FR2556818A1 - Composite assembly capable of being cut in the form of bars - Google Patents
Composite assembly capable of being cut in the form of bars Download PDFInfo
- Publication number
- FR2556818A1 FR2556818A1 FR8320422A FR8320422A FR2556818A1 FR 2556818 A1 FR2556818 A1 FR 2556818A1 FR 8320422 A FR8320422 A FR 8320422A FR 8320422 A FR8320422 A FR 8320422A FR 2556818 A1 FR2556818 A1 FR 2556818A1
- Authority
- FR
- France
- Prior art keywords
- holes
- sheet metal
- bars
- penetrating
- composite assembly
- 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.)
- Withdrawn
Links
- 239000002131 composite material Substances 0.000 title claims description 8
- 239000002184 metal Substances 0.000 claims abstract description 7
- 238000004873 anchoring Methods 0.000 claims abstract description 4
- 230000000149 penetrating effect Effects 0.000 claims abstract 4
- 239000013536 elastomeric material Substances 0.000 claims description 4
- 239000006096 absorbing agent Substances 0.000 abstract description 2
- 229920001971 elastomer Polymers 0.000 abstract description 2
- 239000000806 elastomer Substances 0.000 abstract description 2
- 239000000463 material Substances 0.000 abstract description 2
- 230000035939 shock Effects 0.000 abstract description 2
- 238000000465 moulding Methods 0.000 description 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/06—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of natural rubber or synthetic rubber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- 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
- F16F1/371—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by inserts or auxiliary extension or exterior elements, e.g. for rigidification
- F16F1/3713—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by inserts or auxiliary extension or exterior elements, e.g. for rigidification with external elements passively influencing spring stiffness, e.g. rings or hoops
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/162—Selection of materials
- G10K11/168—Plural layers of different materials, e.g. sandwiches
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/56—Damping, energy absorption
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Mechanical Engineering (AREA)
- Springs (AREA)
- Vibration Dampers (AREA)
- Laminated Bodies (AREA)
Abstract
Description
L'invention a pour objet un ensemble composite susceptible d'être débite sous forme de barres. The subject of the invention is a composite assembly capable of being fed in the form of bars.
L'ensemble c:oesite selon l'invention est réalisé à partir d'une tôle perforée présentant des moyens d'ancrage et de retenue susceptibles de coopérer avec une bande rapportée par moulage en elastomere par exemple, ladite tôle présentant des parties lisses autorisant une fixation aisée. The assembly c: oesite according to the invention is made from a perforated sheet having anchoring and retaining means capable of cooperating with a strip attached by elastomer molding for example, said sheet having smooth parts allowing a easy fixing.
La figure 1 est une vue en perspective d'un élément composite selon l'invention. FIG. 1 is a perspective view of a composite element according to the invention.
La figure 2 est une vue en coupe transversale selon la figure 1t . Figure 2 is a cross-sectional view according to Figure 1t.
La figure 3 est une vue d'une barre découpée à partir de 1 'element composite. Figure 3 is a view of a bar cut from the composite member.
Cet éLément composite comprend une plaque en tôle (1) présentant une pluralité de trous (11) régulièrement ou non répartis sur la surface de ladite plaque, ceux-ci étant disposes tout en laissant vierges les extrémités longitudinales de la plaque définissant ainsi deux bandes opposées lisses (12), Les trous presen 3 tant sur la face avant de la plaque en tôle des évasements (13) et sur la face arrière des contre dépouilles (14) apparentes servant de moyens d'ancrage et de retenue lors du moulage de la matière élastomère (2)en forme de bloc, sur la face arrière de la tôle. This composite element comprises a sheet metal plate (1) having a plurality of holes (11) regularly or not distributed on the surface of said plate, these being arranged while leaving the longitudinal ends of the plate blank, thus defining two opposite bands. smooth (12), The holes present 3 both on the front face of the sheet metal plate of the flares (13) and on the rear face of the exposed undercuts (14) serving as anchoring and retaining means during the molding of the elastomeric material (2) in the form of a block, on the rear face of the sheet.
Comme illustré figure 2, la matière élastomère pénètre dans les trous (11) en venant affleurer la face avant de la tôle, les contre dépailles assurant la fonction inserts dans ladite matière contribuant à la rigidité de l'ensemble. L'ensemble composite peut etre découpé selon les besoins dans sa longueur sous forme de barres ainsi qu'illustré figure 3. As illustrated in FIG. 2, the elastomeric material penetrates into the holes (11), coming flush with the front face of the sheet, the back pieces ensuring the function of inserts in said material contributing to the rigidity of the assembly. The composite assembly can be cut as needed in its length in the form of bars as shown in Figure 3.
Les bandes lisses (12) apparentes sur les extrémités des barres permettent une fixation aisée lors du positionnement desdites barres sur des éléments d'appui, de liaison ou autres. The smooth bands (12) visible on the ends of the bars allow easy fixing during the positioning of said bars on support, connection or other elements.
On souligne les avantages de cet ensemble comme élément anti-bruit. On peut l'utiliser comme butée, ressort, amortisseurs, patins, élément de chaîne de manutention à débiter ceci d'une manière non limitative. The advantages of this set as an anti-noise element are emphasized. It can be used as a stopper, spring, shock absorbers, pads, handling chain element to deliver this in a non-limiting manner.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8320422A FR2556818A1 (en) | 1983-12-15 | 1983-12-15 | Composite assembly capable of being cut in the form of bars |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8320422A FR2556818A1 (en) | 1983-12-15 | 1983-12-15 | Composite assembly capable of being cut in the form of bars |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2556818A1 true FR2556818A1 (en) | 1985-06-21 |
Family
ID=9295369
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8320422A Withdrawn FR2556818A1 (en) | 1983-12-15 | 1983-12-15 | Composite assembly capable of being cut in the form of bars |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2556818A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0418735A1 (en) * | 1989-09-21 | 1991-03-27 | VSR ENGINEERING GmbH | Shock-absorbing support for sliding belts |
CN102878419A (en) * | 2012-10-12 | 2013-01-16 | 无锡市张泾宇钢机械厂 | Panel of mining mechanical operation platform |
CN102997030A (en) * | 2012-11-29 | 2013-03-27 | 庄河市天成机械有限公司 | Lower supporting board with cold punched special-shaped square holes |
-
1983
- 1983-12-15 FR FR8320422A patent/FR2556818A1/en not_active Withdrawn
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0418735A1 (en) * | 1989-09-21 | 1991-03-27 | VSR ENGINEERING GmbH | Shock-absorbing support for sliding belts |
CN102878419A (en) * | 2012-10-12 | 2013-01-16 | 无锡市张泾宇钢机械厂 | Panel of mining mechanical operation platform |
CN102997030A (en) * | 2012-11-29 | 2013-03-27 | 庄河市天成机械有限公司 | Lower supporting board with cold punched special-shaped square holes |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |