The present invention relates to a pyrotechnic agent.
Pyrotechnic agents within the meaning of the invention are substances or mixtures of substances that can produce a pyrotechnic effect.
In particular the present invention provides a pyrotechnic agent that can be used as a thermal early-ignition agent.
Areas of application of such thermal early-ignition agents are for example safety systems, preferably thermal safety fuses in gas generators or separators for batteries. Such safety systems are in turn preferably used in vehicles.
Thermal early-ignition agents are pyrotechnic substances or mixtures that inter alia have the task of igniting in a controlled manner the mixtures of the gas generator, which as a rule produce thermally very stable gas, in the event of a vehicle fire.
Another example of application of thermal early-ignition agents is their use as a pyrotechnic charge in separators, preferably for battery terminals. These separators are designed to interrupt the power supply in the event of a fire, in particular a vehicle fire, or in the event of a vehicle accident, in which the gas generator is triggered.
As thermal early-ignition agents there are used for example nitrocellulose, propellant charge powders derived therefrom, or the mixtures based on nitrotriazolone and guanidine nitrate, described in patent application DE 197 30 873 A1. These mixtures have ignition temperatures of ca. 160° C., and in the case of nitrocellulose have inadequate long-term storage stability.
The object of the present invention was to provide a pyrotechnic agent with an ignition temperature of around 180° C. and with satisfactory long-term storage stability. A further object of the present invention was to provide a pyrotechnic agent that can be used as a thermal early-ignition agent for gas generators in vehicle safety systems. Yet a further object of the present invention was to provide a pyrotechnic agent that can be used in separators for battery terminals.
According to the invention this object is surprisingly achieved by the features of the main claim. Preferred embodiments are disclosed in the sub-claims. In this connection, according to the invention azotetrazolates are used as components. In particular aminoguanidine-5,5′-azotetrazolate (C4H14N18), abbreviated to AGATZ, and guanidine-5,5′-azotetrazolate (C4H12N16), abbreviated to GATZ, are used as azotetrazolate component.
The azotetrazolate component can be used either alone or in mixtures with one another and/or with further components. The structural formulae of AGATZ and GATZ are as follows:
Aminoguanidine-5,5′-azotetrazolate (C4H14N18, AGATZ)
Guanidine-5,5′-azotetrazolate (C4H12N16, GATZ)
The deflagration temperature of pure AGATZ is 209° C., and of GATZ is 240° C.
It was surprisingly found that with mixtures of AGATZ and/or GATZ and/or selected components, the deflagration temperatures can be controlled in the range from 165° C. to 195° C. and the deflagration temperatures of the mixture may be lower than those of the individual components.
For early-ignition agents deflagration temperatures below 200° C. are particularly useful. The pyrotechnic agents according to the invention meet this requirement, and have excellent long-term storage stability.
The following can be used as additives:
The production and processing is carried out according to conventional processes known per se. These include for example kneading, extrusion, extrusion moulding, tabletting or granulation.
The present invention provides in particular:
The invention is described in more detail by means of the following examples, without however being restricted thereto:
The compositions of 27 different mixtures of the pyrotechnic agent are listed in Table 1. The components were weighed out in the specified amounts (amounts refer to weight percent) into plastics containers and homogenised for 30 minutes in a tumble mixer.
The deflagration temperatures and friction and impact sensitivities of the mixtures are given in Table 2. The friction and impact sensitivities were measured according to the methods of the Bundesanstalt für Materialforschung (BAM) (Federal Institute for Materials Testing), while the deflagration temperatures were measured by thermo-gravimetric analysis (Mettler Company) at a heating rate of 10° C. per minute.
The weight losses and deflagration temperatures after thermal loading (24 hours, 125° C. and 400 hours, 110° C.) of some of the mixtures chosen from the examples are summarised in Table 3. The measurement of the weight loss was carried out in a similar way to the Holland Test. The deflagration temperatures were measured by thermo-gravimetric analysis (Mettler Company) at a heating rate of 10° C. per minute.
After 400 hours only slight weight losses of 0.1 to 0.7 wt. % are detected, and there are no significant changes in the deflagration temperature after thermal loading.
These results show that the specific pyrotechnic agents according to the invention have deflagration temperatures in the range from 172° to 191° C. and should be regarded as stable according to the requirements of the automobile industry.
In addition the following mixtures have proved to be particularly advantageous, in particular also for use in separators for battery terminals:
Number | Date | Country | Kind |
---|---|---|---|
10 2005 025 746.1 | Jun 2005 | DE | national |
10 2006 013 622.5 | Mar 2006 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2006/062862 | 6/2/2006 | WO | 00 | 12/5/2008 |
Publishing Document | Publishing Date | Country | Kind |
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WO2006/128910 | 12/7/2006 | WO | A |
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Number | Date | Country | |
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20090133787 A1 | May 2009 | US |