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US3257825A - Flexible couplings - Google Patents

Flexible couplings Download PDF

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Publication number
US3257825A
US3257825A US349824A US34982464A US3257825A US 3257825 A US3257825 A US 3257825A US 349824 A US349824 A US 349824A US 34982464 A US34982464 A US 34982464A US 3257825 A US3257825 A US 3257825A
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blocks
blades
width
diameter
peripheral surface
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US349824A
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Croset Louis Paul
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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G5/00Component parts or accessories for scaffolds
    • E04G5/02Scaffold feet, e.g. with arrangements for adjustment
    • 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
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/64Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members comprising elastic elements arranged between substantially-radial walls of both coupling parts
    • F16D3/68Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members comprising elastic elements arranged between substantially-radial walls of both coupling parts the elements being made of rubber or similar material
    • 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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/121Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon using springs as elastic members, e.g. metallic springs
    • F16F15/124Elastomeric springs

Definitions

  • This invention relates to flexible vibration damping spondingly lower coupling stiflness.
  • the blocks operate in pairs, one driving, one trailing, for
  • any direction of rotation is to base the coupling characteristics, namely stiffness and torsional deflection, not by a haphazard choice of the number of cells, but by the calculation of the desired number of cells which determines the angle of torsional deflection as a function of the cell angle for any specific mass-elastic system, the size or diameter of the blocks and the number of blocks per cell being determined by the desired coupling capacity.
  • a flexible vibration damping apparatus comprises two coaxial members, two sets of blades which extend radially and axially of the apparatus and which blades are connected alternately to said coaxial members so as to form cells, a plurality of solid circular blocks of elastic material in each cell, the blocks having circular flat end surfaces parallel to each other of smaller diameter than that of the blocks, an outer circular peripheral surface of smaller width than that of the blocks,
  • solid is intended to mean that the blocks are free from any major holes or cavities, e.g. no bolts,
  • pins or the like pass through the 'blocks and in fact the blocks should even be as free as possible from smaller cavities although in practice it may be impossible to avoid occasional minor cavities altogether.
  • the width may be 0.45 to 0.55' D, and the blocks may have an end surface diameter of 0.5 to 0.6 D (preferably 0.45 to 0.55) and a width of peripheral surface 0.2 to 0.3 D.
  • the size of blocks is preferably such as to fit the cells Without pre-compression or such as to require up to 3.0 percent (preferably not more than 1.5 percent) pre-compression in both diameter and width.
  • Each'cell may contain 2 to 6 blocks.
  • the roots of the blades may have a radius equal to half the radial height of the cells and the remainder of the blades may have their sides parallel to each other.
  • FIGURE 1 is a half sectional view on a radial plane I-I of a coupling made in accordance with the invention.
  • FIGURE 2 is a half end view thereof with the end' plate removed.
  • the two coaxial members consist of an inner member 10 carrying blades 11 surrounded by an outer member 12 carrying blades 13.
  • the outermember 12 is bolted by bolts 14 to a driving flange 16 on a driving sleeve 17.
  • Each blade on one member is located normally midway between two blades on the other member to form cells.
  • A shows'the cell angle and B, shows the centre of blade angle, both angles being identical.
  • Each cell contains three solid rubber blocks and the cells and closed by an end plate 18 bolted by bolts 19 to the member 12.
  • Each block has an outer peripheral surface 22 two circular end surfaces 23, 24 and two frustoconical surfaces 26, 27 connecting the surface 22 to the end surfaces 23, 24.
  • the width W of the block is 0.5 D
  • the end surfaces contact each other and/or the flange 16 or plate 18.
  • the roots of the blades are curved to a radius equal to half the radial height of the cells.
  • the number of cells may vary for example between 6 and 16 and it will be realised that in a coupling having 6 cavities only the cavity angle will be 60 and in a coupling with 16 cavities 22.5 so that for a given maximum compressive strain of say 25% the appropriate torsional deflection angles obtained would be 15 and 5.6, respectively.
  • the preferred number of blocks in each cell is 2, 3, or 5 but it is also possible to make a coupling with only 1 block or if desired 6 blocks per cavity.
  • the blocks whether driving or trailing at all times make contact with the parts 16, 18 with a pre-compression of the order of 1 to 1.5% to ensure that the blocks are maintained in their true plane of rotation at all times and cannot possibly twist in the cavities.
  • only the block end-faces contact the cell end walls, both under no-load and under full-load conditions, in order to reduce the friction between the driving blocks and the cavity walls.
  • the driving block end-faces become slightly elliptical, the conical flanks 26, 27 remain out of contact with the cavity walls at all times and an increase in the block deformation of the order of is thereby obtained compared with the cylindrical blocks.
  • the blades may if desired by slightly tapered.
  • the use of tapered instead of parallel blades makes the cell volume a little larger, obtaining thereby an increased torsional flexibility of the coupling and incidentally effecting a reduction in weight.
  • the increase in torsional flexibility is of the order of 5%.
  • a flexible vibration damping apparatus comprising two coaxial members, two sets of'blades which extend radially and axially of the apparatus and-which blades are connected alternately to said coaxial members so as to form cells, a plurality of solid circular blocks of of said blocks having a width 0.45 to 0.55 D, an end surface diameter 0.5 to 0.6 D and a width of peripheral surface 0.2 to 0.3 D.
  • a flexible vibration damping apparatus comprising two coaxial members, two sets of bladeswhich extend radially and axially of the apparatus and which blades are connected alternately to said coaxial members so as t to form 6 to 16 cells at least two and not more than six solid circular blocks of elastic material in each cell, the blocks having circular fiat end surfaces parallel to each other of smaller diameter than that of the blocks, an outer circular peripheral surface of smaller width than that of the blocks, and inclined outer annular surfaces from the end faces to the peripheral surface, said blocks having a diameter D, each of said blocks having a width of 0.45 to 0.55 D, an end surface diameter of 0.5 to 0.6 D, and a Width of peripheral surface 0.2 to 0.3 D.
  • the roots of the blades have a radius equal to half the radial height of the cells and the remainder of the blades have their sides parallel to each other.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Operated Clutches (AREA)
  • Vibration Prevention Devices (AREA)
  • Vibration Dampers (AREA)

Description

June 28, 1966 L. P. CROSET 3,257,825
FLEXIBLE COUPLINGS Filed March 6. 1964 100/; PM; Geasrr 3,257,825 Patented June 28, 1966 United States Patent Office 3,257,825 FLEXIBLE COUPLINGS Louis Paul Croset, Im Schleipfenacker 10, Forch, Zurich, Switzerland Filed Mar. 6, 1964, Ser. No. 349,824
Claims priority, application Great Britain, Mar. 14, 1963,
10,137 63 4 Claims. (Cl. 64-14) This invention relates to flexible vibration damping spondingly lower coupling stiflness.
the blocks operate in pairs, one driving, one trailing, for
any direction of rotation, is to base the coupling characteristics, namely stiffness and torsional deflection, not by a haphazard choice of the number of cells, but by the calculation of the desired number of cells which determines the angle of torsional deflection as a function of the cell angle for any specific mass-elastic system, the size or diameter of the blocks and the number of blocks per cell being determined by the desired coupling capacity.
According to the invention, a flexible vibration damping apparatus comprises two coaxial members, two sets of blades which extend radially and axially of the apparatus and which blades are connected alternately to said coaxial members so as to form cells, a plurality of solid circular blocks of elastic material in each cell, the blocks having circular flat end surfaces parallel to each other of smaller diameter than that of the blocks, an outer circular peripheral surface of smaller width than that of the blocks,
and inclined outer annular surfaces from the end faces of the peripheral surface.
The term solid is intended to mean that the blocks are free from any major holes or cavities, e.g. no bolts,
pins or the like pass through the 'blocks and in fact the blocks should even be as free as possible from smaller cavities although in practice it may be impossible to avoid occasional minor cavities altogether.
For blocks having a diameter D, the width may be 0.45 to 0.55' D, and the blocks may have an end surface diameter of 0.5 to 0.6 D (preferably 0.45 to 0.55) and a width of peripheral surface 0.2 to 0.3 D.
The size of blocks is preferably such as to fit the cells Without pre-compression or such as to require up to 3.0 percent (preferably not more than 1.5 percent) pre-compression in both diameter and width.
Each'cell may contain 2 to 6 blocks.
The roots of the blades may have a radius equal to half the radial height of the cells and the remainder of the blades may have their sides parallel to each other.
The cone-shape block ofiers the following advantages:
(a) Softer effect than cylindrical blocks;
(b) Area of contact with cell end-walls is less than 50% of that of cylindrical blocks used hitherto;
(c) Lesser volume of rubber and simple mould shape.
A constructional form of the invention is illustrated by Way of example in'the accompanying drawing.
FIGURE 1 is a half sectional view on a radial plane I-I of a coupling made in accordance with the invention; and
FIGURE 2 is a half end view thereof with the end' plate removed.
The two coaxial members consist of an inner member 10 carrying blades 11 surrounded by an outer member 12 carrying blades 13. The outermember 12 is bolted by bolts 14 to a driving flange 16 on a driving sleeve 17. Each blade on one member is located normally midway between two blades on the other member to form cells. A shows'the cell angle and B, shows the centre of blade angle, both angles being identical.
Each cell contains three solid rubber blocks and the cells and closed by an end plate 18 bolted by bolts 19 to the member 12. Each block has an outer peripheral surface 22 two circular end surfaces 23, 24 and two frustoconical surfaces 26, 27 connecting the surface 22 to the end surfaces 23, 24. For a block diameter D the width W of the block is 0.5 D, the diameter E of end face 0.55 D, and the width P of the peripheral surface 0.25 D. The end surfaces contact each other and/or the flange 16 or plate 18. The roots of the blades are curved to a radius equal to half the radial height of the cells.
The number of cells may vary for example between 6 and 16 and it will be realised that in a coupling having 6 cavities only the cavity angle will be 60 and in a coupling with 16 cavities 22.5 so that for a given maximum compressive strain of say 25% the appropriate torsional deflection angles obtained would be 15 and 5.6, respectively.
The preferred number of blocks in each cell is 2, 3, or 5 but it is also possible to make a coupling with only 1 block or if desired 6 blocks per cavity.
The blocks whether driving or trailing at all times make contact with the parts 16, 18 with a pre-compression of the order of 1 to 1.5% to ensure that the blocks are maintained in their true plane of rotation at all times and cannot possibly twist in the cavities. In other words, only the block end-faces contact the cell end walls, both under no-load and under full-load conditions, in order to reduce the friction between the driving blocks and the cavity walls. Whilst under maximum torque load the driving block end-faces become slightly elliptical, the conical flanks 26, 27 remain out of contact with the cavity walls at all times and an increase in the block deformation of the order of is thereby obtained compared with the cylindrical blocks.
The blades may if desired by slightly tapered.
The use of tapered instead of parallel blades makes the cell volume a little larger, obtaining thereby an increased torsional flexibility of the coupling and incidentally effecting a reduction in weight. The increase in torsional flexibility is of the order of 5%.
I claim:
1. A flexible vibration damping apparatus comprising two coaxial members, two sets of'blades which extend radially and axially of the apparatus and-which blades are connected alternately to said coaxial members so as to form cells, a plurality of solid circular blocks of of said blocks having a width 0.45 to 0.55 D, an end surface diameter 0.5 to 0.6 D and a width of peripheral surface 0.2 to 0.3 D.
2. A flexible vibration damping apparatus comprising two coaxial members, two sets of bladeswhich extend radially and axially of the apparatus and which blades are connected alternately to said coaxial members so as t to form 6 to 16 cells at least two and not more than six solid circular blocks of elastic material in each cell, the blocks having circular fiat end surfaces parallel to each other of smaller diameter than that of the blocks, an outer circular peripheral surface of smaller width than that of the blocks, and inclined outer annular surfaces from the end faces to the peripheral surface, said blocks having a diameter D, each of said blocks having a width of 0.45 to 0.55 D, an end surface diameter of 0.5 to 0.6 D, and a Width of peripheral surface 0.2 to 0.3 D.
3. A damping apparatus as claimed in claim 1 wherein the blocks fit in the cells without rare-compression or with a pre-compression not exceeding 3.0 percent in diameter and width.
the roots of the blades have a radius equal to half the radial height of the cells and the remainder of the blades have their sides parallel to each other.
References Cited by the Examiner UNITED STATES PATENTS BROUGHTON G. DURHAM, Primary Examiner.
4. A damping apparatus as claimedin claim 1 wherein H C (1015, A i t Examiner,

Claims (1)

1. A FLEXIBLE VIBRATION DAMPING APPARATUS COMPRISING TWO COAXIAL MEMBERS, TWO SETS OF BLADES WHICH EXTEND RADIALLY AND AXIALLY OF THE APPARATUS AND WHICH BLADES ARE CONNECTED ALTERNATELY TO SAID COAXIAL MEMBERS SO AS TO FORM CELLS, A PLURALITY OF SOLID CIRCULAR BLOCKS OF ELASTIC MATERIAL IN EACH CELL, THE BLOCKS HAVING CIRCULAR FLAT END SURFACES PARALLEL TO EACH OTHER OF SMALLER DIAMETER THAN THAT OF THE BLOCKS, AN OUTER CIRCULAR PERIPHERAL SURFACE OF SMALLER WIDTH THAN THAT OF THE BLOCKS, AND INCLINED OUTER ANNULAR SURFACES FROM THE END FACES TO THE PERIPHERAL SURFACE, SAID BLOCKS HAVING A DIAMETER D, EACH OF SAID BLOCKS HAVING A WIDTH 0.45 TO 0.55 D, AN END SURFACE DIAMETER 0.5 TO 0.6 D AND A WIDTH OF PERIPHERAL SURFACE 0.2 TO 0.3 D.
US349824A 1963-03-14 1964-03-06 Flexible couplings Expired - Lifetime US3257825A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10137/63A GB1000396A (en) 1963-03-14 1963-03-14 Improvements in or relating to torsionally flexible vibration damping apparatus

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US3257825A true US3257825A (en) 1966-06-28

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US (1) US3257825A (en)
AT (1) AT250102B (en)
BE (1) BE645029A (en)
CH (1) CH406742A (en)
DE (1) DE1450096B2 (en)
GB (1) GB1000396A (en)
NL (1) NL6402552A (en)
SE (1) SE308228B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830081A (en) * 1971-10-27 1974-08-20 Barth H Clutch
US4194373A (en) * 1978-02-13 1980-03-25 Sportscoach Corporation Shock isolation coupling
US6045448A (en) * 1997-01-27 2000-04-04 Generac Power Systems, Inc. Power-transmitting drive assembly with improved resilient devices

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5160532A (en) * 1974-11-25 1976-05-26 Konishiroku Photo Ind 1 doryokugenoryoshitefukusuno buzaioanteikudoseshimeuruyona doryokudentatsuseigyokikoojusuru fukushaki
DE3334562A1 (en) * 1983-09-23 1985-04-04 Bayerische Motoren Werke AG, 8000 München DEVICE FOR DAMPING TURNS IN A GEAR, IN PARTICULAR BETWEEN THE CRANKSHAFT AND A DRIVE SHAFT OF INTERNAL COMBUSTION ENGINES
DE29710545U1 (en) * 1997-06-17 1997-08-14 Stromag Ag, 59425 Unna Elastic coupling
DE10131331A1 (en) * 2001-06-28 2003-01-09 Ina Schaeffler Kg Device for torque transfer between rotary masses in IC engine, has damping and/or clamping bodies enabling relative movement in lower speed range and ensuring rigid coupling above this range

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE569343A (en) *
US1861390A (en) * 1929-06-10 1932-05-31 Packard Motor Car Co Vibration dampener for crank shafts
GB786091A (en) * 1955-04-04 1957-11-13 Croset Louis Paul Improvements in or relating to flexible couplings, dampers or the like
US2873590A (en) * 1955-12-16 1959-02-17 Louis P Croset Flexible couplings, dampers, gearwheels and like devices

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE569343A (en) *
US1861390A (en) * 1929-06-10 1932-05-31 Packard Motor Car Co Vibration dampener for crank shafts
GB786091A (en) * 1955-04-04 1957-11-13 Croset Louis Paul Improvements in or relating to flexible couplings, dampers or the like
US2873590A (en) * 1955-12-16 1959-02-17 Louis P Croset Flexible couplings, dampers, gearwheels and like devices

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830081A (en) * 1971-10-27 1974-08-20 Barth H Clutch
US4194373A (en) * 1978-02-13 1980-03-25 Sportscoach Corporation Shock isolation coupling
US6045448A (en) * 1997-01-27 2000-04-04 Generac Power Systems, Inc. Power-transmitting drive assembly with improved resilient devices

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Publication number Publication date
GB1000396A (en) 1965-08-04
DE1450096A1 (en) 1969-02-13
DE1450096B2 (en) 1970-07-09
BE645029A (en)
CH406742A (en) 1966-01-31
AT250102B (en) 1966-10-25
NL6402552A (en) 1964-09-15
SE308228B (en) 1969-02-03

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