The present application relates generally to the field of airbag modules. In particular, the application relates to the packaging of an airbag in a module.
One disclosed embodiment relates to an airbag module with an airbag packed in foil under vacuum, including a gas generator and a covering cap. The foil includes at least one predetermined tearing point. Additionally, the foil is connected or can be at least partially connected to the covering cap in sections that lie next to the tear-open edges of the covering cap. Further, the connection can be configured to take place only upon deployment of the airbag.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only, and are not restrictive of the invention as claimed.
These and other features, aspects, and advantages of the present invention will become apparent from the following description, appended claims, and the accompanying exemplary embodiments shown in the drawings, which are briefly described below.
a-c shows tear-open geometries of the foil and of the associated covering cap, according to an exemplary embodiment.
Airbags may be packed in airbag modules in a folded state in foil under vacuum. These folded packages are subsequently inserted into the airbag modules. In certain situations it may be possible for a folded package to tear open, in the event of a crash, in an undefined manner in terms of force and geometrical profile. As described further below, the disclosed embodiments of an airbag module are configured so that the foil tears and the airbag deploys in a defined and predictable manner.
According to a disclosed embodiment, an airbag module includes an airbag packed in foil under vacuum, with a gas generator and a covering cap. The foil includes at least one predetermined tearing point. Further, the foil is connected to or can be at least partially connected to the covering cap in sections that lie next to the tear-open edges of the covering cap.
In the case of airbag modules, predetermined tearing points in the covering caps are known. The predetermined tearing points have been inserted in the form of material weakenings during the production of the covering caps. Additionally, it is known from DE 199 07 742 A1, which is herein incorporated by reference in its entirety, to only produce material weakening in the event of a crash by inserting a heating wire into the covering cap at the designated tear-open points of the covering cap. Thus, in the basic state, the covering cap includes a continuous wall without gaps or visible edge notchings. The predetermined tearing points have previously been provided only in the covering caps in airbag modules. Conventionally, the tearing points have a thickness in the millimeter range. No conventional predetermined tearing points have been provided in the foils, which are only a few tenths of a millimeter thick, for the packing of the airbag. The presence of the predetermined tearing point in the event of a crash means that it does not have to be provided beforehand.
The predetermined tearing point is preferably provided in the region of the tear-open edges of the covering cap. Thus, during tearing open of the covering cap, the tearing edges of the foil lie approximately in the region of the tear-open edges of the covering cap.
The predetermined tearing point of the foil can differ in design. The first basic option is for the foil to already have a predetermined tearing point before the airbag is packed. Therefore, a tear-open seam or an impressed contour may be provided as the predetermined tearing point. It is advantageous for the predetermined tearing point to be provided in one layer when a multi-layer foil is used. More particularly, the predetermined tearing point should be configured on the outer layer that faces the covering cap.
According to an exemplary embodiment, the foil is connected at least partially to the covering cap in sections that lie next to the tear-open edges of the covering cap. Thus, it is possible for an all-over, linear or spot-shaped connection to be provided. As a result of the aforementioned connection, movement of the covering cap and of the foil relative to each other can be prevented. Therefore, during opening, stress can be concentrated on the relatively narrow regions of the foil below the tear-open edges of the covering cap. Thus, a rapid and defined tearing open of the foil can occur.
The second basic design of the predetermined tearing point is wherein the foil has a predetermined tearing point only upon or directly before firing of the gas generator.
According to an exemplary embodiment, the foil includes a mechanically produced predetermined tearing point. This can be achieved, for example, by sharp edges on the inside of the covering cap. When the airbag is deployed, the foil is pressed against the sharp edges. As a result, the foil is perforated at these points, i.e. is locally weakened.
According to a further exemplary embodiment, the foil includes a thermally produced predetermined tearing point. At least one heating wire can be provided to produce the predetermined tearing point. According to a preferred embodiment, the heating wire can be arranged between the covering cap and the foil.
According to a yet further exemplary embodiment, the foil can be at least partially connected to the covering cap in sections that lie next to the tear-open edges of the covering cap. For example, the inside of the covering cap can include adhesive agents that the foil can be pressed against when the airbag is deployed. Double-sided adhesive tape or structural elements with a high coefficient of friction can be included as the adhesive agents. However, a corresponding structure may also be molded onto the elements of the covering cap.
a to 3c illustrate how the predetermined breaking points can run in the foil, according to an exemplary embodiment. The foil section lying below the covering cap is illustrated. The predetermined breaking points of the covering cap include the same profile. In the embodiment of
According to the exemplary embodiment of
According to the exemplary embodiment of
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The embodiments of
The priority application, German Patent Application No. 20 2006 005 319.0, filed Mar. 28, 2006, including the specification, drawings, claims and abstract, is incorporated herein by reference in its entirety.
Given the disclosure of the application, one versed in the art would appreciate that there may be other embodiments and modifications within the scope and spirit of the application. Accordingly, all modifications attainable by present application are to be included as further embodiments of the present application. The scope of the present application is to be defined as set forth in the following claims.
Number | Date | Country | Kind |
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20 2006 005 319.0 | Mar 2006 | DE | national |
This application is a Continuation of International Application No. PCT/EP2007/002707, filed Mar. 22, 2007, which was published in German as WO 2007/112887 and is incorporated herein by reference in its entirety.
Number | Date | Country | |
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Parent | PCT/EP2007/002707 | Mar 2007 | US |
Child | 12285017 | US |