect to the turning axis ,of the vanes are resisted by the peripheral bearing.
  • a propeller In a propeller, the combination of a hub, vanes rotatably mounted therein, and bearing means for the vanes comprising laterally grooved flanges, an annular bearing ring for said grooveand capable of permit ting transversely directed play in said vane, a centrally disposed pivot, and a bearing sleeve adapted to bear about the pivot and to have play in an axial direction with respect to the axis of the vane.
  • a propeller vane having a central pivot, and a peripheral bearing means comprising an annular member adapted to resist axial displacement of the vane, said resistance be ing brought about by the surface of the annular member being a greater distance from the center of rotation of the vane than the bearing surface of the pivot.
  • a propeller vane having a central pivot, and a peripheral bearing means comprising an annular member adapted to resist axial displacement of the vane, said resistance being transmitted directly to the vane without affecting the pivot, the said resistance, being brought about by the bearing surface of the annular member being a greater distance from the center of rotation of the vane than the bearing surface of the pivot.
  • a hearing for rotatably mounted ropeller vanes comprising a ring embrac by the hub of the vane at its periphery, the inner diameter of the ring being greater than the diameter of the adjacent wall of the vane, and a pivot pin disposed centrally of the vane and adapted to extend to a point short of the end of the opening in which it is mounted.
  • a hub the combination of a hub, blades rotatably mounted therein, and bearing means for the blades, comprising a central member and a peripheral member, each member having its bearings arranged in the body of the hub itself and being adapted to permit play of the blade should the other member be absent.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Actuator (AREA)
  • Hydraulic Turbines (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Mounting Of Bearings Or Others (AREA)

Description

Sept. 30 192 4.
J. E. ENGLESSON ARRANGEMENT AT HUBS FOR TURBI PUM OR PROPELLER WHEELS WITH NA VA Filed Mar 14. 1923 3 Sheets-Sheet 1 {IEHN ELOv Encmesso INVENTOR;
. Attorney.
Sept. 30 1924. 1,510,086
J. E. ENGLESSON ARRANGEMENT AT HUBS FOR TURBINE, PUMP, OR PROPELLER WHEELS WITH TURNABLE VANES Filed March 14, 1923 3 Sheets-Sheet 2 Jorm ELOV ENeLEssoN 1N ENTQ L Attorney,
Sept. 30 1924.
J. E. ENGLESSON ARRANGEMENT AT HUBS FOR TURBINE, PUMP, OR PR OPELLER WHEELS WITH TURNABLE VANES Filed March 14, 1923 a Sheet$-$heet 5 JAN? ELOV ENGLESSON INVENTOR;
' Attorney.
Patented Sept. 30, 1924.
UNITED STATES PATENT OFFICE.
JOHN ELOV ENGLESSON, F KEISTINEHA 'MTI, SWEDEN.
ARRANGEMENT AT HUBS FOR TURBINE, JPUMP, OR PROPELLER WHEELS WITH TURNAIBLE YANES.
Application filed March 14, 1923.
To all whom it may concern:
Be it known that 1, JOHN ELov ENGLES- soN, engineer, residing at Kristinehamn,
' the same time the work required to turn the vanes about their bearings should be reduced toa minimum, and also for the sake of mechanical efliciency the bearings should not be of excessively heavy design.
My design has these desirable characteristics. The vane is pivoted upon a journal or pivot of relatively small diameter and is t-urnable about the axis of this pivot. At the same time the outer extremities of the vane base are supported upon an annular ring bearing. Inasmuch as the bearing is so designed that the pivot takes up only stresses at right angles to its axis, this pivot may be made of very small diameter and because of this the friction is reduced greatly and the work required to turn the vane about the pivot axis is very small. time the base of the vane is made relatively very broad and its extremities are sup ported upon the separate ring bearing atxa relatively large distance from the axis of rotation, i. e., the center of the pivot One embodiment of my invention is shown in the accompanying drawings inwhich Fig. 1 is a longitudinal sectional view and Fig. 2 is a cross sectional view through the middle'of the hub of Fig. 1. Fig. 3 is a longitudinal sectional view of another form of my invention.
Referring to Figs. 1 and 2, a hollow hub body 1 is supported on a hollow main shaft 1 in which there is a connecting rod 3. This rod is movable longitudinally in bearings 4 and 5 formed by the body 1, and such longitudinal movement imparts the turning'motion to the vanes as will be described hereinafter.
Each ofvanes 7 is supported by two bearpivot alone.
At the same Serial No. 624,937.
ings. One is a journal or pivot 9 which is integral with the hub body and about whose axis the vane is turnable. The other is a ring bearing 10, separate and distinct from pivot 9. This ring may be fastened either to the hub as shown at 12 and be movable in a groove 2 in the vane base, or it may be fastened to the latter and move in a corresponding channel in the hub body. A
suitable packing ring 13 is fitted around the vane base.
A flange 6 on the connecting rod 3 engages a spider 8 so that movement up and down of rod 3 imparts a similar motion to the spider 8. ries agroove 15 which engages a small journal 17 on the vane base through a loose sleeve 16 fitted around journal 17".
To turn the vanes, the spider 8 is moved For each vane, the spider carup or down by means of rod. 3 and carries with it the journals 17', Pivots 9 being fixed, the vanes will turn around the axes of these pivots.
A special feature of my design are" clearance spaces 11 (between the inside surfaces of rings 10 andthe bases of the corresponding grooves 2), and 11 (between the butt ends of pivots 9 and thebases of their bearings in the vanes). The space at 11 insures the taking up of all forces in a direction perpendicular to the axis of pivot 9 by the The space at the end of the latter allows all forces parallel to the axis of. pivot 9 to be taken up by the bearing surface of ring 10. These latter forces are due to be taken care of by the ordinary running fit of the vane on this pivot, and by placing the bearing 10 at a relatively very large distance from the center of the pivot, substantially all forces parallel to the axis of pivot 9 will be borne by this hearing 10. The smallness of ivot 9 reduces the work required to turn t e vanes; the breadth of the vane base and its support at its extremities by ring bearing 10 assures a firm and staunch anchorage of the vane.
The lubrication of the vane bearings is accomplished by forcing oil undebropressure through channels 14 in the hub' y 1.
In the embodiment illustrated in Fig. 3 the pivot 9 is made spherical in shape. The
center of the sphere must of course lie in the lane of the ring bearing 10.
at I claim is: p
l. in a propeller, the combination with a hub and vanes rotatably mounted therein, of a central pivot for each vane and an annular bearing member engaged by the vane, said bearing member being adapted to resist only forces parallel to the axis of said pivot.
2. In a propeller, the combination with a hub and vane rotatably mounted therein, of an annular bearing member for each vane and a central. pivot designed as an axis for the turning of said vanes and adapted to re sist only forces perpendicular to the axis of said pivot.
' 3. In a propeller, the combination of a hub, vanes rotatably mounted therein, a central pivot for each vane, and an annular bearing member engaged by the vane to per- ;mit only transverse play of the latter with respectto the pivot.
- 4. In a propeller, the combination of a hub, vanes notatably mounted therein, an annular bearing member for each vane, and a pivot disposed axially of the vane to permit only axial play of the latter with respect to the bearing member.
5. A rotary Vane having-its bearing in the periphery, and means coaxially disposed with respect to the vane to only prevent transverse play thereof, whereby all forces directed against the vanes other than those being in a transverse direction with respect to the turning axis ,of the vanes are resisted by the peripheral bearing.
6.' In a propeller, the combination of a hub, vanes rotatably mounted therein, and bearing means for the vanes comprising laterally grooved flanges, an annular bearing ring for said grooveand capable of permit ting transversely directed play in said vane, a centrally disposed pivot, and a bearing sleeve adapted to bear about the pivot and to have play in an axial direction with respect to the axis of the vane.
7. A propeller vane having a central pivot, and a peripheral bearing means comprising an annular member adapted to resist axial displacement of the vane, said resistance be ing brought about by the surface of the annular member being a greater distance from the center of rotation of the vane than the bearing surface of the pivot. I
8. A propeller vane having a central pivot, and a peripheral bearing means comprising an annular member adapted to resist axial displacement of the vane, said resistance being transmitted directly to the vane without affecting the pivot, the said resistance, being brought about by the bearing surface of the annular member being a greater distance from the center of rotation of the vane than the bearing surface of the pivot.
9. A hearing for rotatably mounted ropeller vanes, comprising a ring embrac by the hub of the vane at its periphery, the inner diameter of the ring being greater than the diameter of the adjacent wall of the vane, and a pivot pin disposed centrally of the vane and adapted to extend to a point short of the end of the opening in which it is mounted. e
10. In a propeller, the combination of a hub, blades rotatably mounted therein, and bearing means for the blades, comprising a central member and a peripheral member, each member having its bearings arranged in the body of the hub itself and being adapted to permit play of the blade should the other member be absent. 1
11. In impellers for water turbines the combination with a hub and vanes rotatably mounted therein ofa central pivot for each vane and an annulafbearing member engaged by the vane both bearings being arranged in the body of the hub itself annular bearing member being adapted to resist only forces parallel to the axis of said pivot.
12. In impellers for water turbines the combination with a hub and vanes rotatably mounted therein, of an annular bearing member for each vane and a central pivot designed as an axis for the turning of said vanes both bearings being arranged in the body of the hub itself and said pivot being adapted to iesist only forces perpendicular to the axis of the same.
13. In impellers for water turbines the combination with a hub and vanes rotatably mounted therein, of a central pivot for each vane and an annular bearing member engaged by the vane said annular bearing memher being adapted to resist only forces parallel to the axis of said pivot.
In testimony whereof, I have signed my name to this specification in the presence of two subscribing witnesses.
JOHN ELOV ENGLESSON.
Witnesses ERNST NORDLINDH, HA NS PETTERSSON.
US624937A 1922-02-18 1923-03-14 Arrangement at hubs for turbine, pump, or propeller wheels with turnable vanes Expired - Lifetime US1510086A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DEE28602D DE394525C (en) 1922-02-18 1922-10-19 Signal box for rotatable impeller blades with a hydraulic cylinder (servo motor) firmly connected to the turbine axis and rotating with it
GB4476/23A GB208434A (en) 1922-02-18 1923-02-15 Improvements in or relating to hubs for turbine, pump or propeller wheels with turnable vanes
FR562287D FR562287A (en) 1922-02-18 1923-02-16 Hubs for turbine, pumps or propellers, with variable-angle vanes or blades
US624937A US1510086A (en) 1922-02-18 1923-03-14 Arrangement at hubs for turbine, pump, or propeller wheels with turnable vanes

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE562287X 1922-02-18
GB4476/23A GB208434A (en) 1922-02-18 1923-02-15 Improvements in or relating to hubs for turbine, pump or propeller wheels with turnable vanes
US624937A US1510086A (en) 1922-02-18 1923-03-14 Arrangement at hubs for turbine, pump, or propeller wheels with turnable vanes

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US1510086A true US1510086A (en) 1924-09-30

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US624937A Expired - Lifetime US1510086A (en) 1922-02-18 1923-03-14 Arrangement at hubs for turbine, pump, or propeller wheels with turnable vanes

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DE (1) DE394525C (en)
FR (1) FR562287A (en)
GB (1) GB208434A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474635A (en) * 1943-08-18 1949-06-28 Harry J Nichols Variable pitch propeller
US2514097A (en) * 1947-01-14 1950-07-04 Morgan Smith S Co Hub construction for variable pitch propellers or the like
US2612229A (en) * 1945-03-06 1952-09-30 Tornes Ferdinand Variable pitch propeller blade root construction
US2612961A (en) * 1943-03-09 1952-10-07 Konink Mij De Schelde Nv Propeller having adjustable blades
US2620887A (en) * 1947-09-30 1952-12-09 Curtiss Wright Corp Electrically operated propeller pitch change mechanism
US3247908A (en) * 1962-08-27 1966-04-26 Robook Nicolay Nikolaevich Adjustable blades hydraulic turbine runner

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB777908A (en) * 1954-11-13
DE1264284B (en) * 1966-07-25 1968-03-21 Eisenwerke Reintjes G M B H Ship propeller with adjustable blades
EP0548817A3 (en) * 1991-12-20 1993-11-24 Siemens Ag Process and apparatus for insulation testing of insulated electrical conductors, and for measurements of the length of insulation faults

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2612961A (en) * 1943-03-09 1952-10-07 Konink Mij De Schelde Nv Propeller having adjustable blades
US2474635A (en) * 1943-08-18 1949-06-28 Harry J Nichols Variable pitch propeller
US2612229A (en) * 1945-03-06 1952-09-30 Tornes Ferdinand Variable pitch propeller blade root construction
US2514097A (en) * 1947-01-14 1950-07-04 Morgan Smith S Co Hub construction for variable pitch propellers or the like
US2620887A (en) * 1947-09-30 1952-12-09 Curtiss Wright Corp Electrically operated propeller pitch change mechanism
US3247908A (en) * 1962-08-27 1966-04-26 Robook Nicolay Nikolaevich Adjustable blades hydraulic turbine runner

Also Published As

Publication number Publication date
FR562287A (en) 1923-11-08
GB208434A (en) 1923-12-20
DE394525C (en) 1924-04-19

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