Tubular gas generator

Details Tubular gas generator Tubular gas generator

2003-05-19

2004-12-28

Keith, Jack (Department: 3641)

Ammunition and explosives

Jacketed or cartridge gas generator

C102S531000, C102S275100, C102S275900

Reexamination Certificate

active

06834594

ABSTRACT:

TECHNICAL FIELD
This invention relates to a gas generator for use in a vehicle occupant restraint system.
BACKGROUND OF THE INVENTION
Gas generators are known in the art which comprise a tubular housing of a pressure-resistant material and a propellant strand incorporated in the housing, at least one channel being provided between the envelope and the propellant strand so as to extend in an axial direction.
Such tubular gas generator is already known from DE-A1 100 09 417. In the known gas generator, the axially extending channels are formed by a propellant charge which has a central bore and is cross-shaped in cross-section, the propellant charge being surrounded by a shrinkable tube. For insulation purposes, the shrinkable tube may also be disposed on the outside of the tubular housing.
EP 0 995 645 A2 describes a tubular gas generator, in which a propellant strand provided with radially extending extensions is inserted in a tubular housing of pressure-resistant material, the radial extensions resting against the inner wall of the housing. Due to the special geometry of the propellant strand channels are thus formed, which extend in axial direction between the respective radial extensions so as to pass on the pressure wave generated by the igniter. To ensure a rather complete deflagration of the solid propellant, the bores incorporated in the housing are at least partly insulated.
DE-A1 39 32 576 describes a gas-generating means for a gas generator for ejecting ammunition or for filling air bags, which has a slowly burning solid propellant in the form of a tube or strand and an explosive coating resting against a longitudinal side of the solid propellant. The solid propellant can have a hollow cylindrical shape, so that inside the propellant strand an axially extending channel is formed. The explosive coating then likewise lies inside this channel. Alternatively, it is suggested to provide the solid propellant with an envelope. In this case, the cross-section of the solid propellant is star-shaped.
The tubular gas generators provided for use in vehicle occupant restraint systems must have reaction times within the range of few milliseconds. To this end, a deflagration of propellant must be ensured, which takes place completely and in the shortest time possible. It must therefore be ensured that the propellant is ignited rather simultaneously over the entire length of the gas generator. Ignition is mostly effected via a gas pressure wave generated by an ignition element, which propagates along the channels extending in axial direction in the tubular gas generator. To compensate energy losses of the pressure wave and to ensure a uniform ignition, the propellant usually is also provided with an explosive coating, which is activated by the pressure wave.
In a tubular gas generator, i.e. a gas generator with a ratio of length to diameter (aspect ratio) of larger than 10, preferably larger than 50, channels usually extending in axial direction are formed due to this special ignition mechanism. For forming these channels, complicated propellant geometries had to be used so far. Since the stability of the propellant geometry must be ensured during the lifespan of the vehicle, it is not possible to employ any kind of pyrotechnical propellant charges. In EP 0 995 645 A2, for instance, the use of a fiber-reinforced pyrotechnical propellant is regarded as advantageous. The embodiment of a hollow cylindrical propellant strand with internal explosive coating, which is described in DE 39 32 576 A1, is difficult to realize in technical terms and leads to insufficient deflagration properties.
In comparison with that, the invention provides a tubular gas generator of a simple structure and inexpensive to produce, for the production of which known techniques can be used.
BRIEF SUMMARY OF THE INVENTION
According to the invention, a gas generator comprises a tubular housing of a pressure-resistant material and a propellant strand which is incorporated in the housing and provided with an envelope. At least one channel is provided between the envelope and the propellant strand so as to extend in an axial direction. The propellant strand has a substantially circular (i.e. round) cross-section and the envelope has a polygonal cross-section.
For the purposes of the invention, propellant strands of substantially circular or round cross-section are meant to include those cylindrical propellant strands which in contrast to the circular shape are oval or flattened on their longitudinal side.
Providing a substantially circular propellant strand provides for using known extrusion methods as they are commonly used for instance in the production of single- and multi-hole powders. Thus, all extrudable propellants can be used as well. On the other hand, the production of dimensionally stable envelopes with more complex, polygonal cross-sections is possible without any major technical effort, for instance, be extruding suitable materials. By fitting a substantially circular cylindrical propellant strand into a polygonal, preferably triangular or tetragonal envelope, there is also ensured the formation of the axially extending channels for passing on the gas pressure wave generated by the igniter. On the other hand, the dimensional stability of the propellant strand and of the envelope distinctly reduces the risk of breakage of the strand and hence the risk of failure of the ignition mechanism.
To increase the compressive strength, the tubular housing may comprise a plurality of layers. Preferably, the housing has an inner layer as well as an outer layer of plastics as well as a middle layer of aluminum, which is connected with the inner layer and the outer layer via adhesion-promoting intermediate layers. Such layered structure ensures a particular compressive strength and flexibility at the same time. Another possibility consists in providing a two-layer housing with an outer plastic layer and an inner aluminum layer. In this case, the aluminum layer may constitute a thin metal film with a layer thickness of less than 0.1 mm, preferably between 0.08 and 0.1 mm, and perform the function of an insulation. The aluminum film will then also seal the bores incorporated in the housing.
The multilayer housing can be produced by coextruding the above-mentioned materials. The ratio of length to diameter of the housing is at least 10, preferably at least 50, and particularly preferably at least 100.
The propellant strand preferably has a cross-section in the form of a circular ring, i.e. the strand constitutes a hollow cylinder. The production of such hollow cylindrical solid propellants by extrusion is known already and possible without any technical difficulties. For producing the propellant strand, known pyrotechnical solid propellants can be used, as they are described for instance in EP-A2 995 645. There may be used the composite propellants which are known from DE-A1 44 46 976 and comprise a thermoplastic binder, possibly a plasticizer and an oxidizer. The use of these composite propellants is advantageous due to their higher elasticity. For the purposes of the invention, the propellant strand can furthermore be divided in segments which may preferably have a length of about 3 to 10 cm.
On at least one of its surfaces adjoining the axially extending channels between the envelope and the propellant strand, the propellant strand may be provided with a coating of an ignition mixture. As ignition mixture, an aluminized mixture of boron and potassium nitrate can be used, for instance. The ignition mixture is activated by the gas pressure wave generated by the igniter and ensures a complete ignition of the propellant strand over the entire length of the tubular gas generator. Preferably, however, the propellant itself can sufficiently be activated by the pressure wave.
The envelope surrounding the propellant strand has at least one layer of an extrudable material. This material may for instance be selected from brass, aluminum, plastics or paper. The envelope is dimensionally stable under ambient conditions. Under the i

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