GB1578750A - Springs - Google Patents

Springs Download PDF

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Publication number
GB1578750A
GB1578750A GB35898/76A GB3589876A GB1578750A GB 1578750 A GB1578750 A GB 1578750A GB 35898/76 A GB35898/76 A GB 35898/76A GB 3589876 A GB3589876 A GB 3589876A GB 1578750 A GB1578750 A GB 1578750A
Authority
GB
United Kingdom
Prior art keywords
layers
spring
rubber
plates
layer
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB35898/76A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dunlop Ltd
Original Assignee
Dunlop Ltd
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 Dunlop Ltd filed Critical Dunlop Ltd
Priority to GB35898/76A priority Critical patent/GB1578750A/en
Priority to CA284,938A priority patent/CA1070721A/en
Priority to CH1016977A priority patent/CH612253A5/en
Priority to IN1298/CAL/77A priority patent/IN148753B/en
Priority to DE19772738168 priority patent/DE2738168A1/en
Priority to SE7709528A priority patent/SE7709528L/en
Priority to FR7725916A priority patent/FR2363032A1/en
Priority to HU77DU273A priority patent/HU173176B/en
Priority to PL1977200494A priority patent/PL119454B1/en
Priority to RO7791477A priority patent/RO76133A/en
Priority to JP10353077A priority patent/JPS5329470A/en
Publication of GB1578750A publication Critical patent/GB1578750A/en
Expired legal-status Critical Current

Links

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
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/40Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers

Description

(54) IMPROVEMENTS IN OR RELATING TO SPRINGS (71) We, DUNLOP LIMITED, a British Company of Dunlop House, Ryder Street, St. James's, London S.W.1. do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: This invention relates to springs, and in particular to sandwich type springs comprising a stack of layers of rubber or like elastomeric material bonded to interleaving metal plates.
Sandwich type springs of this type are often used, amongst other applications, as part of a railway vehicle bogie suspension and in such an application the springs are usually mounted with their rubber layers and metal plates substantially horizontal so that the vehicle weight acts to cause substantially only compression loading of the rubber layers whilst relative lateral movements between parts of the vehicle suspension causes shear deflection of the rubber layers.
Especially under relatively large shear displacements there is a significant reduction in the effective cross-sectional area of the spring directly to support compression loads as upper layers of the spring move laterally relative to lower layers and only a relatively small part of an upper layer lies above and is directly supported by lower layers. It is found in this situation that the resulting combination of shear and compression loadings results in the rubber layers being subjected to bending moment stresses, and fatigue failures commonly occur at the outermost layers of the spring where the bending moment stresses are greatest.
It is an object of the present invention to provide a sandwich type spring having an improved fatigue life under the action of shear loadings.
According to the present invention a spring comprises a plurality of layers of rubber or like elastomeric material bonded to and interlocking with a plurality of metal plates wherein the length of the layers of rubber or like elastomeric material as considered in at least one cross-sectional plane extending substantially perpendicular to the plane of said layers and metal plates decreases from each outermost- layer in a direction towards the centre layer or layers and the thickness of the centre layer or layers of rubber or like elastomeric material is less than the thickness of the outermost layers.
Preferably the length of the layers in said cross-sectional plane decreases uniformly from each outermost layer in a direction towards the centre layer or layers of the spring, and successive layers preferably are positioned centrally relative to each other such that, in an unloaded condition.
the spring has a symmetrical profile when viewed in said plane.
In operation of the spring when subjected to shear forces acting in a direction lying in said plane the effective area of the spring for supporting compression loads remains substantially unaltered, at that of the central or smallest area layer of rubber or like elastomeric material, and there is no significant reduction of area as in the case of a conventional sandwich spring where all layers are of equal- size.
Furthermore, it is found in comparison with a conventional sandwich spring that each rubber layer and metal plate is more able to move angularly relative to end faces of the spring under the action of shear loads; the bending resistance of any one layer is more nearly proportional to the bending moment applied by the combination of external compression and shear forces and this results in an improvement of fatigue life compared with a conventional spring.
In addition to the variation in length of successive rubber layers in said cross-sectional plane, the length of the rubber layers may be varied similarly in one or more other planes substantially perpendicular to the plane of the rubber layers and metal plates so as to improve the fatigue resistance of the spring to shear loads acting in more than one direction.
The outer profiles of the rubber layers as considered in planes parallel to the metal plates may be rectangular, square, circular, or elliptical, though other shapes, such as polygonal shapes, may be employed. Considered also in said planes, the rubber layers may be formed with apertures so as to be essentially -ring-shaped, and the metal plates may also be formed with apertures such that the spring has- - a hollow cavity therein, though to obtain good fatigue life it is generally preferred that neither rubber layers nor plates are formed with apertures. The spring may be provided with a passage communicating between the hollow cavity and outside of the spring. The cavity may be air-tight, a suitable valve or seal being provided to maintain the cavity air-tight where the spring is formed with a passage.
In a preferred constructon the thickness of the layers of rubber or like elastomeric material increases progressively from the centre layer or layers towards each outermost layer.
One embodiment of the invention will now be described, by way of example, with reference to the accompanying diagrammatic drawing in which: Figure 1 is a side - view of a spring in accordance with the present invention in an unloaded condition; Figure 2 is a similar view to that of Figure 1 showing the spring loaded in compression, and Figure 3 is a similar view to that of Figure 1 showing the spring loaded in compression and shear.
A sandwich type suspension spring 10 for use in a railway vehicle bogie suspension comprises a plurality of rubber layers 11 bonded to and interleaved with a plurality of metal plates 12 and metal end plates 13.
The thickness of the rubber layers 11 increases progressively from the central layers 1 lea to the outermost layers, and the length of the rubber layers and interleaving plates as viewed in the direction of Figure 1 also increase progressively from the central layers and plates to the outermost layers and plates.
All rubber layers are of equal depth in a direction perpendicular to the plane of Figure 1 along the entire length of each layer as viewed in Figure 1 and the plates are like wise-shaped. The central rubber layers and metal plate are of a square outer profile and accordingly the relatively outer rubber layers and plates are of rectangular outer profile.
When the spring is subjected to a combination of shear and compression loadings, as illustrated in Figure 3, the effective area of the spring directly to support compression loads remains substantially unaltered at the cross-sectional area of the centre rubber layers I la and this assists to minimise the bending stresses on the outermost rubber layers and thus improve their fatigue life as compared with a conventional spring having rubber layers and plates all of similar dimensions. It will be further appreciated from Figure 3 that by use of central rubber layers and plates which are shorter than relatively outer layers and plates, all layers and plates are more able to move angularly relative to the end plates than in a conventional spring where all plates and layers are of similar dimensions, and accordingly there results a more uniform distribution of bending stresses between all of the rubber layers so as to assist in improving the fatigue life of the spring.
WHAT WE CLAIM IS: 1. Aspring comprising a plurality of layers of rubber or like elastomeric material bonded to and interleaved with a plurality of metal plates wherein the length of the layers of rubber or like elastomeric material as considered in at least one cross-sectional plane extending substantially perpendicular to the plane of said layers and metal plates decreases from each outermost layer in a direction towards the centre layer or layers and the thickness of the centre layer or layers of rubber or like elastomeric material is less than the thickness of the outermost layers.
2. A spring according to claim 1 wherein the length of the layers in said cross-sectional plane decreases uniformly from each outermost layer in a direction towards the centre layer or layers of the spring.
3. A spring according to claim 1 or claim 2 wherein successive layers are positioned centrally relative to one another when viewed in cross-sectional plane.
4. A spring according to any one of the preceding claims wherein the length of the layers of rubber or like elastomeric material as considered in one or more other planes substantially perpendicular to the plane of said layers and metal plates decreases from each outermost layer in a direction towards the centre layer or layers.
5. A spring according to any one of the preceding claims wherein considered in planes parallel to the layers of rubber or like elastomeric material and metal plates a layer and/or a metal plate is apertured.
6. A spring according to claim 5 having
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (10)

**WARNING** start of CLMS field may overlap end of DESC **. successive rubber layers in said cross-sectional plane, the length of the rubber layers may be varied similarly in one or more other planes substantially perpendicular to the plane of the rubber layers and metal plates so as to improve the fatigue resistance of the spring to shear loads acting in more than one direction. The outer profiles of the rubber layers as considered in planes parallel to the metal plates may be rectangular, square, circular, or elliptical, though other shapes, such as polygonal shapes, may be employed. Considered also in said planes, the rubber layers may be formed with apertures so as to be essentially -ring-shaped, and the metal plates may also be formed with apertures such that the spring has- - a hollow cavity therein, though to obtain good fatigue life it is generally preferred that neither rubber layers nor plates are formed with apertures. The spring may be provided with a passage communicating between the hollow cavity and outside of the spring. The cavity may be air-tight, a suitable valve or seal being provided to maintain the cavity air-tight where the spring is formed with a passage. In a preferred constructon the thickness of the layers of rubber or like elastomeric material increases progressively from the centre layer or layers towards each outermost layer. One embodiment of the invention will now be described, by way of example, with reference to the accompanying diagrammatic drawing in which: Figure 1 is a side - view of a spring in accordance with the present invention in an unloaded condition; Figure 2 is a similar view to that of Figure 1 showing the spring loaded in compression, and Figure 3 is a similar view to that of Figure 1 showing the spring loaded in compression and shear. A sandwich type suspension spring 10 for use in a railway vehicle bogie suspension comprises a plurality of rubber layers 11 bonded to and interleaved with a plurality of metal plates 12 and metal end plates 13. The thickness of the rubber layers 11 increases progressively from the central layers 1 lea to the outermost layers, and the length of the rubber layers and interleaving plates as viewed in the direction of Figure 1 also increase progressively from the central layers and plates to the outermost layers and plates. All rubber layers are of equal depth in a direction perpendicular to the plane of Figure 1 along the entire length of each layer as viewed in Figure 1 and the plates are like wise-shaped. The central rubber layers and metal plate are of a square outer profile and accordingly the relatively outer rubber layers and plates are of rectangular outer profile. When the spring is subjected to a combination of shear and compression loadings, as illustrated in Figure 3, the effective area of the spring directly to support compression loads remains substantially unaltered at the cross-sectional area of the centre rubber layers I la and this assists to minimise the bending stresses on the outermost rubber layers and thus improve their fatigue life as compared with a conventional spring having rubber layers and plates all of similar dimensions. It will be further appreciated from Figure 3 that by use of central rubber layers and plates which are shorter than relatively outer layers and plates, all layers and plates are more able to move angularly relative to the end plates than in a conventional spring where all plates and layers are of similar dimensions, and accordingly there results a more uniform distribution of bending stresses between all of the rubber layers so as to assist in improving the fatigue life of the spring. WHAT WE CLAIM IS:
1. Aspring comprising a plurality of layers of rubber or like elastomeric material bonded to and interleaved with a plurality of metal plates wherein the length of the layers of rubber or like elastomeric material as considered in at least one cross-sectional plane extending substantially perpendicular to the plane of said layers and metal plates decreases from each outermost layer in a direction towards the centre layer or layers and the thickness of the centre layer or layers of rubber or like elastomeric material is less than the thickness of the outermost layers.
2. A spring according to claim 1 wherein the length of the layers in said cross-sectional plane decreases uniformly from each outermost layer in a direction towards the centre layer or layers of the spring.
3. A spring according to claim 1 or claim 2 wherein successive layers are positioned centrally relative to one another when viewed in cross-sectional plane.
4. A spring according to any one of the preceding claims wherein the length of the layers of rubber or like elastomeric material as considered in one or more other planes substantially perpendicular to the plane of said layers and metal plates decreases from each outermost layer in a direction towards the centre layer or layers.
5. A spring according to any one of the preceding claims wherein considered in planes parallel to the layers of rubber or like elastomeric material and metal plates a layer and/or a metal plate is apertured.
6. A spring according to claim 5 having
formed therein a hollow cavity.
7. A spring according to claim 6 wherein a passage communicates between the hollow cavity and the outside of the spring.
8. A spring according to claim 6 or claim 7 wherein the hollow cavity is airtight.
9. A spring according to any one of the preceding claims wherein the thickness of the layers of rubber or like elastomeric material increases progressively from the centre layer or layers towards each outermost layer.
10. A spring constructed and arranged substantially as herein described with reference to the accompanying drawing.
GB35898/76A 1976-08-28 1976-08-28 Springs Expired GB1578750A (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
GB35898/76A GB1578750A (en) 1976-08-28 1976-08-28 Springs
CA284,938A CA1070721A (en) 1976-08-28 1977-08-15 Springs
CH1016977A CH612253A5 (en) 1976-08-28 1977-08-18 Spring
IN1298/CAL/77A IN148753B (en) 1976-08-28 1977-08-19
DE19772738168 DE2738168A1 (en) 1976-08-28 1977-08-24 FEATHER
SE7709528A SE7709528L (en) 1976-08-28 1977-08-24 SANDWICH TYPE SPRING DEVICE
FR7725916A FR2363032A1 (en) 1976-08-28 1977-08-25 SPRINGS WITH STACKING OF LAYERS OF RUBBER OR SIMILAR ELASTOMERIC MATERIAL LINKED TO INTERCALED METAL PLATES
HU77DU273A HU173176B (en) 1976-08-28 1977-08-26 PRUZHINA, SOSTAVENNAJA IZ METALLICHESKIKH PLASTIN, ZAKREPLJONNYKH MEZHDU EHLASTICHNYMI SLOJAMI
PL1977200494A PL119454B1 (en) 1976-08-28 1977-08-27 Spring
RO7791477A RO76133A (en) 1976-08-28 1977-08-27 ARC TYPE SANDVIS WITH COATED ROOFS
JP10353077A JPS5329470A (en) 1976-08-28 1977-08-29 Spring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB35898/76A GB1578750A (en) 1976-08-28 1976-08-28 Springs

Publications (1)

Publication Number Publication Date
GB1578750A true GB1578750A (en) 1980-11-12

Family

ID=10382773

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35898/76A Expired GB1578750A (en) 1976-08-28 1976-08-28 Springs

Country Status (11)

Country Link
JP (1) JPS5329470A (en)
CA (1) CA1070721A (en)
CH (1) CH612253A5 (en)
DE (1) DE2738168A1 (en)
FR (1) FR2363032A1 (en)
GB (1) GB1578750A (en)
HU (1) HU173176B (en)
IN (1) IN148753B (en)
PL (1) PL119454B1 (en)
RO (1) RO76133A (en)
SE (1) SE7709528L (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103397666A (en) * 2013-08-13 2013-11-20 东南大学 Rubber support for vibration isolation or vibration reduction
CN105156530A (en) * 2015-09-10 2015-12-16 青岛四方车辆研究所有限公司 Middle-concave type overlapped rubber spring

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4211429A (en) * 1978-04-19 1980-07-08 Howard D U Adjustable suspension assembly
JPS6435134A (en) * 1987-07-31 1989-02-06 Yokohama Rubber Co Ltd Laminate rubber
JPH05141463A (en) * 1991-11-15 1993-06-08 Kajima Corp Laminated rubber and vibration control device for structure using laminated rubber
JP4734913B2 (en) * 2004-12-20 2011-07-27 横浜ゴム株式会社 Seismic isolation rubber laminate
JP2010180936A (en) * 2009-02-04 2010-08-19 Bridgestone Corp Layer structure object for damping device
CN102829115A (en) * 2012-08-28 2012-12-19 中国航空工业集团公司北京航空材料研究院 Damping rubber spring for automobile suspension

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103397666A (en) * 2013-08-13 2013-11-20 东南大学 Rubber support for vibration isolation or vibration reduction
CN105156530A (en) * 2015-09-10 2015-12-16 青岛四方车辆研究所有限公司 Middle-concave type overlapped rubber spring

Also Published As

Publication number Publication date
JPS5329470A (en) 1978-03-18
DE2738168A1 (en) 1978-03-02
PL200494A1 (en) 1978-04-10
IN148753B (en) 1981-06-06
CA1070721A (en) 1980-01-29
RO76133A (en) 1981-03-30
CH612253A5 (en) 1979-07-13
JPS6131331B2 (en) 1986-07-19
PL119454B1 (en) 1982-01-30
FR2363032A1 (en) 1978-03-24
HU173176B (en) 1979-03-28
FR2363032B1 (en) 1980-02-01
SE7709528L (en) 1978-03-01

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years

Effective date: 19970810