REFLECTIVE INSULATION SYSTEM

Abstract

Insulation system for thermoacoustic insulation of a component to be insulated, such as an exhaust gas component, comprising a fiber molded part having a surface facing away from the component to be insulated, where the surface facing away is at least in part jacketed with a cladding, and having an insulation surface facing the component to be insulated, where the fiber molded part is applied to the component to be insulated such that at least one cavity is formed between a portion of the insulation surface of the fiber molded part and the component to be insulated.

Claims

1. An insulation system for thermoacoustic insulation of a component to be insulated, such as an exhaust gas component, comprising: a fiber molded part having a surface facing away from the component to be insulated, where the surface facing away is at least in part jacketed with a cladding, and having an insulation surface facing the component to be insulated, where said fiber molded part is applied to the component to be insulated such that at least one cavity is formed between a portion of the insulation surface of said fiber molded part and the component to be insulated.

2. The insulation system according to claim 1, wherein the insulation surface of said fiber molded part is coated with colored pigments which have a TSR, total solar reflectance, value of at least 65%, where the percentage of the colored pigments relative to a total mass of said fiber molded part amounts to between 1-5%, preferably between 1.5-3%.

3. The insulation system according to claim 1, wherein an inner liner is inserted in between the insulation surface of said fiber molded part and the component to be insulated.

4. The insulation system according to claim 1 wherein, the inner liner comprises a metal inner liner.

5. The insulation system according to claim 1, wherein the cladding comprises a metallic cladding or duroplastic-thermoplastic plastic or elastomeric plastic.

6. The insulation system according to claim 1, wherein a predefined proportion of the insulation surface facing the component to be insulated of said fiber molded part is in contact with the component to be insulated, where the predefined proportion amounts to at least 10% and at most 90%.

7. The insulation system according to claim 6, wherein the predefined proportion amounts to at least 25% to at most 55%.

8. The insulation system according to claim 1, wherein the insulation surface facing the component to be insulated comprises one or more predefined indentations.

9. The insulation system according to claim 8, where the indentations are semi-spherical and/or semi-cylindrical indentations so that the cavity is formed to be semi-spherical and/or semi-cylindrical in shape.

10. An exhaust gas component having an insulation arranged at least in part on the component, wherein the insulation is configured as an insulation system according to claim 1.

11. A silencer comprising at least one exhaust gas component according to claim 10.

12. A method for thermoacoustic insulation of an exhaust gas component, said method comprising the steps of: providing a fiber molded part having a surface facing away from the component to be insulated, where the surface facing away is at least in part jacketed with a cladding and having an insulation surface facing the exhaust gas component; and applying the fiber molded part to the exhaust gas component such that at least one cavity is formed between a portion of the insulation surface of said fiber molded part and the component to be insulated.

13. A method according to claim 12, wherein the insulation surface of the fiber molded part is coated with colored pigments which have a TSR, total solar reflectance, value of at least 65%, where a percentage of the colored pigments relative to a total mass of the fiber molded part amounts to between 1-5%.

14. A method according to claim 13, wherein the percentage of the colored pigments relative to the total mass of the fiber molded part amounts to between 1.5-3%.

15. A method according to claim 12, wherein an inner liner is inserted between the insulation surface of the fiber molded part and the component to be insulated.

16. A method according to claim 15, wherein the inner liner comprises a metal inner liner.

17. A method according to claim 12, wherein the fiber molded part further comprises a surface facing away from the component to be insulated, where the surface facing away is at least in part jacketed with a cladding, wherein the cladding is a metal cladding or comprises duroplastic-thermoplastic plastic or elastomeric plastic.

18. A method according to claim 12, wherein a predefined proportion of the insulation surface of the fiber molded part is in contact with the component to be insulated, where the predefined proportion amounts to at least 10% and at most 90%.

19. A method according to claim 18, wherein where the predefined proportion amounts to at least 25% to at most 55%.

20. A method according to claim 12, wherein the insulation surface facing the component to be insulated comprises one or more predefined indentations, where the indentations are preferably formed semi-spherical or semi-cylindrical in shape.

21. An insulation system for thermoacoustic insulation of a component comprising: a component; a fiber molded part having an insulation surface facing said component and a surface facing away from said component, said fiber molded part contacting said component at contact points forming a closed cavity between said component and the insulation surface; and a cladding placed on said fiber molded part over the surface facing away from said component, whereby convection in the closed cavity is substantially reduced improving insulation of the component.

22. The insulation system as in claim 21 wherein: the contact points in contact with said component have a total surface area of a proportion of the insulation surface of at least 10% and at most 90%.

23. The insulation system as in claim 21 wherein: said cladding is movable towards and away from the surface facing away from said component.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0044] FIG. 1 is a schematic view of an insulation system

[0045] FIGS. 2A-B are schematic views of an insulation systems with an inner liner.

[0046] FIG. 3 is a schematic view of a development of an insulation system of FIGS. 1-2B with exchangeable cladding.

[0047] FIG. 4 is a schematic view of an embodiment of an insulation system without a component to be insulated.

[0048] FIG. 5 is a schematic view of an embodiment of an insulation system.

DETAILED DESCRIPTION OF THE INVENTION

[0049] FIG. 1 shows a schematic view of an insulation system 1 for thermoacoustic insulation of a component 200 to be insulated. Component 200 to be insulated can be, for example, an exhaust gas component. Insulation system 1 in FIG. 1 comprises a fiber molded part 12 which comprises insulating material, for example, fibers or non-woven fabric. Fiber molded part 12 has a side or surface facing away from component 200 to be insulated and designated with reference numeral 12.1. Surface 12.1 is in FIG. 1 jacketed with cladding 14. In the schematic illustration in FIG. 1, cladding 14 practically rests on surface 12.1.

[0050] Fiber molded part 12 further has a side or surface 12.2 facing the component to be insulated. Surface 12.2 is an insulation surface. FIG. 1 shows a highly simplified sectional drawing. A component 200 to be insulated is there insulated by an insulation system 1 with a fiber molded part 12. Fiber molded part 12 is applied to component 200 to be insulated such that it contacts component 200 to be insulated with only a portion of insulation surface 12.2. Contacting insulation surface 12.2 is there performed such that a cavity 16 is formed. Cavity 16 can there also be understood to be a chamber. Cavity 16 is entirely enclosed or defined by insulation surface 12.2 and component 200 to be insulated, i.e. is formed therebetween. Cavity 16 is typically filled with air and can also be regarded as being an air chamber. It is understood that several cavities of a similar nature can be formed and that FIG. 1 illustrates only one of the simplest options and shows only one cavity.

[0051] Cavity 16 or several separate cavities each form a closed storage system. Cavity 16 can therefore enclose air. Air in turn has a low heat capacity and therefore according to equation (3) can absorb only a small amount of heat of the system to be insulated. Virtually no convection occurs in cavity 16. This leaves nearly all the heat energy in system 200 to be insulated.

[0052] In the example shown in FIG. 1, insulation surface 12.2 is in contact with component 200 only in the region of points A and B. This is therefore a predefined portion of insulation surface 12.2 of the fiber molded part in region A and B where component 200 to be insulated is in contact with insulation surface 12.2. The predefined portion can typically amount to at least 10%. A typical value within the meaning of an upper limit can amount to 90% of the insulation surface. Other values can also be possible. It can below 10% occur that problems with instability arise. Above 90%, the advantages over a fully contacted insulation surface rapidly disappear. However, other values are possible, in particular a value between a minimum of 25% up to a maximum of 55% is possible.

[0053] Only where insulation surface 12 is in contact with component 200, i.e. at the contact surfaces in region A and B, can additional heat absorption of fiber molded part 12, i.e. the insulating material take place. However, since the contact surfaces are small and limited, only very little absorption of heat occurs via the contact surface. A further advantage is that entire fiber molded part 12 comprises insulating material. Cavity 16 is therefore in the region of fiber molded part 12 enclosed by insulating material. This insulating material can again ensure that the surface temperature can at side 12.1 opposite to the component to be insulated be significantly reduced, so that the surrounding can be protected by insulation system 1. Almost all the heat energy can remain within the system to be insulated and the surrounding components are well protected.

[0054] Insulation surface 12.2 of fiber molded part 12 can additionally be coated with colored pigments, for example, a polishing rutile based on chromium/antimony/titanium, which have a TSR, total solar reflectance, value of at least 65%, where the percentage of colored pigments relative to the total mass of the fiber molded part amounts to between 1-5%, preferably between 1.5-3%. Possible energy output by thermal radiation can therefore additionally be counteracted and the energy can be retained even better within the system to be insulated

[0055] FIG. 2A shows a similar schematic sectional view of an insulation system 1 as shown in FIG. 1. The same elements are given the same reference numerals and shall presently not be explained again. In addition, FIG. 2A shows an inner liner 18 which is provided between component 200 to be insulated and insulation surface 12.2 of the fiber molded part. Inner liner is typically made of metal, such as stainless steel with material number WNr. 1.4541 Inner liner 18 is shown in FIG. 2A such that it rests on component 200 and thereby forms a kind of additional layer on component 200. It is understood, however, that inner liner 18 can also only be provided substantially in region A and B, i.e. where in FIG. 1 insulation surface 12.2 is in contact with component 200. Inner liner 18 can in these contact regions A and B be provided between component 200 and the insulation surface. It is understood that the inner liner does not change the size of the predefined portion of insulation surface 12.2 of the fiber molded part in region A and B explained in FIG. 1 where component 200 to be insulated is in contact with insulation surface 12.2. Inner liner 18 can on the one hand serve to provide additional protection for the insulating material of fiber molded part 12 against mechanical and thermal loads. On the other hand, fiber molded part 12 can easily be mounted or replaced so that greater processing and maintenance flexibility can thereby be provided.

[0056] FIG. 2B shows a variant of the embodiment shown in FIG. 2A. The material properties of inner liner 18 can there be the same. The same reference numerals are used in FIG. 2B. FIG. 2B shows that inner liner 18 can be also provided such that it can assume the shape of the side of the insulating body, i.e. fiber molded part 12, facing the exhaust gas component. Inner liner 18 in FIG. 2B bears against the side with insulation surface 12.2. A preferably metal inner liner 18, as shown, for example, in FIGS. 2A and 2B, can be used to provide a simple manner of removing and remounting the fiber molded part. In addition, a preferably metal inner liner has a protective function for the insulating body, i.e. the fiber molded part.

[0057] FIG. 3 shows a further development of FIG. 2A. The same elements are there designated by same reference numerals. Purely by way of example, FIG. 3 is based on the embodiment shown in FIG. 2A. It is understood, however, that the embodiment shown in FIG. 3 and described below can be based on any of the embodiments described in the context of FIG. 2A and FIG. 2B. Cladding 14 can in FIG. 3 comprise a metal cladding. It is likewise possible to provide a cladding made of duroplastic-thermoplastic plastic and/or elastomeric plastic. Cladding 14 is in FIG. 3 shown to be removable. Though the entire cladding 14 is shown in a simple manner as being removable, it is understood that a multi-part cladding could also provided of which only parts are removable or to be opened and closed, such as with a flap mechanism (presently not shown). Cladding 14 can in FIG. 3 be slid open, for example, in the direction of the double arrow P onto fiber molded part 12 and drawn off from the latter, respectively. Cladding 14 is thereby in this development exchangeable. In the embodiment with a fitting metal cladding, the cladding can be provided such that the outer shell 14 can either completely or in part be closed or opened, whereby an outer shell 14 is provides with the option of a variable opening or closure of the outer shell, i.e. of the cladding. The insulation system is thereby provided with the option to quickly reach the operating temperature corresponding to the exhaust system when shell 14 is closed, and with the open variant cause cooling of component 200 by convection, i.e. to selective switch convection on or off.

[0058] FIG. 4 shows a schematic view of another embodiment or development of an insulation system 21 according to one or more of FIGS. 1-3. A component to be insulated is not shown in FIG. 4, but only the insulation system 21. Insulation system 21 in FIG. 4 again, as already shown in FIGS. 1-3, comprises a fiber molded part 22 with an outwardly facing surface 22.1. The cylindrical shape of fiber molded part 22 suggests that surface 22.1 represents a side facing away from a component to be insulated. Fiber molded part 22 comprises indentations 26H on the inner side of the cylinder. Although eighteen indentations are in FIG. 4 drawn in, it is understood that the number of indentations can be larger or smaller, depending on the present applications. Indentations 26H are in FIG. 4 by way of example formed to be semi-spherical and/or semi-cylindrical in shape. Semi-spherical indentations have the advantage that they can be realized in a simpler manner in terms of production engineering/tool engineering. However, it is understood that other bodies or partial bodies with suitable geometric shapes can be selected, so that one or more cavities are formed. For example, indentations 26H can also have a kind of honeycomb structure. Indentations 26H are provided in insulation surface 22.2. It is understood that the example shown in FIG. 4 and below in FIG. 5 shows a cylindrical symmetry or a tubular symmetry, but other body shapes can exist that have less symmetry.

[0059] Insulation system 21 of FIG. 4 is in FIG. 5 shown for insulating a component 202 to be insulated, such as an exhaust gas component. Component 202 can correspond to component 200 of FIGS. 1-3. Insulation surface 22.2 in FIG. 4 is composed of many small partial surfaces defining indentations 26H or being located between the respective indentations, respectively. This insulation surface 22.2, i.e. the many small partial surfaces are in contact with component 202, so that as many cavities 26 arise as indentations 26H. The sum of all smaller partial surfaces there again results in a predefined proportion of insulation surface 22.2 of the fiber molded part, where component 202 to be insulated is in contact with insulation surface 22.2. The predefined proportion is again typically at least 10% and a typical value within the meaning of an upper limit can amount to approximately 90% of the insulation surface. Other values are also possible, in particular a value between a minimum of 25% up to a maximum of 55%.

[0060] FIG. 5 further shows an outer cladding 24 which encloses surface 22.1 on the side facing away from component 202 to be insulated.

[0061] Air chambers 26H introduced into the insulation system achieve the desired insulating effect, so that a larger portion of the energy remains in the exhaust gas and virtually does not dissipate outwards into the surrounding. Virtually no convective heat transfer of the exhaust gas component occurs into the surrounding. In addition to the thermal properties, improved acoustic insulation also arises. For example, sound absorption arises in the range of 6.3 kHz at about 90%.