GB1578863A - Shock-absorbing support comprising a resilient block with cavities therein - Google Patents
Shock-absorbing support comprising a resilient block with cavities therein Download PDFInfo
- Publication number
- GB1578863A GB1578863A GB1893577A GB1893577A GB1578863A GB 1578863 A GB1578863 A GB 1578863A GB 1893577 A GB1893577 A GB 1893577A GB 1893577 A GB1893577 A GB 1893577A GB 1578863 A GB1578863 A GB 1578863A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cavities
- block
- resilient support
- fixing element
- plates
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G99/00—Subject matter not provided for in other groups of this subclass
- B60G99/004—Other suspension arrangements with rubber springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P7/00—Securing or covering of load on vehicles
- B60P7/06—Securing of load
- B60P7/16—Protecting against shocks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D33/00—Superstructures for load-carrying vehicles
- B62D33/06—Drivers' cabs
- B62D33/0604—Cabs insulated against vibrations or noise, e.g. with elastic suspension
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/373—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape
- F16F1/377—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape having holes or openings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/42—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing
- F16F1/52—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses
- F16F1/54—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses loaded in compression and shear
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
- F16F2236/12—Mode of stressing of basic spring or damper elements or devices incorporating such elements loaded in combined stresses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
- F16F2236/12—Mode of stressing of basic spring or damper elements or devices incorporating such elements loaded in combined stresses
- F16F2236/123—Mode of stressing of basic spring or damper elements or devices incorporating such elements loaded in combined stresses loaded in compression and shear
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Transportation (AREA)
- Health & Medical Sciences (AREA)
- Child & Adolescent Psychology (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Vibration Prevention Devices (AREA)
- Springs (AREA)
- Road Paving Structures (AREA)
- Vibration Dampers (AREA)
Description
(54) SHOCK-ABSORBING SUPPORT COMPRISING A RESILIENT BLOCK WITH
CAVITIES THEREIN
(71) We, PAULSTRA, a Body Corporate organised and existing under the Laws of
France, of 61 Avenue Marius-Aufan, 92305- Levallois-Perret, France, 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:
The present invention relates to a resilient support for interposition between two structures, one of which must be protected against shocks and vibrations which are liable to occur in several directions, for example between the body or engine of a vehicle and its chassis or between a freight container and the vehicle, aeroplane or ship on which it is carried.
For such purposes it is known to use blocks of elastomer having cavities therein.
In accordance with the present invention there is provided a resilient support for interposition between two structures comprising at least one block of elastomer bonded on the one hand to a fixing element for attachment to one of the structures and on the other hand to three orthogonal metal plates for attachment to the other structure, the block having respective cavities disposed between the fixing element and each of the orthogonal plates.
The cavities allow the block of elastomer, when subjected to shocks and vibrations, to work at first by flexing and shearing and thereafter, if the cavities are closed, in compression.
Each of the cavities is preferably defined between surfaces parallel to the respective plate and may open onto a free face of the block.
In a preferred form the block is a rectangular body with the faces which are bonded to the said plates enlarged by means of projections from the rectangular body, the cavities being at least partially with the said projections. This construction enables the dimensions of the cavities to be increased.
The invention will now be described in more detail with the aid of examples illustrated in the accompanying drawings, in which:
Figure 1 is a perspective view of a resilient support in accordance with the invention,
Figure 2 is a similar view of a second form of resilient support in accordance with the invention and
Figures 3 and 4 are sections in two orthogonal planes and Figure 5 is a side elevation of a third form of resilient support in accordance with the invention.
The resilient support shown in Figure 1, which is intended to absorb shocks or vibrations in three orthogonal directions, comprises a rigid metallic member 1 in the form of a triple dihedron consisting of three plates, orthogonal to one another, which in this instance are integral with one another but, as shown in Figures 2 to 5, may be separate. A resilient block 2 in the form of a cube has three of its sides bonded respectively to the three plates of the metallic member 1, the bonding being effected by any of the conventional techniques.
For each of three perpendicular directions in which shocks may occur at least one cavity 3 is formed in the block 2. Each cavity 3 lies adjacent and generally parallel to one of the plates of the member 1 to take up shocks in a direction perpendicular to that plate. Each cavity opens at one end on a free face of the block 2.
Embedded in the block 2 there is a metallic fixing element 4 with a threaded bore 5.
The unit or assembly to be supported, such as a motor or container, can be attached to the fixing element 4 by means of a screw engaged in the threaded bore 5. The member 1 is itself provided with means for fixing it to a chassis or other assembly intended to support the load, such means comprising holes 6 for the passage of pins or the like and/or of projecting screws or pins 7 as shown in Figures 3 to 5.
In such a resilient support, the elastomer, instead of working only by compression, as would be the case if the resilient block 2 was solid, works, at least at the beginning of the reception of shocks, at one and the same time by shearing and by flexion, this flexion being exercised on the arms of elastomer adjacent to the cavities 3. It is only at the end of the process that the rest of the shock-energy is absorbed solely by compression, when the cavity concerned, corresponding to the direction of the shock, has just closed.
To sum up, the shocks are absorbed in the three directions, with substantially the same rigidity in the three axes, but with a good initial flexibility, since the shock is first absorbed by deformations in shearing and flexion, whereas it is only at the end of the process that the effect of check by compression occurs.
As is evident, the symmetry represented in the drawing is not obligatory and the form especially of the cavities could be different in various directions, if differentiation of the respective rigidities were desired.
Moreover, the cavities can be multiple in at least one or in each of the directions concerned.
Figure 1 only explains the principle of the invention, but it is possible to imagine numerous modes of realisation arising from this principle.
Thus it is that it can be desirable to increase the dimensions of the cavities, for which eventuali.y there is provided, as represented in Figure 2, an enlargement of the resilient block 2, at the side of the base connecting it to the metal support 1.
This enlargement can occur for example: -either in the direction of the width d
of the said cavities, as Figure 2 supposes,
which allows the increasing of this width, -or in the direction of their length p, -or in any other way.
As illustrated in Figures 3 to 5 the fixing element 4 is a rectangular metal block which is covered on five sides by a layer of elastomer forming part of the block 2, the bore 5 opening onto the remaining side of the metal block. The fixing element 4 is offset from the regions of the block 2 which are bonded to the plates 1 and the cavities 3, which lie between the fixing element 4 and the plates 1 are therefore inclined, as seen in cross-section, to the faces of the mcmbers 1 and 4.
This solution, which utilises a lesser volume of elastomer than that in the preceding solutions, will be suitable for applications evidencing less shock-energies.
In any case, the dimensions and shapes of the cavities (in oval section, parallelepipedic, trapezoidal or others) will be determined as a function of the rigidities to be obtained and, contingently, of the nature of the shocks to be filtered out.
These cavities do not have to be unique in direction and constitute a network of superposed and/or adjacent cavities.
WHAT WE CLAIM IS:
1. A resilient support for interposition between two structures comprising at least one block of elastomer bonded on the one hand to a fixing element for attachment to one of the structures and on the other hand to three orthogonal metal plates for attachment to the other structure, the block having respective cavities disposed between the fixing element and each of the orthogonal plates.
2. A resilient support as claimed in claim 1 in which each of the cavities is defined between surfaces parallel to the respective plate.
3. A resilient support as claimed in claim 1 or 2 in which each of the cavities opens onto a free face of the block.
4. A resilient support as claimed in any of claims 1 to 3 in which the plates are integral with one another.
5. A resilient support as claimed in any one of the preceding claims in which the block is a rectangular body with the faces which are bonded to the said plates enlarged by means of projections from the rectangular body, the cavities being at least partially within the said projections.
6. A resilient support as claimed in any of the preceding claims in which the fixing element is embedded in the block.
7. A resilient support as claimed in any of the preceding claims in which the fixing element is a metallic element formed with a screw-threaded socket.
8. A resilient support substantially as described with reference to Figure 1, Figure 2, or Figures 3 to 5 of the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (8)
1. A resilient support for interposition between two structures comprising at least one block of elastomer bonded on the one hand to a fixing element for attachment to one of the structures and on the other hand to three orthogonal metal plates for attachment to the other structure, the block having respective cavities disposed between the fixing element and each of the orthogonal plates.
2. A resilient support as claimed in claim 1 in which each of the cavities is defined between surfaces parallel to the respective plate.
3. A resilient support as claimed in claim 1 or 2 in which each of the cavities opens onto a free face of the block.
4. A resilient support as claimed in any of claims 1 to 3 in which the plates are integral with one another.
5. A resilient support as claimed in any one of the preceding claims in which the block is a rectangular body with the faces which are bonded to the said plates enlarged by means of projections from the rectangular body, the cavities being at least partially within the said projections.
6. A resilient support as claimed in any of the preceding claims in which the fixing element is embedded in the block.
7. A resilient support as claimed in any of the preceding claims in which the fixing element is a metallic element formed with a screw-threaded socket.
8. A resilient support substantially as described with reference to Figure 1, Figure 2, or Figures 3 to 5 of the accompanying drawings.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7613618A FR2350514A1 (en) | 1976-05-06 | 1976-05-06 | Shock and vibration protective mounting - has slots in elastomeric block to give required stiffness in each direction (NL 8.11.77) |
FR7707019A FR2383359A2 (en) | 1977-03-09 | 1977-03-09 | Shock and vibration protective mounting - has slots in elastomeric block to give required stiffness in each direction (NL 8.11.77) |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1578863A true GB1578863A (en) | 1980-11-12 |
Family
ID=26219433
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1893577A Expired GB1578863A (en) | 1976-05-06 | 1977-05-05 | Shock-absorbing support comprising a resilient block with cavities therein |
GB858779A Expired GB1578864A (en) | 1976-05-06 | 1977-05-05 | Resilient support comprising a shock-absorbing block with a cavity therein |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB858779A Expired GB1578864A (en) | 1976-05-06 | 1977-05-05 | Resilient support comprising a shock-absorbing block with a cavity therein |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE2719925C2 (en) |
GB (2) | GB1578863A (en) |
IT (1) | IT1081409B (en) |
NL (1) | NL185302C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8491241B2 (en) | 2009-02-27 | 2013-07-23 | Airbus Operations Gmbh | Device for reducing loads on latches and loads on cargo containers |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60152852U (en) * | 1984-03-21 | 1985-10-11 | 株式会社共立 | Vibration isolator |
DE9000665U1 (en) * | 1989-11-07 | 1990-05-10 | Fahrzeugbau Langendorf GmbH & Co KG, 4355 Waltrop | Road transport vehicle with an internal loading space for a transport frame with a load inclined inwards on both sides, preferably consisting of upright glass panes or glass pane packages |
GB9809996D0 (en) | 1998-05-12 | 1998-07-08 | Dunlop Ltd | Elastomeric mounting |
US20050077129A1 (en) * | 2003-10-06 | 2005-04-14 | Joel Sloan | Multi-axis shock and vibration relay isolator |
DE102012103036A1 (en) | 2012-04-10 | 2013-10-10 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Housing, especially against detonation protected vehicle housing |
ITRM20130481A1 (en) * | 2013-08-23 | 2015-02-24 | Andrea Dipanati | ANTIVIBRATION MAGNETIC SUPPORT FOR OUTDOOR UNITS OF AIR-CONDITIONERS. |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3072393A (en) * | 1961-08-11 | 1963-01-08 | Sperry Rand Corp | Vibration and shock mount assembly |
FR1335575A (en) * | 1962-07-09 | 1963-08-23 | Assembly incorporating an anti-vibration device | |
HU166596B (en) * | 1970-09-08 | 1975-04-28 |
-
1977
- 1977-05-04 NL NL7704901A patent/NL185302C/en not_active IP Right Cessation
- 1977-05-04 DE DE19772719925 patent/DE2719925C2/en not_active Expired
- 1977-05-05 GB GB1893577A patent/GB1578863A/en not_active Expired
- 1977-05-05 GB GB858779A patent/GB1578864A/en not_active Expired
- 1977-05-05 IT IT943477A patent/IT1081409B/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8491241B2 (en) | 2009-02-27 | 2013-07-23 | Airbus Operations Gmbh | Device for reducing loads on latches and loads on cargo containers |
Also Published As
Publication number | Publication date |
---|---|
NL185302B (en) | 1989-10-02 |
DE2719925A1 (en) | 1977-11-17 |
NL185302C (en) | 1990-03-01 |
IT1081409B (en) | 1985-05-21 |
NL7704901A (en) | 1977-11-08 |
DE2719925C2 (en) | 1983-08-25 |
GB1578864A (en) | 1980-11-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PE20 | Patent expired after termination of 20 years |
Effective date: 19970504 |