Patent Publication Number: US-2021179010-A1

Title: Gas generator, especially for a vehicle safety system

Description:
The invention relates to a gas generator, especially for a vehicle safety system, as set forth in claim  1 . Further, the invention deals with an airbag module comprising such gas generator and with a vehicle safety system comprising such gas generator. 
     Gas generators supply e.g. gas for filling an airbag or for driving a belt tensioner or a hood stay. 
     It is a drawback in known gas generators that frequently they have single components of complex design which are interconnected by a plurality of elaborate and expensive connecting technologies. 
     Against this background, it is an object of the present invention to eliminate or mitigate at least one of said aforementioned drawbacks. In particular, the invention is intended to state a gas generator that includes components of simple design which are interconnected by little-elaborate connecting technologies. 
     It is another object of the invention, to state an enhanced airbag module, a vehicle safety system and a method for operating a gas generator. 
     In accordance with the invention, this object is achieved, with respect to the gas generator, by the subject matter of claim  1 , with respect to the airbag module, by the subject matter of claim  14  and, with respect to the vehicle safety system, by the subject matter of claim  15 . 
     The gas generator according to the invention includes a sleeve positioned inside the gas generator which has first flow orifices and an ignition chamber including a first propellant, wherein a combustion chamber filled with a second propellant which is surrounded by a diffusor located inside the gas generator and having second flow orifices is connected to the outside of the sleeve. In addition, the gas generator according to the invention includes a baffle plate having third flow orifices and surrounding the diffusor, with the sleeve, the diffusor and the baffle plate being adhesively bonded to each other. 
     In the gas generator according to the invention, three components, i.e. the sleeve, the diffusor and the baffle plate, on the one hand are simply designed and each includes predefined openings in the form of material-penetrating orifices or breakthroughs, and, on the other hand, the three components are tightly interconnected by adhesive bonding, thus preventing all of the three components from being mutually unintentionally displaced or from being inadvertently changed in position relative to each other. This applies both to an idle state of the gas generator in which no activation as intended has been implemented yet and to an activating state in which the gas generator has been or is activated as intended. 
     In addition, said adhesive bonding between the simply designed single components of sleeve, diffusor and baffle plate enables said three single components to act quasi like one single subassembly of substantially more complex design which is understood to be so-to-speak the sum of the three single components. In detail, this means that, on the one hand, already when mounting the gas generator this fact can offer an advantage by appropriately handling or treating such subassembly consisting of a sleeve, a diffusor and a baffle plate. On the other hand, this can be advantageous when or after activating the gas generator, as the adhesively bonded single components of a sleeve, a diffusor and a baffle plate can behave or act at least in portions like a subassembly formed of the same, wherein especially portions of the diffusor and the baffle plate together with the sleeve can be displaced, while acting as structural unit, in one direction, preferably displacing direction, as will be detailed further below. 
     Especially, the sleeve, the diffusor and the baffle plate can be connected by one single welded joint or by plural welded joints, especially a first welded joint and a second welded joint, wherein the welded joints may preferably be configured as radially peripheral welded joints. With respect to the manufacture of the gas generator, it may be of major advantage when the components of sleeve, diffusor and baffle plate are connected by one single welded joint, as before producing the welded joint said three components need to be positioned relative to each other merely once and, in addition, said connection can be made by one single welding operation. This is time-saving and cost-saving and, moreover, imparts a high degree of precision to such design, as components and/or component groups need not be positioned relative to each other several times in succession in an elaborate manner before a welding operation. In addition, when producing such single welded joint, merely one single quality control, especially monitoring of a weld pool for the welded joint, is required. Even if a first welded joint and a second welded joint are provided instead, the already aforementioned advantages concerning an adhesive bonding of the sleeve, the diffusor and the baffle plate are still maintained. 
     Preferably, in the gas generator the sleeve may be in the form of a substantially hollow-cylindrical component having a front-side first opening and an axially opposed second opening, the first opening being closed by the diffusor and a tamping being optionally positioned between the diffusor and the sleeve. As the sleeve has two opposed openings, i.e. has no closure or bottom at any front side, it can be manufactured at extremely low costs. A closure at a front side can be implemented at low cost by the diffusor or a bottom portion thereof. Accordingly, it may be necessary or beneficial in terms of construction that a tamping, e.g. in the form of a thin metal foil, is positioned or inserted between the sleeve and the diffusor. In such design, especially the tamping can equally be fastened by welding even with the one single welded joint that interconnects the sleeve, the diffusor and the baffle plate, and thus can also be adhesively bonded or connected to the sleeve and the diffusor. 
     In particular, the sleeve may be closed at its second opening by a holder which preferably receives an igniter and may be slidably supported on the same in a displacing direction. The sleeve may be attached or press-fitted onto the holder so that it is slidably adjacent along a certain longitudinal extension of the holder in the displacing direction, especially away from the holder. Here the holder can constitute a type of guideway, when the sleeve is displaced. In the case of activation and, resp., operation of the gas generator, pressure which causes the sleeve to be displaced may build up inside the ignition chamber. 
     In particular, a plane radially extending through the first flow orifices, especially the centers thereof, can equally extend through the third flow orifices, especially the centers thereof, and the second flow orifices can be arranged to be spaced apart from the plane. The plane is an imaginary plane that extends especially perpendicularly to a longitudinal axis of the gas generator through the first and third flow orifices and, thus, defines the axial length and, resp., position thereof within the gas generator and relative to each other. Accordingly, the first flow orifices of the sleeve can constitute the first openings for a path of the gas stream which can be generated inside the ignition chamber, wherein the third flow orifices of the baffle plate may be the last orifices for said gas stream along this path inside the gas generator, before the gas stream can leave the gas generator to the outside into environment of the gas generator. Thus, the first and the last orifices for a gas stream on its way through the gas generator may be located at an equal axial position, as indicated by the plane. 
     Preferably, upon activation of the gas generator, the sleeve having the first flow orifices can be displaced in a/the displacing direction, especially along a longitudinal axis of the gas generator, especially such that the plane is positioned outside the third flow orifices, especially between the third and second flow orifices. Upon activation of the gas generator, by burning off the first propellant by means of an igniter inside the ignition chamber pressure can be built up which will increase to such extent that, despite the possibility of reducing pressure through the first flow orifices, it can move and, resp., lift or displace the sleeve especially in a direction away from the igniter. By displacing the sleeve, correspondingly also the first flow orifices in the sleeve are displaced so that the (imaginary) plane is correspondingly displaced as well. The distance of such displacement may be so long that the plane will no longer extend through the third flow orifices. 
     Especially, the sleeve includes a substantially radially extending first sleeve portion that is adhesively bonded to the inside of a bottom of the diffusor and that is transformed into a conical second sleeve portion tapering toward the sleeve center axis to which second sleeve portion a third sleeve portion extending substantially in parallel to the sleeve center axis and especially including the first flow orifices is connected. In this way, the sleeve is designed as a trumpet-type cavity that is easy to manufacture. The third sleeve portion can help attach or push the sleeve onto a/the igniter or onto a/the holder of the igniter so that it can be easily closed by the latter at its second opening. The arrangement of the first flow orifices in the third sleeve portion is advantageous with respect to a gas discharge and, resp., a flow path of a gas, as will be described in more detail further below. However, it is also imaginable for the first flow orifices to be arranged only or additionally in the conical second sleeve portion. 
     The baffle plate may be closed by a closure bottom and with the latter may form an area of the outer housing of the gas generator, and the closure bottom may enclose, together with the diffusor and the sleeve, the combustion chamber especially such that the combustion chamber is in the form of a toroidal chamber which, when viewed in the longitudinal section, preferably includes sidewalls substantially aligned in parallel to each other and facing the closure bottom which are transformed into sidewalls converging obliquely relative to each other in a direction facing away from the closure bottom. If the sidewalls of the combustion chamber converge obliquely relative to each other in an area facing away from the closure bottom, the special spatial configuration of the combustion chamber causes the combustion chamber to narrow in this area. If, in this area of the narrowing, discharge orifices of the combustion chamber, and concretely speaking the second flow orifices in the diffusor, are provided, then the flow rate for gas generated in and exiting the combustion chamber can be advantageously optimized, especially increased in this case. In other words, the combustion chamber extends, when viewed in the longitudinal section of the gas generator, in the form of a nozzle so that a discharge rate for gas exiting the combustion chamber can be advantageously increased. 
     In particular, the baffle plate may be connected to the closure bottom and the diffusor by means of one single, especially radially circumferential, weld, and/or the combustion chamber may include an axis of symmetry which extends through the second flow orifices, especially the centers thereof, substantially in parallel to the longitudinal axis of the gas generator. Here, too, it is of advantage, when manufacturing the gas generator, to adhesively bond three components to each other in a cost-saving and time-saving manner, as with such single welded joint merely one single working step and/or one single quality control, especially monitoring a weld pool for the welded joint, is required. In addition, when the combustion chamber has such a symmetric design that an axis of symmetry extends through the second flow orifices through which gas generated in the combustion chamber can or shall flow out, then the gas can advantageously flow extremely uniformly out of said combustion chamber through the second flow orifices. 
     The baffle plate may be pot-shaped and may have a cylindrical first wall portion to which a conical radially inwardly narrowing second wall portion is connected, the latter being transformed into a bottom portion substantially perpendicularly to the longitudinal axis of the gas generator, wherein the baffle plate preferably includes a recess in the bottom portion and/or the third flow orifices as slot-shaped substantially rectangular openings. As compared to the cylindrical first wall portion, the conical radially inwardly narrowing second wall portion helps provide, outside said wall portion, more space for adjacent components. This is especially the case when the baffle plate here forms an area of the outer housing. Concretely speaking, the gas generator can be mounted in a more space-saving manner into a module surrounding the latter and including an airbag to be inflated by the gas generator. In other words, the gas generator claims less space in the conical area as compared to adjacent components toward the outside than this is the case in the cylindrical area of the first wall portion of the baffle plate. The recess in the bottom portion of the baffle plate can be advantageously utilized for positioning and/or centering the gas generator by the recess engaging, with complementary action, in a projection of a neighboring component such as e.g. the afore-mentioned module. In addition, or as an alternative, the recess may serve as a constructional measure for increasing the wall stiffness of the baffle plate, which is of advantage in an event of elastic and/or plastic deformation of the baffle plate in this area by increasing internal pressure inside the gas generator after activation of the gas generator. By the baffle plate being also adhesively bonded to the diffusor, this advantage may quasi be transferred to the diffusor, too. What is meant by this is the fact that the increase in the wall stiffness of the baffle plate thus has a correspondingly positive effect, quasi like an increase in the wall stiffness, on the diffusor, as the diffusor and the baffle plate are appropriately adhesively bonded to each other in a load-transmitting manner. By configuring the third flow orifices as slot-shaped substantially rectangular orifices, after activation of the gas generator, gas generated inside the gas generator which is to be discharged to the environment of the gas generator can be guided through correspondingly configured third flow orifices in an extremely advantageous manner. 
     The diffusor may be pot-shaped and may include a cylindrical first portion to which a conical radially inwardly narrowing second portion is connected which is transformed into a/the bottom of the diffusor substantially perpendicularly to the longitudinal axis of the gas generator and includes the second flow orifices. This configuration especially helps obtain the afore-mentioned advantageous shape of the combustion chamber. 
     In particular, the baffle plate and the diffusor can enclose a pot-shaped gas guiding chamber and/or extend substantially in parallel to each other over the entire area of the/a gas guiding chamber, with the exception of the/a recess of the baffle plate. Such a design or such designs can help achieve hot gas introduced from the combustion chamber into the gas guiding chamber to be guided as uniformly as possible and along a relatively long distance in the gas guiding chamber, which distance offers sufficient possibilities of efficiently filtering and/or cooling the gas, before the gas can be discharged through the third flow orifices of the baffle plate to the environment of the gas generator. Hence, due to the fact that the gas guiding chamber is pot-shaped, not only lateral areas of the gas guiding chamber but also quasi “ceiling areas” of the gas guiding chamber are available to this end. In other words, such gas guiding chamber extends in axial and radial directions. 
     Preferably, in the case of activation of the gas generator, gas formed in the ignition chamber can flow into the combustion chamber only in the radial direction through the first flow orifices of the sleeve, and gas formed in the combustion chamber can flow into the/a gas guiding chamber only in the axial direction through the second flow orifices of the diffusor, wherein especially areas of the diffusor and of the baffle plate can be displaced together with the sleeve as a structural unit in the displacing direction. By such given direction of the gas, said gas can be guided with a deflection of direction and over a relatively long distance inside the gas generator, with options for efficient filtering and/or cooling of the gas being advantageously given here, for example by efficient desired slag deposition from the gas which may entrain slag/particles. 
     Due to the fact that areas of the diffusor and the baffle plate can be displaced together with the sleeve as a structural unit in the displacing direction, said areas of the diffusor and the baffle plate interact with the sleeve quasi like one single or common pot-shaped container that is closed by the closure bottom, wherein, after activation of the gas generator, internal pressure forming thereafter can raise the structural unit for pressure compensation or deform the same in the displacing direction. In other words, after activation of the gas generator, by burning off the propellants such high internal pressure can be generated within the gas generator that areas of the outer housing thereof can bulge and can deform elastically and/or plastically to a certain small extent, which may be desired as intended. Such deformation may advantageously be carried out or implemented in a material-saving manner by the afore-described displacement of the structural unit comprising the diffusor, the baffle plate and the sleeve, as no single individual components are excessively point-loaded, but the structural unit per se can be loaded in a mechanically optimized way. 
     A coordinate aspect of the invention relates to an airbag module comprising a gas generator, an airbag inflatable by the gas generator and a fastener for mounting the airbag module on a vehicle, the gas generator being preferably configured according to the afore-described manner. 
     Furthermore, within the scope of the present application, there is disclosed and claimed a vehicle safety system, especially for the protection of a person, such as, for example, a vehicle occupant or a pedestrian, comprising a gas generator, an airbag inflatable by the latter as part of an airbag module, and an electronic control unit by means of which the gas generator can be activated if a release situation is given. In the vehicle safety system according to the invention, preferably the gas generator is configured according to the afore-described manner. 
    
    
     
       Hereinafter, the invention shall be illustrated in detail by way of example embodiments with reference to the attached schematic figures, wherein: 
         FIG. 1  shows a longitudinal section view across a gas generator according to the invention, and 
         FIG. 2  shows a three-dimensional representation of the gas generator as shown in  FIG. 1 . 
     
    
    
     In the following, like reference numerals will be used for like and equally acting parts. 
       FIG. 1  illustrates a longitudinal section across a gas generator  10  according to the invention having a longitudinal axis A along which the gas generator axially extends and a center axis M, the axes A being shown in  FIG. 1  such that they are positioned to be congruent with the center axis M. The gas generator  10  includes a pot-shaped baffle plate  12  having a bottom portion  20  and third flow orifices  14  which are arranged in the baffle plate  12  as material-penetrating openings or breakthroughs. A closure bottom  30  closes the baffle plate  12  on the open side of the baffle plate  12  facing the bottom portion  20 . The baffle plate  12  and the closure bottom  30  together form part of an outer housing of the gas generator  10 . The baffle plate  12  includes, especially centrally in the area of its bottom  20 , a recess  21  which is to be understood as an indentation of the bottom  20  in the direction of the interior of the baffle plate  12 . The closure bottom  30  includes an especially central opening  32  which is closed by a holder  46  and an igniter  40  received by the holder  46 . Inside the gas generator  10 , a sleeve  60  is fastened to the holder  46 , wherein especially the holder  46  has a substantially cylindrical portion to which the sleeve  60  is attached with a substantially hollow-cylindrical third sleeve portion  66  shaped to be correspondingly complementary to the portion, in such a way that the sleeve  60  is slidably supported along a longitudinal extension of the holder  46  or along the cylindrical portion of the holder  46  in a displacing direction V away from the closure bottom  30 . A second sleeve portion  64  which extends, with an increasing distance from the third sleeve portion  66 , conically outwardly, viz. away from a central sleeve center axis H, is connected to the substantially parallel sidewall of the third sleeve portion  66 . The second sleeve portion  64  is finally transformed, in an end area of the sleeve  60 , into a first sleeve portion  62  extending radially outwardly and substantially perpendicularly to the sleeve center axis H, said sleeve portion  62  inwardly enclosing a first opening  61  of the sleeve  60 . The sleeve  60  is in the form of a cavity open to both front sides which, on one front side, includes the first opening  61  and, on the front side opposed thereto, includes a second opening  63  which is enclosed by a corresponding end area of the third sleeve portion  66 . Accordingly, the sleeve  60  can also be understood to be a trumpet-type cavity. 
     The sleeve  60  is fastened, with its first sleeve portion  62 , to a diffusor  70  located inside the gas generator  10  and including second flow orifices  78 , especially to a bottom  76  of the diffusor  70  there. A tamping  79 , especially in the form of a thin metal foil made from e.g. steel, copper or aluminum, closes the second flow orifices  78  of the diffusor  70  in an idle state of the gas generator  10  in which the gas generator is not or has not yet been activated as intended. 
     Accordingly, the tamping  79  between the sleeve  60  and the diffusor  70  may be arranged as a full-surface disk-shaped component, as shown in  FIG. 1 . As an alternative to this, it is also possible, however, for the tamping  79  to be configured as a ring-shaped element (not shown) and to close the second flow orifices  78  of the diffusor  70  such that the tamping  79  is not positioned between the sleeve  60  and the diffusor  70  or, resp., need no longer be positioned there. In other words, with this alternative, the tamping  79  would be arranged over the flow orifices  78  to ensure merely minimum covering, but it would not extend further radially inwardly between the sleeve  60  and the diffusor  70 . 
     The sleeve  60  encloses an ignition chamber  52  that is filled with a first propellant  50 . The ignition chamber  52  is delimited by the sleeve  60 , the holder  46  including the igniter  40  and the diffusor  70  and, resp., the tamping  79  applied, especially bonded or welded, to the diffusor  70 . The ignition chamber  52  may be understood to be a space formed corresponding to the trumpet shape of the sleeve  60  and may be described as a substantially frustoconical space including a sidewall which converges tapering in the direction of the igniter  40  toward the sleeve center axis H. 
     Outside the sleeve  60  and directly adjacent thereto, there is formed a combustion chamber  56  in which a second propellant  54  is disposed. Each of the two propellants, the first and second propellants ( 50 ,  54 ), may comprise, as a fill of individual propellant bodies, e.g. compressed, especially dry-compressed propellant pellets or extruded bodies, but may also be present in the form of broken granules or in the form of a monolithic molded body or in the form of stringed disks or rings. The first and second propellants ( 50 ,  54 ) may be similar with respect to their chemical composition and/or their shape, or else may be different in this respect. The combustion chamber  56  is delimited by the sleeve  60 , the diffusor  70  with the tamping  79  fastened there and the closure bottom  30 , and may be understood to be a toroidal chamber which, when viewed in the longitudinal section ( FIG. 1 ), preferably has sidewalls substantially aligned in parallel to each other facing the closure bottom  30  which are transformed into sidewalls converging obliquely relative to each other in the direction away from the closure bottom ( 30 ). Thus, the combustion chamber  56  surrounds the ignition chamber  52  in a radially circumferential manner. 
     Between the diffusor  70  and the baffle plate  12 , a ring-shaped filter  80  is positioned and is especially clamped, press-fitted and/or non-positively or positively connected between said two components. The filter  80  takes a shape which is complementary to its contact faces with said two components. In particular, the filter  80  is understood to be a cavity having a cylindrical portion which is especially in the form of a straight circular cylinder, with a frustoconical portion being connected thereto, and having a sidewall which is tapered radially inwardly. The filter  80  may be made from metal, especially in the form of a knitted mesh, a coil or single-layer or multi-layer sheet members, and has the function to cool gas flowing out of the gas generator  10  and/or to filter said gas for particles. When manufacturing the gas generator, for example, the filter  80  may initially be attached or press-fitted onto the diffusor  70 , and then the baffle plate  12  may be attached or press-fitted onto the filter  80  or fastened by a press-fit connection thereto, from outside while surrounding the filter  80 . 
     The sleeve  60  includes first flow orifices  68  which are formed especially in the third sleeve portion  66  as individual material-penetrating openings or breakthroughs, preferably in the form of circular holes. The number of the first flow orifices  68  is four, but it may as well be less or more, with the first flow orifices  68  being preferred to be arranged at equal axial height radially circumferentially on the sleeve  60 . The first flow orifices  68 , or at least some of them, might also be arranged in the second sleeve portion  64  of the sleeve  60 . The first flow orifices  68  constitute a connection for a gas between the ignition chamber  52  and the combustion chamber  56 , and preferably are unclosed already in an idle state of the gas generator  10 . However, it is also imaginable for the first flow orifices  68  to be closed by a metal foil (not shown) and, in the case of operation, after activation of the gas generator  10 , are opened by an internal pressure increasing in the ignition chamber  52  by the metal foil tearing or being locally destroyed. 
     Hereinafter, a flow path S of a gas inside the gas generator after activation thereof as intended is described. To simplify matters, in the following merely a gas or a flow of gas or a gas flow is mentioned, wherein always gas formed inside the gas generator and a possible admixture of particles in said gas is meant, as by burn-off or disintegration of a propellant also additional, usually hot particles which may be admixed to said gas are generated apart from hot gas. 
     Upon activation of the gas generator  10 , the igniter  40  including one or more, especially two, contact elements  42  is triggered and, resp., activated by means of a current pulse. Accordingly, a plug connected to a control device (both of which are not shown) is plugged to the gas generator  10 , especially into a plug interface  48 , and transmits the current pulse from the control device to or into the igniter  40  which in its interior has an element forming pressure and/or particles, such as pyrotechnics, which is surrounded by a cap  44  of the igniter  40 . After triggering the igniter  40 , such high pressure is built up inside the igniter  40  that the cap  44  opens or breaks, with gas being released into the ignition chamber  52  to ignite the first propellant  50 . In  FIG. 1 , a possible path of a flow of the gas is illustrated by an elongate appropriately shaped line that is interspersed with directional arrows for such flow path S. By the ignition of the first propellant  50  also gas is generated that can enter or flow through the first flow orifices  68  from the ignition chamber  52  into the combustion chamber  56 .
 
The gas that has flown into the combustion chamber  56  then can ignite the second propellant  54  present there, the latter equally generating, by its burn-off, further gas which breaks the tamping  79  by increasing pressure and enables the gas to flow out of the combustion chamber  56  through the second flow orifices  78  of the diffusor  70 .
 
The gas exiting the combustion chamber  56  then flows into a gas guiding chamber  58  which is enclosed by the baffle plate  12  as an outer delimitation and the diffusor  70  as an inner delimitation. In the area of its recess  21 , the baffle plate  12  is connected to and contacts the diffusor  70  so that no gas guiding chamber can form in this area. Accordingly, the gas guiding chamber  58  can be understood to be a pot-shaped chamber, in the aforementioned area of the recess  21  a bottom area of said chamber being quasi spared. In particular, over the entire area of the gas guiding chamber  58 , the baffle plate  12  and the diffusor  70  extend substantially in parallel to each other, wherein the recess  21  is to be excluded therefrom and, resp., is not to be considered.
 
After flowing into the gas guiding chamber  58 , the gas is guided along the contour of the baffle plate  12  and the diffusor  70  through the filter  80  up to the third flow orifices  14  of the baffle plate  12  through which it then passes and flows into an outer area or into the environment of the gas generator  10 .
 
     On the whole, the afore-mentioned generation and guidance of the gas by way of the arrow symbol for the flow path S can also be described as follows with respect to the direction, especially with respect to one, advantageously several changes of direction of the flow path S. 
     After activating the gas generator  10 , initially by breaking the cap  44  of the igniter  40 , a first quantity of gas is released into the ignition chamber  52 , substantially in the direction of the bottom  76  of the diffusor  70  facing the breaking cap  44 . Then, after a relatively short distance, a reversal of the flow path S substantially by 180° in the direction of the first flow orifices  68  of the sleeve  60  will follow. This flow path is due to the fact that the first flow orifices  68  are the only orifices through which the gas can flow out of the ignition chamber  52 . Here, a particular advantage of the specific cone-shaped ignition chamber  52  and, resp., of the correspondingly conical area of the sleeve  60  takes effect, for, as the second sleeve portion  64  is appropriately tapered toward the sleeve center axis H, gas generated in the ignition chamber  52 , especially ignition gas for igniting the second propellant  54 , can be guided extremely quickly toward or through the first flow orifices  68 . The afore-mentioned conical shape results, toward the first flow orifices  68  and in the environment thereof inside the ignition chamber  52 , in a nozzle-type narrowing or a nozzle-shaped annular passage toward the first flow orifices  68 . In this way, the gas can be advantageously accelerated in the direction of first flow orifices  68  to pass through the first flow orifices  68  as quickly as possible so as to ignite the second propellant  54  in the combustion chamber  56  as effectively as possible and with correspondingly efficient impact. 
     The sleeve  60 , the diffusor  70  and the baffle plate  12  are adhesively bonded to each other. It is possible for said three components to be interconnected by one single joint, especially one single welded joint  15 . The welded joint  15  is provided as a radially circumferential weld or welding extending across the materials of all three components and may especially be a laser weld. When manufacturing the gas generator  10 , the three components of sleeve  60 , diffusor  70  and baffle plate  12  can be positioned properly relative to each other. After that, by means of suitable laser adjustment, especially focal adjustment of a welding laser, a laser beam can appropriately act upon the three components from the inside of the diffusor  70  or from the outside of the baffle plate  12  so that the three components are adhesively bonded to each other in one single melting area which is symbolically represented by the reference numeral  15  only on one side in the views of  FIGS. 1 and 2 . 
     As an alternative, the sleeve  60 , the diffusor  70  and the baffle plate  12  may also be adhesively bonded to each other by plural welded joints, especially a first welded joint  17  and a second welded joint  18 . Accordingly, the baffle plate  12  may be bonded to the diffusor  70  by the first welded joint  17 , and the diffusor  70  can be bonded to the sleeve  60  by means of the second welded joint  18 . In this case, too, the first and second welded joints  17 ,  18  may be in the form of radially circumferential welded joints and in the Figures are shown only symbolically on one side by a corresponding material bond. 
     Thus, the sleeve  60 , the diffusor  70  and the baffle plate  12  are connected tightly and non-slidably relative to each other, and thus can advantageously act quasi as an assembled complete component. In particular, during manufacture of the gas generator, said component group comprising the sleeve  60 , the diffusor  70  and the baffle plate  12  can be treated as a pre-mounted subassembly. 
     Further, especially areas of the diffusor  70  and of the baffle plate  12  can be displaced along with the sleeve  60  as a structural unit in the displacing direction V. What is meant here is that, upon or after activation of the gas generator  10 , an increasing pressure forming inside the ignition chamber  52  and/or inside the combustion chamber  56  can elastically and/or plastically deform areas of the diffusor  70  and of the baffle plate  12  to the outside. In other words, said areas are bulging and, resp., are deformed to the outside. Such deformation may be desired as intended. In addition, a displacement of the sleeve  60  in the displacing direction V may equally be desired so that, for example, the first flow orifices  66  of the sleeve  60  are equally displaced in the displacing direction V so as to be able to ignite the second propellant  54  more efficiently over a particular longer axial distance through the hot gas which flows through the first flow orifices  66  into the combustion chamber  56 . In other words, a hot gas jet flowing through the first flow orifices  66  into the combustion chamber  56  will so-to-speak pass, over a certain axial distance, along the plurality of propellant bodies in the combustion chamber  56  and will ignite them more extensively and more effectively.
 
Both aforementioned desired effects and, resp., dynamic processes, viz. the bulging and, resp., deforming of the baffle plate  12  and the diffusor  70  and the displacement of the sleeve  60  in the displacing direction V, may advantageously be implemented precisely and without great effort by the fact that the three components of sleeve  60 , diffusor  70  and baffle plate  12  are adhesively bonded to each other. The three components cannot be inadvertently displaced or deformed detrimentally relative to each other in the afore-mentioned dynamic processes. The baffle plate  12  and the diffusor  70  are especially deformed and moved to be outwardly bulging while acting together quasi like one single component, and the sleeve  60 , while being quasi attached to said two components, is also displaced simultaneously with this movement, without an inadvertent displacement of the sleeve  60  such as e.g. a leakage in the form of a gap between the first sleeve portion  62  and the diffusor  70 , being possible to occur.
 
       FIG. 1  especially illustrates an idle position of the gas generator  10  at which the gas generator  10  has not yet been activated or triggered as intended. The afore-mentioned dynamic processes after activation of the gas generator  10 , viz. the bulging or deforming of the baffle plate  12  and the diffusor  70  and the displacement of the sleeve  60  in the displacing direction V, are not shown separately per se. As is evident from  FIG. 1 , in the idle state of the gas generator  10 , a plane E extends through the first flow orifices  68  of the sleeve  60 , especially the centers thereof, in the radial direction, wherein the plane E equally extends through the third flow orifices  14  of the baffle plate  12 , especially the centers thereof. The second flow orifices  78  of the diffusor  70  are arranged to be spaced apart from the plane E. The plane E is understood to be an imaginary afore-described plane. Upon activation of the gas generator  10 , the sleeve  60  including the first flow orifices  68  can be displaced in the displacing direction V such that the plane E is positioned outside the third flow orifices  14  between the third and second flow orifices  14 ,  78 . In this way, the plane E is displaced quasi upwards (reference to  FIG. 1 ) in the direction of the second flow orifices  78 . 
     The baffle plate  12  may be connected to the closure bottom  30  and the diffusor  70  by means of one single radially circumferential weld  38 , as is symbolically indicated in each of the Figures on one side only (on the left in the Figures). Herefrom similar advantages are resulting, as this has been described already further above concerning the single welded joint  15 . In addition, with the one single weld  38  the further advantage is resulting that also two components comprising the major part of the outer housing of the gas generator  10 , viz. the baffle plate  12  and the closure bottom  30 , can be connected as shell-type components quasi enclosing the gas generator  10  in a pressure-resistant manner. In other words, the single weld  38  allows to manufacture not only a major part of the outer housing but, at the same time, also to adhesively fasten a third component which is pressure-loaded upon activation of the gas generator  10 , i.e. the diffusor  70 . 
     As an alternative, the three components of baffle plate  12 , closure bottom  30  and diffusor  70  may also be adhesively bonded to each other by implementing two separate welds, i.e. a first welded joint  36  between the diffusor  70  and the closure bottom  30  and a second welded joint  37  between the closure bottom  30  and the baffle plate  12 . Accordingly, both welded joints  36  and  37  can be configured as radially circumferential welds. 
     As shown in  FIG. 1 , the combustion chamber  56  includes an axis of symmetry Z which extends through the second flow orifices  78 , especially the centers thereof, substantially in parallel to the longitudinal axis A of the gas generator  10 . As the combustion chamber  56  has such symmetric design, as is visible from  FIG. 1 , the gas can be advantageously generated, in the case of activation, extremely uniformly in the combustion chamber  56  by burning off the second propellant  56 , and then can be guided also homogenously and uniformly inside the combustion chamber  56  and, in such way, can also flow out of the combustion chamber  56  through the second flow orifices  78 . 
     The baffle plate  12  is pot-shaped and includes a cylindrical first wall portion  22  to which a conical radially inwardly narrowing second wall portion  24  is connected which is transformed into the bottom portion  20  substantially perpendicularly to the longitudinal axis A of the gas generator  10 . Over most of its shape, as compared to the afore-described shape or configuration of the baffle plate  12 , the diffusor  70  has a relatively similar outline or a similarly complementary contour, as is clearly visible from  FIG. 1 . 
     The diffusor, too, is pot-shaped and has a cylindrical first portion  72  to which a conical radially inwardly narrowing second portion  74  is connected which is transformed into the bottom  76  of the diffusor  70  substantially perpendicularly to the longitudinal axis A of the gas generator  10 . Thus, the baffle plate  12  and the diffusor  70 , and, resp., the contours thereof, extend along a relatively large distance, viz. substantially along the extension of the gas guiding chamber  58  formed by said two components, substantially in parallel to each other. Consequently, the gas guiding chamber  58  has a very homogenous design and, resp., gas can be guided through the gas guiding chamber  58  in an advantageously homogenous manner. 
     The closure bottom  30  has an arch  34  which, upon activation of the gas generator  10 , may serve as a type of resilient member. As also in this case the closure bottom  30  can be deformed elastically and/or plastically somewhat outwardly by increasing internal pressure inside the gas generator  10 , the arch  34  serves as a type of dynamically loadable compensation member which is adapted to absorb or cushion at least a certain proportion of deformation. In so doing, the arch  34  may bend in the direction of the outer area of the gas generator  10  (not shown) and may absorb and, resp., compensate a proportion of respective deformation forces. 
     The baffle plate  12  includes an outwardly radially projecting edge or collar which is in the form of a flange  16  and may serve for mounting the gas generator  10  to further components (not shown), such as e.g. components of an airbag module or a vehicle. For this purpose, the flange  16  may include openings or breakthroughs (not shown). 
     Especially the third flow orifices  14  of the baffle plate  12  are slot-shaped substantially rectangular orifices. Concretely speaking, six of said orifices extend to be radially circumferential, preferably equally spaced from one another, about the periphery of the baffle plate  12 . Orifices of this type enable gas to flow out of the gas generator  10  to the environment thereof in an extensive and smoother way than this would be the case with plural smaller orifices. Thus, especially the large-area third flow orifices  14  and, resp., the material of the baffle plate  12  surrounding said orifices are not loaded in an excessively eroding manner by a quickly discharging gas. 
       FIG. 2  illustrates the same embodiment of the gas generator  10  as it is shown in  FIG. 1 , in a perspective view. Here the same reference numerals as in  FIG. 1  are used for like and equally acting parts. Especially, in  FIG. 2  furthermore an opening or a bore in the flange  16  of the baffle plate  12  is shown which may be used to fasten the gas generator  10  to an airbag module (not shown). In addition, in  FIG. 2  a possible configuration of a third flow orifice  14  of the baffle plate  12  is visible which, as already described in the foregoing, may be in the form of an elongate rectangular orifice or of a corresponding slot-shaped orifice. 
     REFERENCE NUMERALS 
     
         
           10  Gas generator 
           12  baffle plate 
           14  third flow orifice 
           15  welded joint 
           16  flange 
           17  first welded joint 
           18  second welded joint 
           20  bottom portion 
           21  recess 
           22  first wall portion 
           24  second wall portion 
           30  closure bottom 
           32  opening 
           34  arch 
           36  first weld seam 
           37  second weld seam 
           38  weld 
           40  igniter 
           42  contact element 
           44  cap 
           46  holder 
           48  plug interface 
           50  first propellant 
           52  ignition chamber 
           54  second propellant 
           56  combustion chamber 
           58  gas guiding chamber 
           60  sleeve 
           61  first opening 
           62  first sleeve portion 
           63  second opening 
           64  second sleeve portion 
           66  third sleeve portion 
           68  first flow orifice 
           70  diffusor 
           72  first portion 
           74  second portion 
           76  bottom 
           78  second flow orifice 
           79  tamping 
           80  filter 
         A longitudinal axis 
         E plane 
         H sleeve center axis 
         M center axis 
         S flow path 
         V displacing direction 
         Z axis of symmetry