CA1216161A

CA1216161A - Low torsional stiffness flexible coupling

Info

Publication number: CA1216161A
Application number: CA000436074A
Authority: CA
Inventors: John Wright
Original assignee: Koppers Co Inc
Current assignee: Beazer East Inc
Priority date: 1982-09-07
Filing date: 1983-09-06
Publication date: 1987-01-06
Also published as: GB8322381D0; GB2126690A; GB2126690B

Abstract

ABSTRACT OF THE DISCLOSURE
Disclosed is a flexible coupling which is characterized by low torsional stiffness when a relatively low torque load is applied to the coupled shafts.
The coupling includes a plurality of variable stiffness torque transmitting elements which permit low torsional stiffness at low torque but also permit the coupling to operate at a relatively higher torque load.

Description

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BACKGROUND OF THE INVENTION
This invention relates to flexible couplings by which torque is transmitted between two shafts by means of elastomeric elements in compression and, more particularly, to such a flexible coupling which has a low torsional stiffness when a relatively low torque load is applied to the coupled shafts.
DESCRIPTION OF THE PRIOR ART
Flexible couplings for transmitting torque between misaligned driving and driven shafts by means of elastomeric elements in compression are old and well known in the arts, see US. Patent Nos. 2,764,003 and 2,873,590. Such couplings have not only demonstrated the ability to compensate for misalignment between the driving and driven shaft but also to protect the driving and driven members from torsional shock loading and torsional vibration in most applications. Use of such couplings in diesel marine drive systems has presented a unique set of problems since the coupling must be designed to act over a wide range of speeds and therefore over a wide range of torque, since in marine propellers the torque is proportional to the square of the speed. It is desirable to provide a torsional stiffness low enough to place the resonances or critical speeds for a particular mode of torsion vibrations below minimum operating speed. When the coupling used is designed to handle the highest torque loadings at full speed, it is sometimes too stiff under low speed, low torque conditions and torsional resonance may occur at the lower operating speeds. This vibration can damage the propulsion system. However, if the coupling used has a suitably low torsional stiffness, it often cannot handle the high torque developed at higher speeds. This has led to numerous cases of coupling and other drive component failure. Both vibration damage and coupling failure are expensive in terms of repair parts and downtime.
SUMMARY OF THE INVENTION
The present invention overcomes the foregoing problems of the prior art by 12~ L61 providing a coupling having low torsional stiffness at low torque loads but also having sufficient stiffness to handle high torque loads. Each cavity formed in part by the blades of the hub and sleeve of the coupling contains a plurality of elastomeric elements of different harnesses. Under low torque only the lower hardness elements are compressed resulting in a low torsional stiffness. However, at high torque loadings the higher hardness elements also become compressed and limit the torsional windup of the coupling so that the lower hardness elements will not become overstrainecl.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a side view, partially in section, of the coupling of the present invention, Figure 2 is a fragmentary and view of the coupling of Figure l; and Figure 3 is an enlarged view of the portion of Figure 1 in section.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Couplings by which torque is transmitted between two shafts by means of elastomeric elements in compression are fully described in US. Patent Nos.

2,764,003 and 2,873,590.
Referring to Figures 1 and 2, the coupling of the present invention generally designated lo is comprised of a hub 12 which has blades 14 that is mounted on one of the pair of shafts to be rotated. In the preferred embodiment, the hub 12 is made of cast ductile iron or cast steel. The sleeve element 16 of the coupling which is mounted on the other shaft has blades 18 which in combination with blades 14, plate 20 and end plate 22 form the cavities 24 which contain the elastomeric elements 26 and I The size of blades 14 and 18 and the corresponding size of cavities 24 are design considerations based on the use the coupling is to undergo. These design considerations are well known and understood in the art and will not be repeated here as they form no part of the present invention.

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Elastomeric elements 26 are made of a relatively hard, of approximately 75 dormitory, rubber and are placed on each side of an element 28 in each cavity 24. Element 28 is made of a softer rubber, of approximately 45 dormitory.
Elements 26 which is circular in cross section have a smaller diameter than the diameter of element 28 and a pin 30 through elements 26 and 28 maintains their concentricity. Pin 30 may be of metal or plastic or some other suitable material. Under a low torque load only elements 28 would be compressed and the coupling would have a low torsional stiffness; but as torque increased elements 26 would be compressed preventing overtraining of element 28.
While I have described a certain preferred embodiment of my invention, it will be understood it may otherwise be embodied within the scope of the following claims.

Claims

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE PROEPRTY OR
PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:

1. An improved flexible coupling for transmitting torque between a driving and driven shaft comprised of a hub means having outwardly extending blade members, said hub being mounted on one of said shafts and a sleeve element having inwardly extending blade members, said sleeve member being mounted on the other of said shafts, said blades defining cavities for containing elastomeric elements in compression for transmitting torque between said shafts, the improvement comprising;
the elastomeric elements in compression in each of said cavities including at least one element having a relatively low hardness and at least one element having a comparable, relatively high hardness.

2. The coupling of claim 1 wherein said elastomeric elements in compression in each cavity include one element of relatively low hardness contained between two elements of relatively high hardness.

3. The coupling of claim 2 wherein the elements having a relatively high hardness have a smaller diameter than the element having a relatively low hardness.

4. The coupling of claim 3 wherein a pin member maintains the concentricity of the elastomeric elements.