The present invention relates generally to the field of automotive protective systems. More specifically, the present invention relates to inflators and airbag systems.
Understanding that drawings depict only typical embodiments of the invention and are not therefore to be considered to be limiting of its scope, the invention will be described and explained with additional specificity and detail through the use of the accompanying drawings in which:
Described below are embodiments of an inflation apparatus for airbag systems. Generally, in the embodiment shown in the accompanying figures the inflator includes two gas chambers containing pressurized gas. A first gas port is positioned to be in fluid communication with the first gas chamber and a second gas port is positioned to be in fluid communication with the second gas chamber. A third gas port, otherwise referred to as an exit gas port, is positioned to be in fluid communication, directly or indirectly, with an inflatable airbag. An initiator is positioned and configured to rupture a burst disk that temporarily prevents fluid communication through the exit gas port.
Upon deployment of the initiator and accompanying rupturing of the burst disk, the pressurized gas from the first and second chambers passes through the first and second gas ports, respectively, after which it passes through the exit gas port and ultimately into the inflatable airbag. The inflator is configured to allow a greater flow rate of gas through the first gas port than through the second gas port. In this manner, the airbag may be primarily inflated via gas from one gas chamber, after which the airbag may be substantially maintained in an inflated state for a predetermined period of time primarily via gas from the other gas chamber. Allowing a greater volume of gas to pass through one of the chamber gas ports may be achieved in a number of ways.
For instance, in one embodiment the higher flow rate may be achieved by making the first gas port larger than the second gas port. In another embodiment, the higher flow rate through the first gas port may be achieved by isolating the chambers and storing gas at a higher pressure in the first chamber than the second chamber. In still another embodiment, the first gas chamber may include a heater. In this embodiment, the higher flow rate through the first gas port may be achieved by increasing the gas pressure in the first gas chamber with the heater.
With reference to the accompanying figures, embodiments of the invention will now be described in greater detail. In
An intermediate chamber 130 is defined by an intermediate chamber assembly 160. Intermediate chamber assembly 160 is connected with both gas chambers 110 and 120, which in the depicted embodiment are situated across from one another on opposing sides of the intermediate chamber assembly 160. Intermediate chamber assembly 160 in
As can be seen from the figures, gas port 115 is larger than gas port 125. This allows for a greater flow rate of gas through gas port 115 than through gas port 125 at a given pressure. The reasons for providing gas chambers that discharge at uneven rates will be apparent and will be described later in connection with a description of the use of an embodiment of the inflator apparatus.
Optionally, a diffuser may be positioned adjacent to the gas exit port. In
A closure member may be positioned and configured to block fluid communication through the gas exit port until the initiator is deployed. In the embodiment shown in
Another embodiment is shown in
In order to maintain chamber 210 at a higher pressure than chamber 220, ports 215 and 225 are blocked with burst disks 219 and 229, respectively, such that they are isolated from one another. Both chambers also have fill ports and fill port plugs. High pressure chamber 210 has fill port 216 occupied by fill port plug 218, whereas low pressure chamber 220 has fill port 226 occupied by fill port plug 228.
Initiator mount assembly 244 differs significantly from initiator mount assembly 144. Specifically, initiator mount assembly 244 includes a tunnel portion 246. Tunnel portion 246 may be included to provide a way to direct the shock wave generated by the initiator 242 towards burst disks 219 and 229. As shown in
As shown in
Still another embodiment is shown and will now be described with reference to
Heater 370 may be activated simultaneously with, or just prior to, deployment of initiator 342. In this manner, the pressure of the gas in chamber 310 can be increased at the time of or just prior to deployment. This further facilitates allowing the airbag to be primarily inflated by gas from gas chamber 310 and substantially maintained in an inflated state for a predetermined period of time primarily by gas from gas chamber 320.
Without further elaboration, it is believed that one skilled in the art can use the preceding description to utilize the invention to its fullest extent. The examples and embodiments disclosed herein are to be construed as merely illustrative and not a limitation of the scope of the present invention in any way. It will be apparent to those having skill in the art that changes may be made to the details of the above-described embodiments without departing from the underlying principles of the invention. In other words, various modifications and improvements of the embodiments specifically disclosed in the description above are within the scope of the appended claims. The scope of the invention is therefore defined by the following claims.
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