Hybrid gas generator for a vehicle safety system with an opening device for a pressurized gas container

The hybrid inflator design with a bendable combustion chamber base and opening device addresses the complexity of existing inflators, achieving efficient and controlled gas outflow for airbag deployment, enhancing safety and reducing weight.

DE102014018007B4Active Publication Date: 2025-10-30ZF AIRBAG GERMANY GMBH
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Patent Information

Application Number
DE102014018007
Authority / Receiving Office
DE · DE
Patent Type
Patents
Current Assignee / Owner
Filing Date
2014-12-05
Publication Date
2025-10-30
Estimated Expiration
2034-12-05

AI Technical Summary

Technical Problem

Existing hybrid inflators for vehicle safety systems have complex constructions with many components and seals, leading to potential faults and inefficiencies in the controlled outflow of gases for airbag deployment.

Method used

A hybrid inflator design featuring a combustion chamber with a sleeve-like side wall and a combustion chamber base that is firmly connected and bendable, allowing for a simple construction without movable parts, and includes a bendable opening device to control the outflow of gases by bending and opening a membrane, ensuring a controlled and efficient gas flow into the airbag.

Benefits of technology

The solution enables a controlled and efficient outflow of cold and hot gases into the airbag, reducing complexity and potential faults, while allowing for weight savings and improved safety system performance.

✦ Generated by Eureka AI based on patent content.

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Abstract

Hybrid gas generator (20) for a vehicle safety system with a pressurized gas container (21) an opening (23) which, in a rest state of the hybrid gas generator (20), is closed with a membrane (25) which, in the event of operation, can be destroyed by an opening device, such that the pressure gas container (21) is fluidly connected to a mixing chamber (40) and to a combustion chamber (30) with the opening device for the pressure gas container (21), wherein the combustion chamber (30) comprises a sleeve-like combustion chamber side wall (34) defining a combustion chamber interior (31) and a combustion chamber bottom (10), wherein the opening device is arranged on a surface (11) of the combustion chamber bottom (10) pointing away from the combustion chamber interior (31) and the combustion chamber bottom (10) is firmly bonded to the combustion chamber side wall (34) in such a way that the combustion chamber bottom (10) is bendable in the event of operation, characterized in that a fuel (42) is contained in the combustion chamber (30), which burns down when in operation,and at least one outlet opening (15) is formed in the combustion chamber floor (10), which in the standby state of the hybrid gas generator (20) is closed on the side of the combustion chamber interior (31) with a closure cover (28), wherein the closure cover (28) is destructible in the operating case in such a way that the combustion chamber (30) is fluidly connected to the mixing chamber (40), wherein , In the event of operation, the fluid connection from the pressure gas container (21) to the mixing chamber (40) can be formed before the fluid connection from the combustion chamber (30) to the mixing chamber (40).
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Description

[0001] The invention relates to a hybrid gas generator, a gas bag module and a vehicle safety system.

[0002] Occupant restraint systems for motor vehicles typically include airbag modules containing a gas bag that inflates upon impact to reduce the likelihood of a vehicle occupant's body parts colliding with a vehicle component. To inflate the gas bag upon impact, hybrid gas generators are used, for example. These generators comprise a pressurized gas cylinder containing a compressed gas or fluid and a pyrotechnic assembly. The pyrotechnic assembly serves to trigger the hybrid gas generator and / or heat the initially compressed gas that is then released upon activation. The pressurized gas of such a hybrid gas generator can be sealed pressure-tight from the pyrotechnic assembly. This is achieved, for example, by a rupture membrane.This is made possible by a rupture cap, which, in its resting state, can be exposed to the pressurized gas stored in the pressure vessel on one end face and / or its outer circumferential side. The term "resting state" means that the hybrid gas generator has not yet been activated, or in other words, that the rupture diaphragm is closed and no activation signal has yet been received that would cause the rupture diaphragm to open or burst.

[0003] The publication EP 1 053 915 B1, in particular the information contained therein Fig. Figures 1 to 4 illustrate the construction of a hybrid gas generator with a storage chamber and a pyrotechnic ignition device. The storage chamber is separated from a combustion chamber by an inner cone. During activation, the inner cone or membrane is ruptured by a piston-like device. This device consists of a movable piston and a guide mechanism. During activation, the piston is pressurized, causing it to pierce the inner cone or membrane. Supports and guides are required to guide the piston. This is a relatively complex design, comprising numerous components and seals, which necessitates considerable effort to ensure reliable operation.

[0004] Document DE 44 19 752 A1 discloses a hybrid gas generator for a vehicle safety system with a pressure gas container, which includes an opening that is closed in a rest state of the hybrid gas generator with a membrane which acts as an opening device for the pressure gas container in the case of operation and is destructible in such a way that the pressure gas container is fluidly connected to a mixing chamber.

[0005] The generic document DE 197 27 047 A1 discloses a hybrid gas generator for a vehicle safety system with a pressure gas container comprising an opening which, in a rest state of the hybrid gas generator, is closed with a membrane which, in the event of operation, can be destroyed by an opening device such that the pressure gas container is fluidly connected to a mixing chamber, and with a combustion chamber with the opening device for the pressure gas container, wherein the combustion chamber comprises a sleeve-like combustion chamber side wall and a combustion chamber bottom, the opening device being arranged on a surface of the combustion chamber bottom pointing away from the combustion chamber interior, and the combustion chamber bottom being firmly connected to the combustion chamber side wall in such a way that the combustion chamber bottom is bendable in the event of operation.

[0006] The object of the present invention is to further develop a hybrid gas generator in such a way that an optimally controlled outflow into a gas bag is made possible.

[0007] Furthermore, the object of the invention is to provide a gasbag module and a vehicle safety system with an advanced hybrid gas generator.

[0008] According to the invention, this problem is solved with regard to the hybrid gas generator by the subject matter of claim 1, with regard to the gas bag module by the subject matter of claim 11 and with regard to the vehicle safety system by the subject matter of claim 12.

[0009] Advantageous and appropriate embodiments of the hybrid gas generator according to the invention are specified in the dependent claims.

[0010] The invention is based on the concept of a combustion chamber with an opening device for a pressure gas container of a hybrid gas generator, wherein the combustion chamber comprises a sleeve-like combustion chamber side wall and a combustion chamber bottom, the opening device being arranged on a surface of the combustion chamber bottom facing away from the combustion chamber interior, and the combustion chamber bottom being firmly bonded to the combustion chamber side wall in such a way that the combustion chamber bottom is bendable when in operation. When the combustion chamber bottom is bent, it remains connected to the combustion chamber side wall. Preferably, the combustion chamber bottom is or remains firmly connected to the combustion chamber side wall along its entire circumference, so that the combustion chamber bottom cannot, for example, perform a folding movement similar to a hinge movement.

[0011] The combustion chamber base therefore includes an opening device that points away from the interior of the combustion chamber, whereby the opening device, together with the combustion chamber base, is bendable in the event of operation. In the event of operation, i.e., when the hybrid gas generator is triggered as intended, i.e., when a fuel is burned in the combustion chamber, the pressure in the combustion chamber increases such that the combustion chamber base deflects towards a pressurized gas container to be opened, whereby the opening device opens a diaphragm that seals the pressurized gas container. The combustion chamber with this opening device therefore requires no sliding elements or components, since the combustion chamber base with the opening device attached to it is designed to be bendable in such a way that no additional movable element is necessary. The design comprises a small number of components and has a simple construction.

[0012] The sleeve-like combustion chamber side wall can, for example, be cylindrical, preferably circular cylindrical. The combustion chamber interior, which is bounded by the sleeve-like combustion chamber side wall, can therefore also have a cylindrical, particularly circular cylindrical, volume. The combustion chamber bottom preferably has a shape adapted to the combustion chamber side wall. In other words, the combustion chamber bottom is complementary to the cross-section of the combustion chamber interior. If the combustion chamber interior is circular cylindrical, the combustion chamber bottom can have a round shape. For other cylindrical shapes of the combustion chamber interior, corresponding square, rectangular, elliptical, oval, or polygonal shapes can be formed.

[0013] The combustion chamber floor is rigidly connected to the combustion chamber side wall. The combustion chamber floor is bonded to the combustion chamber side wall by a material bond. For example, the combustion chamber floor can be welded to the combustion chamber side wall. The combustion chamber floor itself is therefore not designed or mounted in a way that allows it to slide. In the event of activation or operation, the combustion chamber floor, along with the opening device located on the surface of the combustion chamber floor facing away from the combustion chamber interior, can be bent or flexed towards a pressurized gas container to be opened.

[0014] The opening device can be designed as an opening mandrel, in particular as a pyramidal point, round mandrel, flat mandrel, cross mandrel, or ring cutting edge. In other words, the opening device is designed as a projection extending away from the combustion chamber interior, the projection being capable, for example, of opening the membrane of a pressurized gas container.

[0015] At least one outlet opening can be formed in the combustion chamber floor and / or in the combustion chamber side wall, which has a closing cover, in particular a dam, on the side of the combustion chamber interior.

[0016] The combustion chamber floor can have at least one spacer element, in particular in the form of a projection, groove, recess, or depression, on the side of the opening device, i.e., on the surface of the combustion chamber floor facing away from the interior of the combustion chamber. In other words, the combustion chamber floor can be provided with or have a structure on the opening device side so that the outlet openings can establish sufficient fluid contact with a mixing chamber, even if the combustion chamber floor rests on another element of the pressurized gas container and / or the hybrid gas generator.

[0017] In the combustion chamber base, on the side of the opening device, several spacer elements in the form of straight and / or curved lines can be formed, extending from a first, in particular concentric, inner circle to a second, in particular concentric, outer circle, wherein at least one exhaust opening is formed on the second outer circle. The exhaust opening can, for example, be formed as a partial element or as a section of at least one spacer element. A separate or independent formation of the at least one exhaust opening is also possible.

[0018] Preferably, several outlet openings are formed in the combustion chamber floor. The outlet openings are preferably circular. The outlet openings are preferably arranged regularly or at uniform intervals from each other on a preferably concentric circle of the combustion chamber floor. Preferably, at least two, in particular at least four, in particular at least eight, in particular at least twelve, in particular at least fourteen, outlet openings are formed in the combustion chamber floor.

[0019] With regard to a hybrid gas generator, the problem is solved by the features of claim 1. Such a hybrid gas generator with a pressurized gas container comprises a combustion chamber with an opening device for a pressurized gas container.

[0020] The pressure gas container comprises an opening which, in a rest state of the hybrid gas generator, is closed with a membrane which, in the event of operation, is destructive with the opening device, such that the pressure gas container is fluidly connected to a mixing chamber, and to a combustion chamber with the opening device for the pressure gas container, wherein the combustion chamber comprises a sleeve-like combustion chamber side wall and a combustion chamber bottom, which delimits a combustion chamber interior, wherein the opening device is arranged on a surface of the combustion chamber bottom pointing away from the combustion chamber interior and the combustion chamber bottom is firmly connected to the combustion chamber side wall in such a way that the combustion chamber bottom is bendable in the event of operation.

[0021] According to the invention, a fuel is contained in the combustion chamber, which burns during operation. At least one outlet opening is formed in the combustion chamber floor. In the standby state of the hybrid gas generator, this outlet opening is closed on the combustion chamber interior side by a cover. During operation, the cover is destructively ruptured in such a way that the combustion chamber is fluidly connected to the mixing chamber. During operation, the fluid connection from the pressurized gas container to the mixing chamber is established prior to the fluid connection from the combustion chamber to the mixing chamber. Therefore, at least one outlet opening can be formed in the combustion chamber floor of the hybrid gas generator according to the invention. This outlet opening is provided with a cover in the standby state, i.e., in the inactive state of the hybrid gas generator. The cover is located on the combustion chamber interior side of the combustion chamber floor.In the event of operation, i.e., when the hybrid gas generator is activated, the sealing cover of at least one outlet opening is destructible, so that the combustion chamber is fluidly connected to the mixing chamber of the hybrid gas generator.

[0022] The combustion chamber side wall of the combustion chamber of the hybrid gas generator according to the invention can also have an outlet opening, which, in the resting state, is closed on the combustion chamber interior side with a cover. This cover is also breakable during operation, so that the combustion chamber is fluidly connected to, for example, a gas bag. If both the combustion chamber floor and the combustion chamber side wall have outlet openings, all outlet openings are provided with a cover on the combustion chamber interior side, the cover preferably being of the same dimensions for all outlet openings. Therefore, during operation, both the covers of the outlet openings in the combustion chamber floor and the covers of the outlet openings in the combustion chamber side wall are breakable.After the sealing cover(s) are destroyed, the combustion chamber is fluidly connected to both the mixing chamber and the gas bag. Preferably, several outlet openings, preferably at least four, in particular at least eight, in particular at least twelve, in particular at least fourteen, outlet openings are formed in the combustion chamber base and / or in the combustion chamber side wall.

[0023] In the event of a malfunction, both the diaphragm of the pressurized gas container and the sealing cover of an outlet opening in the combustion chamber floor and / or side wall are susceptible to destruction. The diaphragm of the pressurized gas container is destroyed due to internal combustion chamber pressure, which causes the combustion chamber floor to deflect or bend. The combustion chamber floor is forced away from the combustion chamber interior. Since an opening device, specifically designed as an opening mandrel or ring cutter, is located on or arranged in the combustion chamber floor, this opening device is also forced away from the combustion chamber interior due to the deflection of the combustion chamber floor. The opening device, which is located on the surface of the combustion chamber floor facing away from the combustion chamber interior, performs a lifting motion corresponding to the deflection or bending of the combustion chamber floor.The opening device is therefore moved or pressed towards the membrane of the pressurized gas container. Upon contact with or penetration of the membrane, the opening device either opens or destroys it.

[0024] Furthermore, in the event of a malfunction, the sealing cover of at least one exhaust opening in the combustion chamber floor and / or the combustion chamber side wall will be destroyed. The destruction of the sealing cover, particularly the tamping mechanism, occurs, for example, through the material or the cover itself bursting.

[0025] In normal operation, the fluid connection from the pressurized gas container to the mixing chamber can be established before the fluid connection from the combustion chamber to the mixing chamber. In other words, in normal operation, the diaphragm of the pressurized gas container is destroyed before the sealing cover of at least one exhaust port of the combustion chamber is ruptured.

[0026] The closure cover, in particular the dam, of the at least one outlet opening is dimensioned in such a way that, in the event of operation, the fluid connection from the pressure gas container to the mixing chamber can be formed before the fluid connection from the combustion chamber to the mixing chamber.

[0027] Furthermore, the closure cover, in particular the dam, of the at least one outlet opening is dimensioned such that, in the event of operation, a pressure can be built up in the combustion chamber that the membrane of the pressure gas container can be destroyed by bending the combustion chamber floor in the direction of the membrane with the opening device, in particular with the opening mandrel or the ring cutting edge, preferably with at least one through-hole.

[0028] Furthermore, the closure cover, in particular the sealing, of the at least one outlet opening should be dimensioned in such a way that, in the event of operation, the combustion chamber is fluidly connected to the mixing chamber and / or a gas bag.

[0029] In other words, the dam of the at least one outlet opening should be designed and dimensioned such that sufficient pressure can build up in the combustion chamber interior in every operating or activation scenario, so that the opening device located at the bottom of the combustion chamber is reliably moved towards the diaphragm of the pressurized gas container and the diaphragm opens reliably. Due to the damaged or opened diaphragm of the pressurized gas container, gas contained within the container, particularly cold gas, can flow into a mixing chamber. Furthermore, the dam or sealing cover of the at least one outlet opening should be designed and dimensioned such that it can be damaged or opens in time to prevent excessively high pressures in the combustion chamber interior and to allow hot gas, i.e., gas flowing from the combustion chamber, to enter the mixing chamber in a timely manner.

[0030] The sealing cover or tamper of the at least one outlet opening must be dimensioned, with regard to both the material selection and the thickness of the sealing cover material, such that the membrane of the pressurized gas container is ruptured before the sealing cover or tamper is activated. The cold gas from the pressurized gas container can therefore flow into the mixing chamber first, and through openings in the mixing chamber leading towards the gas bag, the cold gas from the pressurized gas container also flows into the gas bag first. After a further pressure increase in the combustion chamber interior, the sealing cover, in particular the tamper, can be ruptured, so that hot gas from the combustion chamber, or from the combustion chamber interior, flows into the mixing chamber and is cooled by the cold gas already present there.

[0031] The combustion chamber's operating pressure is preferably designed such that even if the sealing cover or dam opens prematurely, the pressure prevailing inside the combustion chamber is sufficient to open the membrane with the aid of the opening device, due to the flexible combustion chamber floor. If the combustion chamber side wall has outlet openings, it is conceivable that these outlet openings, or the outlet opening itself, also have a sealing cover, particularly in the form of a dam, with the sealing cover being formed or arranged on the side facing the combustion chamber interior. When the combustion chamber side wall has outlet openings, the mixing of the cold gas with the hot gas generated inside the combustion chamber occurs directly in the gas bag.

[0032] The hybrid gas generator according to the invention provides a controlled outflow of cold gas and hot gas or combustion gas. Since first cold gas and subsequently combustion gas, in particular hot combustion gas, flow into a gas bag, this is particularly gentle on the gas bag of a gas bag module.

[0033] Furthermore, it is possible to design the pressurized gas cylinder, which can also be called a cold gas cylinder, for a specific filling pressure. This results in corresponding weight savings.

[0034] Furthermore, the hybrid gas generator combustion chamber floor with the ring cutting edge and an ignition sleeve, which preferably has a transfer opening, can be designed as a pre-assembled, in particular one-piece, component group, wherein in particular the ring cutting edge and the ignition sleeve are attached to opposite end faces of the combustion chamber floor, which is preferably substantially disc-shaped.

[0035] The ignition sleeve can also include an ignition chamber, preferably containing an ignition mixture, and extend into the combustion chamber in such a way that an annular chamber is formed around the ignition sleeve, which in particular contains a fuel.

[0036] Furthermore, in the event of operation, the ignition chamber can be fluidly connected to the combustion chamber, in particular the annular chamber, and to the mixing chamber and / or a gas bag, preferably via the overflow opening.

[0037] Additionally, it is possible that, in the event of operation, the interior of the pressurized gas container is fluidly connected to the mixing chamber and / or a gas bag via the interior of the ring cutting edge, in particular via its passage opening.

[0038] The pressurized gas container of the hybrid gas generator according to the invention can further comprise a diaphragm holder that encompasses the diaphragm. Preferably, the combustion chamber floor can be supported against the diaphragm holder when pressure is applied to the side of the combustion chamber interior.

[0039] If, during operation or activation, the combustion chamber floor of the hybrid gas generator according to the invention approaches the diaphragm holder of the pressure gas container very closely or is supported by it, the effective outflow cross-section for the gas contained in the pressure gas container could be too small for proper outflow into a mixing chamber or into a gas bag of a gas bag module. To prevent or overcome such a disadvantage, at least one spacer element, in particular in the form of a projection, groove, recess, or depression, can be formed in the combustion chamber floor on the side of the opening device. Alternatively or additionally, the diaphragm holder can have at least one spacer element, in particular in the form of a projection, groove, recess, or depression, on the side facing the opening direction.In other words, both the combustion chamber base, in particular the side of the combustion chamber base's opening device, and / or the diaphragm holder, in particular the side of the diaphragm holder facing the opening direction, can be provided with a structure. This structure, or the at least one spacer element, ensures that the gas from the pressurized gas container can flow out of the pressurized gas container even when the combustion chamber base is in contact with or approaching the diaphragm holder.

[0040] The hybrid gas generator according to the invention is characterized by a small number of components that are easy to construct.

[0041] With regard to a gasbag module, the problem is solved by the features of claim 11. Such a gasbag module according to the invention comprises a hybrid gas generator according to the invention.

[0042] With regard to a vehicle safety system, the problem is solved by the features of claim 12. Accordingly, a vehicle safety system comprises a hybrid gas generator or a gas bag module according to the invention. Similar advantages arise as those already explained in connection with the hybrid gas generator according to the invention.

[0043] The invention is explained in more detail below with reference to exemplary embodiments and the accompanying schematic figures. These show: Fig. 1 a cross-sectional view of a combustion chamber floor of a combustion chamber; Fig. 2 a top view of a combustion chamber floor of a combustion chamber with an opening device; Fig. 3 a sectional view of an igniter-side section of a hybrid gas generator according to the invention with a combustion chamber without combustion chamber-side gas supply (rest state); Fig. 4 a sectional view of an igniter-side section of a further hybrid gas generator according to the invention with a further combustion chamber without combustion chamber-side gas supply (rest state); and Fig. 5 a sectional view of the in Fig. 4 shown partial area of ​​the hybrid gas generator according to the invention with its combustion chamber, but with gas supply on the combustion chamber side (functional case).

[0044] In the following, the same reference numbers are used for identical and identically functioning parts.

[0045] Fig. 1 represents the combustion chamber floor of a combustion chamber. On the combustion chamber floor, on the side facing away from the combustion chamber interior (see Fig. 3) An opening device in the form of an opening mandrel 12 is arranged on surface 11 of the combustion chamber floor 10. In the example shown, the combustion chamber floor 10 and the opening mandrel 12 are formed as a single piece. Furthermore, it is conceivable that the opening device or the opening mandrel 12 is positively and / or materially and / or force-fit connected to the combustion chamber floor 10. The opening mandrel 12 points out from the interior of the combustion chamber (see Fig. 3) away.

[0046] The opening device or opening mandrel 12 is designed as a pyramid tip or pyramid-shaped tip in the illustrated example. Furthermore, it is conceivable to design the opening device as a cross mandrel and / or round mandrel and / or flat mandrel and / or ring cutting edge (see Fig. 4) to train.

[0047] The combustion chamber floor 10 is essentially disc-shaped, but also has a radially projecting collar 13. This serves to connect it to a combustion chamber side wall (see Fig. 3) The collar 13 is formed perpendicular to the surface 11 of the combustion chamber floor 10, which points away from the combustion chamber interior.

[0048] As in Fig. 2, as can be seen in the top view of the combustion chamber floor 10, the combustion chamber floor 10 has a circular shape. The cross-section or shape of the combustion chamber floor 10 is adapted to the combustion chamber or the combustion chamber interior (see Fig. 3) adapted.

[0049] The combustion chamber base 10 has outlet openings 15. In this case, fourteen outlet openings 15 are formed in the combustion chamber base 10. Two outlet openings 15 are arranged opposite each other in relation to the center point of the combustion chamber base 10, namely the opening mandrel 12. A first pair of outlet openings 15 is formed, for example, by an outlet opening 15 located at the 12 o'clock position and another outlet opening 15 located at the 6 o'clock position. All outlet openings 15 are formed on a concentric outer circle 16. The two outlet openings 15 at the 6 and 12 o'clock positions lie on an axis A, which also passes through the opening mandrel 12. The axis A represents a symmetry axis to which the remaining 12 outlet openings 15 are arranged in a mirror-symmetrical manner.

[0050] The outlet opening 15 is designed as a continuous opening from the surface 11 of the combustion chamber floor facing away from the combustion chamber interior to the side 19 of the combustion chamber floor 10 facing the combustion chamber interior. In the example shown, the outlet openings 15 have a circular cross-section. A rectangular, square, elliptical, oval, or polygonal cross-section is also conceivable.

[0051] Straight grooves 18 are formed on side 11 of the opening mandrel 12 in the combustion chamber base 10. These straight grooves 18 serve as spacers. In the illustrated example, 14 grooves 18 are formed in the combustion chamber base 10. Starting from a first concentric inner circle 17, these grooves 18 extend to the second concentric outer circle 16. The outlet openings 15 are formed on the second concentric circle 16. The grooves 18 are also arranged symmetrically with respect to the axis of symmetry A. The straight grooves 18 have rounded ends. A rounded end of each straight groove 18 is arranged between every pair of outlet openings 15. The rounded end is located on the concentric outer circle 16. In a further embodiment of the invention, it is conceivable that the grooves 18 have a curved shape. Furthermore, it is conceivable that the grooves 18 end in the outflow openings 15.In other words, a groove 18 could be connected to an outlet opening 15. In the example shown, the outlet openings 15 are separated from the grooves 18 by their surface area.

[0052] In Fig. Figure 3 shows an igniter-side section of a hybrid gas generator 20 according to the invention, comprising a combustion chamber 30 with a combustion chamber base 10. Regarding identical reference numerals and their meaning, reference is made to the explanations concerning the embodiment according to [reference to relevant figure]. Fig. 1 and Fig. 2 referred.

[0053] The hybrid gas generator 20 has a pressurized gas container 21 with an interior 22. For the sake of clarity, a complete representation of the pressurized gas container 21, i.e., a pressure-tight seal at the top of the pressurized gas container 21, has been omitted. In the Fig. 3. The interior space 22 is already pressurized. This means that there is a pre-compressed gas, preferably cold gas, in the interior space 22. This is in Fig. 3. This can be seen from the fact that a membrane 25, which closes the pressure gas container, is curved downwards, i.e., away from the interior 22, in the example shown. The pressurized gas to be filled into the pressure gas container 21 during the manufacture of the hybrid gas generator 20 can be a pre-compressed gas such as nitrogen, argon, helium or oxygen, or a mixture of two or more of these gases.

[0054] The combustion chamber interior 31 shown is still unpressurized, or rather, only atmospheric pressure prevails there, since the igniter 32 is still in its resting state, i.e., it has not yet been activated or ignited.

[0055] In Fig. Figure 3 further shows an igniter carrier 33 and the igniter 32. The combustion chamber 30 also includes a sleeve-like combustion chamber side wall 34, which delimits the combustion chamber interior 31. In the example shown, the combustion chamber side wall is circular-cylindrical, i.e., the combustion chamber interior shown has a circular cross-section.

[0056] In Fig. Figure 3 shows that the opening pin 12 of the combustion chamber base 10 is located on the surface 11 facing away from the combustion chamber interior 31 and points away from the combustion chamber interior 31. The combustion chamber base 10 is connected to the combustion chamber side wall 34 in such a way that it is flexible when in operation. A material-locking, form-locking, and / or force-locking connection is conceivable for the firm connection of the combustion chamber base 10 to the combustion chamber side wall 34. In the example shown, the combustion chamber base 10 is pressed into the sleeve-like combustion chamber side wall 34. For this purpose, the collar 13 of the combustion chamber base 10 rests against a notch 35 in the combustion chamber side wall 34. The notch 35 secures the combustion chamber floor 10 against complete movement, detachment, or displacement of the combustion chamber floor 10 towards the pressure gas container 21 when subjected to pressure from inside the combustion chamber.

[0057] During the combustion of a fuel located in the combustion chamber interior 31, which for clarity is shown in Fig. As not shown in Figure 3, the pressure in the combustion chamber interior 31 increases such that the combustion chamber floor 10 deflects towards the pressure gas container 21 to be opened, whereby the opening pin 12 opens or pierces the membrane 25 sealing the pressure gas container 21. In other words, in the operating condition, the opening pin 12 moves along the longitudinal axis L towards the membrane 25, without the entire combustion chamber floor 10 moving, since it remains firmly connected to the combustion chamber side wall 34 in the area of ​​its collar 13. Due to the deflection of the combustion chamber floor 10, the opening pin 12, which is located on the combustion chamber floor 10, can perform a lifting movement upwards along the longitudinal axis L.

[0058] The outlet openings 15 of the combustion chamber floor 10 have a sealing cover 28, in particular a dam, on side 19 of the combustion chamber interior 31. In other words, the outlet openings 15 are closed on side 19 of the combustion chamber interior 31 in the resting state by a sealing cover 28, namely the dam shown, wherein the sealing cover 28 is destructive in the operating state such that the combustion chamber 30, in particular the combustion chamber interior 31, is fluidly connected to a mixing chamber 40.

[0059] The pressure gas container 21 includes an opening 23 which is closed with the membrane 25 in the rest state and is destructive in the operating state in such a way that the pressure gas container 21, in particular the interior 22 of the pressure gas container 21, is fluidly connected with the mixing chamber 40.

[0060] In the operating case, the fluid connection from the pressure gas container 21 to the mixing chamber 40 can be formed before the fluid connection from the combustion chamber 30, in particular from the combustion chamber interior 31, to the mixing chamber 40.

[0061] The sealing cover 28 is preferably dimensioned such that, under normal operating conditions, the fluid connection from the pressure gas container 21 to the mixing chamber 40 can be established before the fluid connection from the combustion chamber 30, in particular from the combustion chamber interior 31, to the mixing chamber 40. The sealing covers 28 of the outlet openings 15 are dimensioned with regard to the material and / or material thickness such that the membrane 25, due to the bending of the combustion chamber base 10 and the resulting piercing of the membrane 25 by the opening mandrel 12, is destroyed or burst by the sealing covers 28. The sealing cover 28 can be formed from a disc or foil made of, for example, copper, aluminum, or steel.

[0062] The gas or cold gas from the pressure vessel 21 thus initially flows into the mixing chamber 40 and through side openings 41 into a gas bag (not shown) of a gas bag module. After a further or continuous pressure increase in the combustion chamber 30 or in the combustion chamber interior 31, at least one sealing cover 28 bursts, so that hot gas flows from the combustion chamber 30 into the mixing chamber 40, thus cooling the gas or cold gas from the pressure vessel 21 in the mixing chamber 40.

[0063] The design of the functional pressure of the combustion chamber 30 is preferably to be determined such that even in the event of premature opening or bursting of the closure cover 28, the pressure in the combustion chamber interior 31 is sufficient to cause the combustion chamber floor 10 to bend towards the membrane 25, so that the opening pin 12 opens or pierces the membrane 25 which closes the pressure gas container 21.

[0064] The pressurized gas container 21 further comprises a diaphragm holder 24, which encompasses the diaphragm 25. The diaphragm holder is attached to and connected with the opening-side wall 23 of the pressurized gas container 21. The diaphragm 25 is held in place by the diaphragm holder 24. When pressure is applied to the side 19 of the combustion chamber interior 31, the combustion chamber floor 10 can preferably be supported by the diaphragm holder 24.

[0065] In the membrane holder 24, at least one spacer element, in particular in the form of a projection and / or a groove and / or a recess and / or a depression, can be formed on the surface 26 facing away from the pressure gas container 21. The formation of the spacer element in the membrane holder 24 can be additional to or alternative to the spacer element that is formed in the combustion chamber base 10 (see Fig. 2) is formed. The formation of one or more spacer elements in the combustion chamber base and / or in the membrane holder ensures that the gas or cold gas from the pressure gas container 21 can flow out of the pressure gas container 21 even when the combustion chamber base 10, in particular surface 11 of the combustion chamber base 10, is in contact with the membrane holder 24, in particular surface 26. The described spacer elements (grooves 18 in the combustion chamber base 10) thus prevent the effective outflow cross-section for the gas or cold gas from the pressure gas container from being too small for proper outflow. A controlled outflow, namely a pre-emptive outflow of the gas followed by a subsequent outflow of combustion gas from the combustion chamber 30, which is particularly gentle on the expansion and stress of a gas bag, is therefore achieved with the hybrid gas generator according to the invention.

[0066] In Fig. Figure 4 shows an igniter-side section of a further hybrid gas generator 20 according to the invention, comprising a further combustion chamber 30 with a combustion chamber base 10, without gas being supplied to the combustion chamber side, i.e., in its resting state. Regarding identical reference numerals and their meaning, reference is made to the explanations concerning the embodiment according to [reference to relevant figure]. Fig. 1, Fig. 2 and Fig. 3 referred.

[0067] The hybrid gas generator 20 of the Fig. 4 is basically like the hybrid gas generator 20 of the Fig. 3, but differs mainly in the design and additional functions of the combustion chamber floor 10. In the Fig. 4. The combustion chamber floor 10 has an annular cutting edge 44, which is centrally located on the surface 11 facing away from the interior of the combustion chamber, essentially parallel to the longitudinal axis L, and is formed integrally with the combustion chamber floor 10. The annular cutting edge 44 can also be designed as a separate component firmly connected to the combustion chamber floor 10. The annular cutting edge 44 is designed as a hollow cylinder with a circular cross-section and has a cutting edge at its end face, which faces away from the surface 11 facing away from the interior of the combustion chamber. This cutting edge is designed such that, in the event of operation, the diaphragm 25 sealing the pressure gas container 21 can be opened or destroyed by the annular cutting edge 44.

[0068] The ring cutting edge 44 additionally has several through-holes 47 at the end region facing away from its cutting edge, wherein all through-holes 47 are arranged at the same axial height of the ring cutting edge 44 such that in the event of a bending (functional case see Fig. 5) of the combustion chamber base 10 and thus an axial stroke movement of the ring cutting edge 44 towards the diaphragm holder 24, the passage openings 47 are not covered by the diaphragm holder 24, i.e., the entire flow area of ​​all passage openings 47 remains unobstructed during operation. A single passage opening 47 is technically sufficient, although preferably two to eight, and in particular four to six, passage openings 47 may be present.

[0069] In Fig. 4. The combustion chamber base 10 has an integrally formed ignition sleeve 45 on its side 19 facing the combustion chamber interior 31. This ignition sleeve is designed as a hollow cylinder with a circular cross-section, essentially parallel to the longitudinal axis L. The ignition sleeve 45 can also be designed as a separate component, firmly connected to the combustion chamber base 10. The ignition sleeve 45 has an outer diameter approximately twice that of the ring cutting edge 44 and, like the latter, is arranged concentrically with respect to the longitudinal axis L.

[0070] The ignition sleeve 45 extends from the side 19 of the combustion chamber base 10, which faces the combustion chamber interior 31, almost through the entire combustion chamber 30 or the combustion chamber interior 31. Its open end, which is opposite side 19 of the combustion chamber base, is placed on the igniter 32, specifically on its axial end face, or at least partially surrounds it. The ignition sleeve 45 is positioned relative to the igniter 32 such that the igniter 32 closes the open end of the ignition sleeve 45. Together, the ignition sleeve 45 and the igniter 32 define a cylindrical ignition chamber 48, which is at least partially filled with an ignition mixture 43. Geometrically speaking, this configuration of the ignition chamber 48 results in an annular chamber 49 around it, which can be considered the effectively usable combustion chamber 30. The ring chamber 49 or combustion chamber 30 is, at least partially, filled with fuel 42.The propellant 42 and the ignition mixture 43 are known pyrotechnic solid propellants which may be in common shaped bodies, such as pressed tablets, granules or extruded bodies, whereby the shape, size or chemical composition of the propellant 42 and the ignition mixture 43 may be identical or different.

[0071] The ignition sleeve 45 additionally has at least one overflow opening 46 at its end facing the igniter 32, wherein the at least one overflow opening 46 is located in the Fig. In the resting state shown in Figure 4, the ignition sleeve 45 is positioned such that it is covered by the igniter 32, in particular by its radial end face, in such a way that no parts of the ignition mixture 43 can pass through the overflow opening 46 from the ignition chamber 48 into the annular chamber 49. The at least one overflow opening 46 is, so to speak, closed off by the igniter 32 on the ignition chamber side, such that immediately after ignition of the ignition mixture 43, no combustion gas or hot gas forming can yet pass through the at least one overflow opening 46 into the annular chamber 49. Only after the ignition mixture 43 has burned continuously, as described in more detail below, is the ignition sleeve 45 moved away from the igniter 32, such that combustion gas or hot gas can flow through the at least one overflow opening 46 into the annular chamber 49 as intended (see Figure 4). Fig. 5).

[0072] The at least one overflow opening 46 can also be additionally closed from the ignition chamber 48 side with a bursting foil or tamping (not shown), which opens at a predefined pressure in the ignition chamber 48 to allow combustion gas to flow through the at least one overflow opening 46 into the annular chamber 49. The at least one overflow opening 46 can also be positioned axially further away from the igniter 32 than shown in the Fig. 4 shown, whereby it can then no longer be sealed by the igniter 32, but exclusively by a bursting foil or tamping not shown.

[0073] For Fig. 4 and Fig. 5 applies, that, just as in Fig. 2, the combustion chamber floor 10 is so firmly connected to the combustion chamber side wall 34 in the areas of its formed collar 13 that the combustion chamber floor 10 is bendable when in operation. Regarding the firm connection of the combustion chamber floor 10 to the combustion chamber side wall 34, a material-locking and / or form-locking and / or force-locking connection is conceivable. In the case of the Fig. 4 and Fig. 5 the combustion chamber floor 10 is materially connected to the combustion chamber side wall 34, in particular welded, so that when subjected to an internal combustion chamber pressure, a complete movement or detachment or displacement of the combustion chamber floor 10 in the direction of the pressure gas container 21 is not possible.

[0074] In Fig. 4. The combustion chamber floor 10 is slightly pre-shaped or pre-bent towards the igniter 32, towards the side of the combustion chamber interior 31. In other words, the angle between the surface section of the combustion chamber floor 10 having the outlet openings 15 and the collar 13 of the combustion chamber floor is less than 90°. The combustion chamber floor 10 of Fig. 4 is therefore biased downwards, in the direction of the igniter 32, which in the case of operation (see Fig. 5) has an advantageous effect, as it allows for a larger stroke distance or stroke movement of the ring cutting edge 44.

[0075] In Fig. 5 is the igniter-side section of the hybrid gas generator 20 according to the invention. Fig. Figure 4 shows the combustion chamber with gas supply, i.e., in its functional state. Regarding the corresponding reference numerals and their meaning, reference is made to the explanations concerning the embodiment according to... Fig. 1, Fig. 2, Fig. 3 and Fig. 4 referred.

[0076] The combustion chamber floor 10 of the Fig. 5 is in the direction of the opening 23 of the pressure gas container 21, i.e. in the opposite direction to how it is in Fig. 4 is pre-bent, deformed, or bent. In other words, the angle between the surface section of the combustion chamber floor 10 having the exhaust openings 15 and the collar 13 of the combustion chamber floor 10 is greater than 90°. The exhaust openings 15 are no longer closed by the cover 28 (see Fig. 4), but is already opened or destroyed by the pressure arising in the combustion chamber interior 31, so that the combustion chamber interior 31 is fluidly connected to the mixing chamber 40 via the outflow openings 15.

[0077] In the Fig. 5 is the end of the ring cutting edge 44, which has the cutting edge positioned in an area of ​​the pressure gas container 21, which in the rest state (see Fig. 4) is closed by the membrane 25. In other words, the position of the ring edge 44 of the Fig. 5, that the membrane 25 of the pressure gas container 21 is destroyed and the pressure gas container 21 is open, so that the stored gas or cold gas can flow out of the pressure gas container 21. In this case, the pressure gas container 21 is fluidly connected to the mixing chamber 40 via the passage openings 47 of the hollow cylindrical ring cutting edge 44.

[0078] Fig. Figure 5 shows a position of the ignition sleeve 45 in which it is raised towards the opening 23 of the pressurized gas container 21, i.e., away from the igniter 32, by the deformation of the combustion chamber base 10 described above, to which it is firmly connected. In this position, the ignition sleeve 45 is positioned so far away from the igniter 32 that at least one overflow opening 46 of the ignition sleeve 45 is exposed. In other words, in Fig. 5 the ignition sleeve 45 is positioned such that the ignition chamber 48 of the ignition sleeve 45 is fluidly connected to the combustion chamber interior 31 via at least one overflow opening 46.

[0079] The following describes the operating principle of the hybrid gas generator 20. Fig. 4 and Fig. 5 described. In other words, it will now be explained how the hybrid gas generator 20 is brought from its standby state (see Fig. 4) into the functional case (see Fig. 5) is brought.

[0080] After the in Fig. When the hybrid gas generator 20 shown in Figure 4 is activated, i.e., when its igniter 32 receives an electrical activation signal for ignition, the igniter opens at its front face to expel hot gases and / or hot particles to ignite the adjacent ignition mixture 43. The pressure generated in the ignition chamber 48 then lifts the ignition sleeve 45 away from the igniter 32, essentially parallel to the longitudinal axis L, to such an extent that at least one overflow opening 46 is released, allowing further hot gas and / or hot particles from the ignition chamber 48 to flow into the annular chamber 49 to ignite the propellant 42 located there and to cause a pressure increase in the annular chamber 49.

[0081] Since all three components, ignition sleeve 45, combustion chamber base 10, and ring cutting edge 44, are firmly connected to one another, the aforementioned lifting of the ignition sleeve 45 causes the combustion chamber base 10 to bend, thereby positioning or lifting the ring cutting edge 44 towards the pressure gas container 21 or its sealing membrane 25. The lifting movement of the ring cutting edge 44 is designed such that the membrane 25 sealing the pressure container 21 is reliably opened or pierced by the ring cutting edge 44, allowing gas or cold gas from the pressure gas container 21 to flow into the interior of the hollow cylindrical ring cutting edge 44 and through its openings 47 first into the mixing chamber 40 and then into a gas bag (not shown), through the side openings 41 of the hybrid gas generator 20. The stroke movement of the ring cutting edge 44 can be achieved solely by the pressure increase in the ignition chamber 48, but the pressure increase in the ring chamber 49 also contributes to the stroke movement of the ring cutting edge 44, up to its end position (see Fig. 5) can contribute.

[0082] After the propellant 42 has been ignited, as described above, and a correspondingly predefined pressure has built up in the annular chamber 49, the sealing cover 28 is opened or destroyed so that hot gas can flow through the outlet openings 15 of the combustion chamber floor 10 into the mixing chamber 40 in order to bring the combustion chamber 30, or the combustion chamber interior 31, into fluid contact with the mixing chamber 40 and a gas bag (not shown) through the side openings 41 of the hybrid gas generator 20.

[0083] The hybrid gas generator 20, in particular by means of the sealing cover 28, is designed such that, in terms of timing, the fluid connection from the pressure gas container 21 to the mixing chamber 40 is established before the fluid connection from the combustion chamber 30 to the mixing chamber 40. This allows only pure cold gas from the pressure gas container 21 to flow initially through the mixing chamber 40 into the outer area of ​​the hybrid gas generator 20 to enable gentle expansion of the gas bag. Subsequently, hot gas from the combustion chamber 30 is mixed with cold gas from the pressure gas container 21 before flowing into the gas bag to ensure its complete expansion. Reference symbol list 10 Combustion chamber floor 11. Area pointing away from the combustion chamber interior 12 Opening mandrels 13 collars 15 Outlet opening 16 outer circle 17 inner circle 18 groove 19th page combustion chamber floor 20 Hybrid gas generator 21 pressurized gas containers 22 Interior of pressurized gas container 23 Opening of pressurized gas container 24 membrane holders 25 Membran 26 Area Membrane Holder 28 Closure cover 30 combustion chamber 31 Combustion chamber interior 32 lighters 33 lighter carriers 34 Combustion chamber side wall 35 notches 40 Mixing chamber 41 Side opening 42 Fuel 43 Firelighters 44 ring cutting edge 45 Ignition sleeve 46 Overflow opening 47 Passage opening Ring cutting edge 48 Ignition chamber 49 ring chamber Axis L Longitudinal axis

Claims

[1] Hybrid gas generator (20) for a vehicle safety system with a pressurized gas container (21) an opening (23) which, in a rest state of the hybrid gas generator (20), is closed with a membrane (25) which, in the case of operation, can be destroyed by an opening device such that the pressure gas container (21) is fluidly connected to a mixing chamber (40) and to a combustion chamber (30) with the opening device for the pressure gas container (21), wherein the combustion chamber (30) comprises a sleeve-like combustion chamber side wall (34) defining a combustion chamber interior (31) and a combustion chamber bottom (10), wherein the opening device is arranged on a surface (11) of the combustion chamber bottom (10) pointing away from the combustion chamber interior (31) and the combustion chamber bottom (10) is firmly connected to the combustion chamber side wall (34) in such a way that the combustion chamber bottom (10) is bendable in the case of operation, characterized by, that a fuel (42) is located in the combustion chamber (30), which burns during operation, and that at least one outlet opening (15) is formed in the combustion chamber floor (10), which is closed with a closure cover (28) on the side of the combustion chamber interior (31) when the hybrid gas generator (20) is at rest, wherein the closure cover (28) is destructible during operation in such a way that the combustion chamber (30) is fluidly connected to the mixing chamber (40), wherein In the event of operation, the fluid connection from the pressure gas container (21) to the mixing chamber (40) can be formed before the fluid connection from the combustion chamber (30) to the mixing chamber (40). [2] Hybrid gas generator (20) according to claim 1, characterized by , that the membrane (25) of the pressure gas container (21) can be destroyed by an opening mandrel (12) or a ring cutting edge (44) of the opening device. [3] Hybrid gas generator (20) according to claim 2, characterized by, that the combustion chamber floor (10) is formed as a pre-assembled component group with the ring cutting edge (44) and an ignition sleeve (45), wherein the ring cutting edge (44) and the ignition sleeve (45) are attached to opposite end faces of the combustion chamber floor (10). [4] Hybrid gas generator (20) according to claim 3, characterized by , that the ignition sleeve (45) comprises an ignition chamber (48) containing an ignition mixture (43) and extends into the combustion chamber (30) in such a way that an annular chamber (49) is formed around the ignition sleeve (45), which contains the propellant (42). [5] Hybrid gas generator (20) according to any one of the preceding claims, characterized by, that the closure cover (28) is dimensioned such that, in the event of operation, such a pressure can be built up in the combustion chamber (30) that the diaphragm (25) of the pressure gas container (21) can be destroyed by bending the combustion chamber floor (10) in the direction of the diaphragm (25) with the opening device. [6] Hybrid gas generator (20) according to any one of the preceding claims, characterized by , that the closure cover (28) is dimensioned such that, in the event of operation, the combustion chamber (30) is fluidly connected to the mixing chamber (40). [7] Hybrid gas generator (20) according to claim 4, characterized by , that in the case of operation the ignition chamber (48) is fluidly connected to the combustion chamber (30) and to the mixing chamber (40). [8] Hybrid gas generator (20) according to claim 2, characterized by , that in the case of operation the interior (22) of the pressure gas container (21) is fluidly connected to the mixing chamber (40) via the interior of the ring cutting edge (44). [9] Hybrid gas generator (20) according to any one of the preceding claims, characterized by , that the pressure gas container (21) has a membrane holder (24) which includes the membrane (25), wherein the combustion chamber floor (10) can be supported by a pressure on the membrane holder (24) when pressure is applied to the side of the combustion chamber interior (31). [10] Hybrid gas generator (20) according to claim 9, characterized by , that in the membrane holder (24) on the surface (26) facing away from the pressure gas container (21) at least one spacer element in the form of a projection or a groove or a channel or a recess or a depression is formed. [11] Gasbag module with a hybrid gas generator (20) according to one of the preceding claims. [12] Vehicle safety system with hybrid gas generator (20) or a gas bag module according to any of the preceding claims.

Citation Information

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