WO1988006687A1 - Vibration compensator apparatus - Google Patents

Vibration compensator apparatus Download PDF

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Publication number
WO1988006687A1
WO1988006687A1 PCT/DK1988/000036 DK8800036W WO8806687A1 WO 1988006687 A1 WO1988006687 A1 WO 1988006687A1 DK 8800036 W DK8800036 W DK 8800036W WO 8806687 A1 WO8806687 A1 WO 8806687A1
Authority
WO
WIPO (PCT)
Prior art keywords
shafts
rotary
cranked
shaft
rotation
Prior art date
Application number
PCT/DK1988/000036
Other languages
French (fr)
Inventor
Henning Lindquist
Original Assignee
F.L. Smidth & Co. A/S - Maskinfabriken
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by F.L. Smidth & Co. A/S - Maskinfabriken filed Critical F.L. Smidth & Co. A/S - Maskinfabriken
Publication of WO1988006687A1 publication Critical patent/WO1988006687A1/en

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Classifications

    • 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
    • F16F15/22Compensation of inertia forces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H21/00Use of propulsion power plant or units on vessels
    • B63H21/30Mounting of propulsion plant or unit, e.g. for anti-vibration purposes
    • B63H21/302Mounting of propulsion plant or unit, e.g. for anti-vibration purposes with active vibration damping

Definitions

  • the present invention relates to a vibration compensato apparatus comprising a housing, where two shafts ar joilrnaled, each shaft having an excentric mass provide by rotary bodies, said shafts be " ing arranged to rotat around two mutually parallel axes of rotation and bein interconnected in order to rotate with the same number o revolutions but in opposite directions in order to generat a resulting force component equal to zero in one directio as well as a second resulting force component harmoni between zero and twice the force of the individual ex- centric mass in a direction perpendicular to the firs one .
  • A. known vibration compensator apparatus of the type men ⁇ tioned above compensates vertical, unbalanced moments of the second order in large ships with four, five and six cylinder engines.
  • this known vibration compensator apparatus the rotary bodies rotate in opposite directions such that the direction of the resulting, harmonic force component is " perpendicular to the common plane of the axes of rotation.
  • the axes of rotation are mounted at such a distance that the rotary bodies are able to simul ⁇ taneously pass the area between the axes of rotation with- out impeding each other.
  • Such a vibration compensator apparatus requires a large amount of space. Moreover it is very difficult or even impossible to instal it when it is desired to balance vibrations in the hull caused by a varying shaft pressure from the propeller or by varying side pressure from of the crosshead of the engine.
  • the object of the invention is to provide a vibration compensator apparatus of the type mentioned in the intro ⁇ duction for balancing hull vibrations, said apparatus being su ficiently compact to enable its installation in existing machines as well as in new ones.
  • the vibration compensator appa ⁇ ratus is characterized in that the shafts are interconnec ⁇ ted in such a way that the forces generated by the two excentric masses always point in a direction away from each other when the resulting, harmonicg force component is zero, and that the distance between the shafts is less than the diameter of the area defined by the rotation of the shafts and their rotary bodies.
  • the vibra- tion compensator apparatus is more compact than known ones . This is especially due to the fact that the rotary bodies do not have to pass the area between the axes of rotation simultaneously in opposite directions.
  • the shafts are interconnected In such a way that the direction of the resulting, harmonic force component is parallel to the common plane of the axes of rotation.
  • each shaft is a cranked shaft journaled in opposite walls of the housing, each cranked shaft being provided with one or more bends and being shaped in such- a way as to enable it to move passed the inner side of corresponding bends in the other cranked shaft.
  • each shaft comprises two journals, each mounted i opposite walls of the housing and permanently connecte with rotary arms, said rotary arms being interconnecte by means of rotary bodies arranged symmetrically aroun the plane of the cranked shafts and being of such an outer shape that they are able to pass each other at a close distance.
  • the rotary bodies providing the excentric masses have one or more inner cavities for the optional accomodation of further rotary mass. Consequently it is possible to adapt the resulting force component to the varying vibrations to be balanced.
  • the rotary bodies each comprise two tubes symmetrically arranged around the plane of the cranked shafts and being of cir- cular cross -section, said tubes being interconnected by means of two curved panels forming a convex, cylindrical body, each end of said cylindrical body being closed by means of an end plate, and the space between the tubes is filled with a material of high density, such as lead, and one of the end plates has openings corresponding to the inner clear of the tubes, each opening • being closed by means of a removable cover such that the tubes are able to be filled with further rotary masses for achieving the desired resulting force component, the rotary masses being for example weights of different density and with a cross- section corresponding to the inner clear of the tubes, and the wall opposite the cover is provided with an aper ⁇ ture for removing and replacing the cover and the weights, the center of said aperture being in one of the inter- sections between two cylinder surfaces defined by the tube axes of the rotary bodies during rotation.
  • Fig. 1 is a schematic, lateral view of the preferred embodiment of the inventive vibration compensator apparatus
  • Fi , 2 is a sectional view along the line II-II of Fig. 1,
  • Fig. 3 is a graph of the forces as well as the force com ⁇ ponents generated by the vibration compensator apparatus during operation
  • Fig. 4 is a detailed and partially sectional end view of the preferred embodiment of the inventive vibration compensator apparatus.
  • Fig. 5 is a sectional view along the line V-V of Fig. 4.
  • Figs. 1 and 2 are schematic views of a preferred embodiment of the inventive vibration compensator apparatus comprising a housing 1, where two cranked shafts 4, 4' with one bend each are journaled in opposite walls 2, 3 of the housing.
  • the distance a. between the axes of rotation 5, 5' of the oranked shafts 4, 4' is less than the radius of the area defined by the rotation of the cranked shafts 4, 4' .
  • the cranked shafts 4, 4' are of such a shape that each one is able to pass the inner side of the other cranked shaft during rotation, cf. Fig. 2.
  • the shafts are interconnected by means of gears 6, 6' to counterrotate at the same rpm and with such a phase as to generate a harmonic force com ponent in a direction parallel to the common plane of th axes of rotation 5, 5' , said force component varying be tween zero and twice the force of the individual shaft 4, 4' , and a second force component being constantly zer and perpendicular to the common plane of the axes of ro tation 5, 5' .
  • This is graphically illustrated in Fig. 3 where the force F generated by the two cranked shaft 4, 4 is resolved into component F ⁇ in the " common plane of th axes of rotation and component F t perpendicular to sai plane .
  • the vibration compensator apparatus is preferably drive by means of a hydraulic motor 7 coupled to one of th cranked shafts 4, said motor having a speed correspondin to the frequency of the vibrations to be balanced by th vibration compensator apparatus, i.e. a frequency corres ponds to the current speed of the motor times the numbe of cylinders, when the varying shaft pressure of a ship' propeller, the varying side pressure of the crosshead o the engine or the vertical, unbalanced moments of secon order of the engine are to be balanced.
  • the vibratio compensator apparatus is mounted in a strategic positio for balancing the current vibrations.
  • the best position In case of balancin vibrations generated by the varying shaft pressure of th propeller the best position is in the area behind the fly ⁇ wheel of the diesel engine. In case of balancing vibration generated by the varying side pressure of the crosshead o the engine the best position is on the top and/or botto of the diesel engine. In case of balancing vibrations generated by the vertical, unbalanced moments of the engine the best position is in the control machine room of the ship .
  • the preferred embodiment of the vibration compensator apparatus is described in greater detail below and with reference to Figs. 4 and 5. It comprises, as described with reference to Figs. 1 and 2, a housing 11, where two cranked shafts 14, 14' are j ournaled in opposite walls 12, 13 of the housing rotatably around parallel axes of rota ⁇ tion 15, 15' .
  • the shafts 14, 14' are driven by means of a hydraulic motor 17.
  • Two gears 16, 16 ' cause the shafts 14, 14' to rotate in opposite directions.
  • Each cranked shaft includes two shaft journals 18, 19, 18' , 19' rotatably journaled in opposite walls 12, 13 by means of roller bearings.
  • Each shaft journal is permanently connected to a rotary arm 20, 21, 20' , 21'.
  • the rotary arms 20, 21, 20' , 21' are interconnected by means of rotary bodies 22, 22' symmetrically arranged around the plane of the cranked shafts 14, 14' .
  • Each rotary body comprises two tubes 23, 24, 23 ' , 24' symmetrically arranged around the plane of the cranked shafts and being of circular cross- section. In Figs. 4 and 5 only 23 and 23' are fully visible.
  • the tubes are interconnected by means of two curved panels 25, 26, 25' , 26', forming a convex, cylin- drical body.
  • the cylindrical body is closed at each end by means of an end plate 27, 28, 27' , 28' .
  • the space be ⁇ tween the circular tubes 23 and 24, 23' and 24' and the curved panels 25, 26, 25' 26' is filled with a material of large density, such as lead.
  • One end plate 27, 27' of each rotary body 22 r 22' has two openings 29, 30, 29' , 30' corresponding to the inner clear of the tube. In Figs. 4 and 5 only 29 and 29' are visible.
  • Each opening 29, 30, 29 ' , 30' is closed by means of a removable cover 31 also having a diameter corresponding to the inner clear of the circular tubes 23, 24, 23', 24' .
  • the cover is furthermore provided with two throughholes 32, 33.
  • each of the other end plates 28, 28' is provided with two axially extending stay bolts 34, 35 mutually spaced corresponding to the distance be ⁇ tween the two throughholes 32, 33, In the cover 31.
  • the inside of each tube 23, 24, 23' , 24' is completel filled with weights 36 with throughbores corresponding t the stay bolts.
  • the weights are retained by the cover 3 by means of the latter being fastened by screwing nuts o 5 the stay bolts 34, 35.
  • Ad- 10 vantageously the weights are manufactured of a materia of high density, such as lead, as well as a material o low density, such a wood. Consequently the resulting force component is variable within a rather large area.
  • the rotary bodies 22, 22' are of such a shape, cf. the sectional part of Fig. 4, that they pass each other at a narrow distance and on each other's inner side whe crossing the plane of the axes of rotation in opposite directions in order to render the vibration compensator
  • the opposing walls 12, 13 are interconnected by means of a housing wall 37 having a cross- section corresponding to the area defined by the rotation of the rotary bodies 22,
  • One wall 12 is provided with an aperture 38, the center of which is on one of the intersections between the two cylinder surfaces 39, 39' defined by the tube axes of the rotary bodies 22, 22' during rotation.
  • the aperture 38 is of a slightly larger diameter than the
  • the transmission housing 41 is closed by means of a top 42 provided with an opening 43. Through said opening 43 the shaft journal 18 Is connected with the hydraulic motor 17 via a planet gear 44 fastened to the top 42. Furthermore the top 42 is pro ⁇ vided with an aperture (not shown) corresponding to the aperture 38 in the wall 12, said aperture being used for removing and replacing the weights 36 from the rotary bodies 22, 22 ' .

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

Vibration compensator apparatus comprising a housing (1, 11) where two shafts (4, 4', 14, 14') are journaled, each shaft having an excentric mass provided by rotary bodies (22, 22'). The shafts (4, 4', 14, 14') are arranged to rotate around two mutually parallel axes of rotation (5, 5', 15, 15') and are interconnected in order to rotate with the same number of revolutions but in opposite directions in order to generate a resulting force component equal to zero in one direction as well as a second resulting force component harmonic between zero and twice the force (F) of the individual excentric mass in a direction perpendicular to the first one. The shafts (4, 4', 14, 14') are interconnected in such a way that the forces generated by the two excentric masses always point in a direction away from each other when the resulting, harmonic force component is zero. The distance between the shafts (a) is less than the diameter of the area defined by the rotation of the shafts (4, 4', 14, 14') and their rotary bodies (22, 22').

Description

Title: Vibration compensator apparatus
Technical Field
The present invention relates to a vibration compensato apparatus comprising a housing, where two shafts ar joilrnaled, each shaft having an excentric mass provide by rotary bodies, said shafts be"ing arranged to rotat around two mutually parallel axes of rotation and bein interconnected in order to rotate with the same number o revolutions but in opposite directions in order to generat a resulting force component equal to zero in one directio as well as a second resulting force component harmoni between zero and twice the force of the individual ex- centric mass in a direction perpendicular to the firs one .
Background Art
A. known vibration compensator apparatus of the type men¬ tioned above compensates vertical, unbalanced moments of the second order in large ships with four, five and six cylinder engines. In this known vibration compensator apparatus the rotary bodies rotate in opposite directions such that the direction of the resulting, harmonic force component is" perpendicular to the common plane of the axes of rotation. The axes of rotation are mounted at such a distance that the rotary bodies are able to simul¬ taneously pass the area between the axes of rotation with- out impeding each other. Such a vibration compensator apparatus requires a large amount of space. Moreover it is very difficult or even impossible to instal it when it is desired to balance vibrations in the hull caused by a varying shaft pressure from the propeller or by varying side pressure from of the crosshead of the engine.
Disclosure of the Invention The object of the invention is to provide a vibration compensator apparatus of the type mentioned in the intro¬ duction for balancing hull vibrations, said apparatus being su ficiently compact to enable its installation in existing machines as well as in new ones.
According to the invention the vibration compensator appa¬ ratus is characterized in that the shafts are interconnec¬ ted in such a way that the forces generated by the two excentric masses always point in a direction away from each other when the resulting, harmonicg force component is zero, and that the distance between the shafts is less than the diameter of the area defined by the rotation of the shafts and their rotary bodies. As a result the vibra- tion compensator apparatus is more compact than known ones . This is especially due to the fact that the rotary bodies do not have to pass the area between the axes of rotation simultaneously in opposite directions.
According to the invention the shafts are interconnected In such a way that the direction of the resulting, harmonic force component is parallel to the common plane of the axes of rotation. This is an especially suitable embodiment of the present invention, as the inner moment in the vibration compensator apparatus is reduced.
In another embodiment the distance between the shafts is less than the radius of the area defined by the rotation of the shafts and their rotary bodies and each shaft is a cranked shaft journaled in opposite walls of the housing, each cranked shaft being provided with one or more bends and being shaped in such- a way as to enable it to move passed the inner side of corresponding bends in the other cranked shaft. This embodiment results in an especially compact vibration compensator apparatus, reducing the inner moment even further. In a further embodiment the cranked shafts are identical and each shaft comprises two journals, each mounted i opposite walls of the housing and permanently connecte with rotary arms, said rotary arms being interconnecte by means of rotary bodies arranged symmetrically aroun the plane of the cranked shafts and being of such an outer shape that they are able to pass each other at a close distance. This is an especially simple and preferred em¬ bodiment of the invention.
In yet another embodiment the rotary bodies providing the excentric masses have one or more inner cavities for the optional accomodation of further rotary mass. Consequently it is possible to adapt the resulting force component to the varying vibrations to be balanced.
In a preferred embodiment of the invention the rotary bodies each comprise two tubes symmetrically arranged around the plane of the cranked shafts and being of cir- cular cross -section, said tubes being interconnected by means of two curved panels forming a convex, cylindrical body, each end of said cylindrical body being closed by means of an end plate, and the space between the tubes is filled with a material of high density, such as lead, and one of the end plates has openings corresponding to the inner clear of the tubes, each opening being closed by means of a removable cover such that the tubes are able to be filled with further rotary masses for achieving the desired resulting force component, the rotary masses being for example weights of different density and with a cross- section corresponding to the inner clear of the tubes, and the wall opposite the cover is provided with an aper¬ ture for removing and replacing the cover and the weights, the center of said aperture being in one of the inter- sections between two cylinder surfaces defined by the tube axes of the rotary bodies during rotation. Brief Description of the Drawings
The invention is described in greater detail below and with reference to the accompanying drawings , in which
Fig. 1 is a schematic, lateral view of the preferred embodiment of the inventive vibration compensator apparatus ,
Fi , 2 is a sectional view along the line II-II of Fig. 1,
Fig. 3 is a graph of the forces as well as the force com¬ ponents generated by the vibration compensator apparatus during operation,
Fig. 4 is a detailed and partially sectional end view of the preferred embodiment of the inventive vibration compensator apparatus, and
Fig. 5 is a sectional view along the line V-V of Fig. 4.
Best Mode for Carrying out the Invention
Figs. 1 and 2 are schematic views of a preferred embodiment of the inventive vibration compensator apparatus comprising a housing 1, where two cranked shafts 4, 4' with one bend each are journaled in opposite walls 2, 3 of the housing. The distance a. between the axes of rotation 5, 5' of the oranked shafts 4, 4' is less than the radius of the area defined by the rotation of the cranked shafts 4, 4' .
The cranked shafts 4, 4' are of such a shape that each one is able to pass the inner side of the other cranked shaft during rotation, cf. Fig. 2. The shafts are interconnected by means of gears 6, 6' to counterrotate at the same rpm and with such a phase as to generate a harmonic force com ponent in a direction parallel to the common plane of th axes of rotation 5, 5' , said force component varying be tween zero and twice the force of the individual shaft 4, 4' , and a second force component being constantly zer and perpendicular to the common plane of the axes of ro tation 5, 5' . This is graphically illustrated in Fig. 3 where the force F generated by the two cranked shaft 4, 4 is resolved into component F^ in the "common plane of th axes of rotation and component Ft perpendicular to sai plane .
The vibration compensator apparatus is preferably drive by means of a hydraulic motor 7 coupled to one of th cranked shafts 4, said motor having a speed correspondin to the frequency of the vibrations to be balanced by th vibration compensator apparatus, i.e. a frequency corres ponds to the current speed of the motor times the numbe of cylinders, when the varying shaft pressure of a ship' propeller, the varying side pressure of the crosshead o the engine or the vertical, unbalanced moments of secon order of the engine are to be balanced. The vibratio compensator apparatus is mounted in a strategic positio for balancing the current vibrations. In case of balancin vibrations generated by the varying shaft pressure of th propeller the best position is in the area behind the fly¬ wheel of the diesel engine. In case of balancing vibration generated by the varying side pressure of the crosshead o the engine the best position is on the top and/or botto of the diesel engine. In case of balancing vibrations generated by the vertical, unbalanced moments of the engine the best position is in the control machine room of the ship .
The preferred embodiment of the vibration compensator apparatus is described in greater detail below and with reference to Figs. 4 and 5. It comprises, as described with reference to Figs. 1 and 2, a housing 11, where two cranked shafts 14, 14' are j ournaled in opposite walls 12, 13 of the housing rotatably around parallel axes of rota¬ tion 15, 15' . The shafts 14, 14' are driven by means of a hydraulic motor 17. Two gears 16, 16 ' cause the shafts 14, 14' to rotate in opposite directions.
Each cranked shaft includes two shaft journals 18, 19, 18' , 19' rotatably journaled in opposite walls 12, 13 by means of roller bearings. Each shaft journal is permanently connected to a rotary arm 20, 21, 20' , 21'. The rotary arms 20, 21, 20' , 21' are interconnected by means of rotary bodies 22, 22' symmetrically arranged around the plane of the cranked shafts 14, 14' . Each rotary body comprises two tubes 23, 24, 23 ' , 24' symmetrically arranged around the plane of the cranked shafts and being of circular cross- section. In Figs. 4 and 5 only 23 and 23' are fully visible. The tubes are interconnected by means of two curved panels 25, 26, 25' , 26', forming a convex, cylin- drical body. The cylindrical body is closed at each end by means of an end plate 27, 28, 27' , 28' . The space be¬ tween the circular tubes 23 and 24, 23' and 24' and the curved panels 25, 26, 25' 26' is filled with a material of large density, such as lead. One end plate 27, 27' of each rotary body 22r 22' has two openings 29, 30, 29' , 30' corresponding to the inner clear of the tube. In Figs. 4 and 5 only 29 and 29' are visible. Each opening 29, 30, 29 ' , 30' is closed by means of a removable cover 31 also having a diameter corresponding to the inner clear of the circular tubes 23, 24, 23', 24' . The cover is furthermore provided with two throughholes 32, 33.
In the area inside the tubes each of the other end plates 28, 28' is provided with two axially extending stay bolts 34, 35 mutually spaced corresponding to the distance be¬ tween the two throughholes 32, 33, In the cover 31. The inside of each tube 23, 24, 23' , 24' is completel filled with weights 36 with throughbores corresponding t the stay bolts. The weights are retained by the cover 3 by means of the latter being fastened by screwing nuts o 5 the stay bolts 34, 35. Due to filling the inside of eac tube 23, 24, 23' , 24' with weights 36 manufactured o materials with different density the overall mass of eac rotary body 22, 22' and thus the resulting force componen can be varied in order to achieve the desired value. Ad- 10 vantageously the weights are manufactured of a materia of high density, such as lead, as well as a material o low density, such a wood. Consequently the resulting force component is variable within a rather large area.
15 The rotary bodies 22, 22' are of such a shape, cf. the sectional part of Fig. 4, that they pass each other at a narrow distance and on each other's inner side whe crossing the plane of the axes of rotation in opposite directions in order to render the vibration compensator
20 apparatus as compact as possible.
The opposing walls 12, 13 are interconnected by means of a housing wall 37 having a cross- section corresponding to the area defined by the rotation of the rotary bodies 22,
2522' , cf. Fig. 4. One wall 12 is provided with an aperture 38, the center of which is on one of the intersections between the two cylinder surfaces 39, 39' defined by the tube axes of the rotary bodies 22, 22' during rotation. The aperture 38 is of a slightly larger diameter than the
30removable cover 31 and is used for removing and replacing the weights 36 in the tubes 23, 24, 23' , 24' . The outside of the wall 12 is connected with the housing wall 37 by means of screws 40. Furthermore a transmission housing 41 is welded onto the outside of the wall 12, the gears 16,
3516' mounted on the ends of the shaft journals 18, 18' meshing inside said housing. The transmission housing 41 is closed by means of a top 42 provided with an opening 43. Through said opening 43 the shaft journal 18 Is connected with the hydraulic motor 17 via a planet gear 44 fastened to the top 42. Furthermore the top 42 is pro¬ vided with an aperture (not shown) corresponding to the aperture 38 in the wall 12, said aperture being used for removing and replacing the weights 36 from the rotary bodies 22, 22 ' .

Claims

Claims
1. Vibration compensator apparatus comprising a housi (1, 11) where two shafts (4, 4' , 14, 14') are journale 5 each shaft having an excentric mass provided by rota bodies (22, 22'), said shafts (4, 4' , 14, 14') bei arranged to rotate around two mutually parallel axes o rotation (5, 5' , 15, 15') and being interconnected in orde to rotate with the same number of revolutions but i
10 opposite directions in order to generate a resulting forc component equal to zero in one direction as well as second resulting force component harmonic between zero an twice the force (F) of the individual excentric mass in direction perpendicular to the first one, c h a r a c -
15 t e r i z e d in that the shafts (4, 4' , 14, 14') ar interconnected in such a way that the forces generated b the two excentric masses always point in a direction awa from each other when the resulting, harmonic force com ponent is zero, and that the distance between the shaft
20 (ϋ.) is less than the diameter of the area defined by th rotation of the shafts (4, 4' , 14, 14') and their rotar bodies (22, 22').
2. A vibration compensator apparatus as claimed in clai 25 1, c h a r a c t e r i z e d in that the shafts ar interconnected in such a way that the direction of th resulting, harmonic force component is parallel to th common plane of the axes of rotation (5, 5' , 15, 15').
303. A vibration compensator apparatus as claimed in clai 1 or 2 , c h a r a c t e r i z e d in that the distanc between the shafts (a.) is less than the radius of th area defined by the rotation of the shafts (4, 4' , 14 14') and their rotary bodies (22, 22') , and that eac
35 shaft (4, 4' , 14, 14') is a cranked shaft journaled i opposite walls (2, 3) of the housing, each cranked shaf being provided with one or more bends and being shaped i such a way as to enable it to move passed the inner side of corresponding bends in the other cranked shaft.
4. A vibration compensator apparatus as claimed in claim 3, c h a r a c t e r i z e d in that the cranked shaf s
(4, 4' , 14, 14') are Identical and that each shaft com¬ prises two journals (18, 19, 18' , 19') each mounted in opposite walls (2, 3) of the housing and permanently connected with rotary arms (20, 21, 20' , 21'), said rotary arms (20, 21, 20', 21') being interconnected by means of rotary bodies (22, 22') arranged symmetrically around the plane of the cranked shafts and being of such an outer shape that they are able to pass each other at a close distance .
5. A vibration compensator apparatus as claimed in one or more of the claims 1-4, c h a r a c t e r i z e d In that the rotary bodies (22, 22') providing the excentric masses have one or more inner cavities for the optional accomodation of further rotary mass.
6. A vibration compensator apparatus as claimed in claims 2-5, c h a r a c t e r i z e d in that the rotary bodies (22, 22') each comprise two tubes (23, 24, 23' , 24') symme- trically arranged around the plane of the cranked shafts and being of circular cross-section, said tubes being interconnected by means of two curved panels (25, 26, 25', 26') forming a convex, cylindrical body, each end of said cylindrical body being closed by means of an end plate (27, 28), and that the space" between the tubes (23 and 24, 23 'and 24') Is filled with a material of high density, such as lead, and that one of the end plates (27, 27') has openings (29, 30, 29' , 30') corresponding to the inner clear of the tubes (23, 24, 23', 24') , each opening being closed by means of a removable cover (31) , such that the tubes are able to be filled with further rotary masses for achieving the desired resulting force component, the rotary masses being for example weights (36) of different density and with a cross - section corres¬ ponding to the inner clear of the tubes (23, 24, 23', 24'), and that the wall (12) opposite the cover is provided with an aperture (38) for removing and replacing the cover (31) and the weights (36), the center of said aperture being in one of the intersections between two cylinder surfaces (39, 39') defined by the tube axes of the rotary bodies (22, 22') during rotation.
PCT/DK1988/000036 1987-03-02 1988-02-25 Vibration compensator apparatus WO1988006687A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DK107487A DK155544C (en) 1987-03-02 1987-03-02 VICTION COMPENSATOR
DK1074/87 1987-03-02

Publications (1)

Publication Number Publication Date
WO1988006687A1 true WO1988006687A1 (en) 1988-09-07

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AU (1) AU1396088A (en)
DK (1) DK155544C (en)
WO (1) WO1988006687A1 (en)
YU (1) YU41988A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0409462A1 (en) * 1989-07-14 1991-01-23 Barry Wright Corporation Inertia force generating device
FR2886176A1 (en) * 2005-05-25 2006-12-01 Eurocopter France CENTRIFUGAL EFFECT VIBRATION GENERATOR WITH COAXIAL CONTRAROTATIVE ROTORS.
EP1818141A2 (en) 2003-03-21 2007-08-15 Black & Decker, Inc. Vibration reduction apparatus for power tool and power tool incorporating such apparatus
WO2008145122A1 (en) * 2007-05-31 2008-12-04 Vestas Wind Systems A/S A system for damping oscillations in a structure

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0011378A1 (en) * 1978-10-12 1980-05-28 Kubota Limited An internal combustion engine having a balancing device
GB2118693A (en) * 1982-03-16 1983-11-02 Aida Eng Ltd Balance device for a press
EP0245583A2 (en) * 1986-05-12 1987-11-19 Tecumseh Products Company Inline counterbalance weight system for a single cylinder engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0011378A1 (en) * 1978-10-12 1980-05-28 Kubota Limited An internal combustion engine having a balancing device
GB2118693A (en) * 1982-03-16 1983-11-02 Aida Eng Ltd Balance device for a press
EP0245583A2 (en) * 1986-05-12 1987-11-19 Tecumseh Products Company Inline counterbalance weight system for a single cylinder engine

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0409462A1 (en) * 1989-07-14 1991-01-23 Barry Wright Corporation Inertia force generating device
EP1818141A2 (en) 2003-03-21 2007-08-15 Black & Decker, Inc. Vibration reduction apparatus for power tool and power tool incorporating such apparatus
EP1932627A2 (en) 2003-03-21 2008-06-18 Black & Decker, Inc. Vibration reduction apparatus for power tool and power tool incorporating such apparatus
EP1932626A2 (en) 2003-03-21 2008-06-18 Black & Decker, Inc. Vibration reduction apparatus for power tool and power tool incorporating such apparatus
EP2119536A2 (en) 2003-03-21 2009-11-18 BLACK & DECKER INC. Power tool incorporating vibration reduction apparatus
DE202004021825U1 (en) 2003-03-21 2011-05-05 Black & Decker Inc., Newark Vibration reduction device for a power tool and power tool with such a device
FR2886176A1 (en) * 2005-05-25 2006-12-01 Eurocopter France CENTRIFUGAL EFFECT VIBRATION GENERATOR WITH COAXIAL CONTRAROTATIVE ROTORS.
EP1728716A1 (en) * 2005-05-25 2006-12-06 Eurocopter Schwingungserreger durch Zentrifugal-Effekt mit koaxialen gegenläufigen Rotoren
US7554237B2 (en) 2005-05-25 2009-06-30 Eurocopter Centrifugal-effect vibration generator having coaxial contrarotating rotors
WO2008145122A1 (en) * 2007-05-31 2008-12-04 Vestas Wind Systems A/S A system for damping oscillations in a structure
US9004246B2 (en) 2007-05-31 2015-04-14 Vestas Wind Systems A/S System for damping oscillations in a structure

Also Published As

Publication number Publication date
DK107487D0 (en) 1987-03-02
DK155544C (en) 1989-10-09
DK107487A (en) 1988-09-03
YU41988A (en) 1990-10-31
AU1396088A (en) 1988-09-26
DK155544B (en) 1989-04-17

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