Explosive and thermic compositions or charges – Structure or arrangement of component or product – Solid particles dispersed in solid solution or matrix
Reexamination Certificate
2001-04-10
2003-05-13
Hardee, John (Department: 1751)
Explosive and thermic compositions or charges
Structure or arrangement of component or product
Solid particles dispersed in solid solution or matrix
C149S038000
Reexamination Certificate
active
06562160
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention pertains to the field of automobile inflatable safety systems and more particularly to propellants for hybrid inflator devices.
2. Brief Description of the Prior Art
Currently, gun-type propellants are used in hybrid inflators or airbag safety systems for vehicles and other personnel transportation devices. U.S. Pat. Nos. 5,602,361, 5,616,883, and 5,695,216 describe airbags devices that mix gases generated by gun type propellants with an inert gas and oxygen to inflate airbags under certain conditions. More particularly, carbon monoxide (CO) and hydrogen (H
2
) in the propellant gases are converted by the oxygen to carbon dioxide (CO
2
) and water. The burning of the gun type propellant and the oxidation of the CO
2
and H
2
provide heat, which drives the expansion of the compressed gases to inflate the airbag. This results in gases, which are non-toxic in nature, which is an important safety feature for airbag devices due to their use in close proximity to persons. Airbag propellants must also maintain their physical properties for use in vehicle systems where they will be subjected to harsh physical and thermal stresses.
However, the gun type propellants described in the U.S. patents above contain low molecular weight plasticizers, which over time, migrate within the propellants. This results in not only changes to the propellant composition, which changes the properties of the propellant, but also possible ballistic changes. These ballistic changes are caused by a decrease in the propellant surface area from the propellant grains sticking together due to a plasticizer-rich layer on the surface of the grains.
U.S. Pat. No. 6,009,810 describes an airbag propellant designed to alleviate this problem. The patent describes an airbag propellant that is plasticizer-free, while maintaining the good physical and mechanical characteristics necessary in commercial airbag systems. However, the propellant described in this patent also produces a pungent odor when used in the newer dual-stage hybrid inflators, which makes it problematic for such commercial uses.
Due to the limitations of the current technology described above, it would be desirable to provide an airbag propellant that maintained its properties, thereby increasing its shelf life, as well as produced no pungent odor. Such an airbag propellant would also need to produce nontoxic gases during operation and provide physical characteristics which make it suitable for vehicle systems subjected to harsh stresses.
SUMMARY OF THE INVENTION
Accordingly, it is an object of this invention to provide a new propellant for hybrid inflator systems for safety airbags.
It is a further object of this invention to provide a new airbag propellant having a long shelf life.
It is still a further object of this invention to provide a new airbag propellant that does not provide a significant decrease in performance after undergoing thermal shock and heat aging.
It is still a further object of this invention to provide a new airbag propellant having no pungent odor upon ignition.
This invention accomplishes these objectives and other needs related to airbag propellants by providing an airbag propellant composition comprising from about 70 weight percent to about 82 weight percent Cyclotrimethylenetrinitramine (RDX), from about 10 weight percent to about weight percent Cellulose Acetate Butyrate (CAB), from about 6 weight percent to about 9 weight percent Acetyl Triethyl Citrate (ATEC), from about 2 weight percent to about 4 weight percent Hydroxypropyl Cellulose (HPC), from about 0.5 weight percent to about 1 weight percent vVestenamer, and from about 0.3 weight percent to about 0.5 weight percent Ethyl Centralite (EC).
DESCRIPTION OF THE PREFERRED EMBODIMENT
The present invention is an airbag propellant composition designed to be used as a substitute for the current gun-type propellants used in hybrid inflators for airbag safety systems in vehicles. The present invention is designed to have a long shelf life, high resistance to performance degradation after thermal aging testing and excellent physical properties such as excellent strength, insensitivity, and safety. The present invention is also designed to be fully operative for use in hybrid inflators for airbag safety systems without emitting a pungent odor during use. The present invention achieves these goals by taking Cyclotrimethylenetrinitramine (RDX) and combining it with a polymer binder, an inert plasticizer, a stabilizing and anti-oxidizing material, and unique processing aids.
In describing the present invention, all percentages given below are percentages by weight. The airbag propellant of the present invention comprises from about 70 percent to about 82 percent RDX particles with from about 10 percent to about 15 percent of a polymer binder, and from about 6 percent to about 9 percent of an inert plasticizer. From about 0.3 percent to about 0.5 percent of a material that acts as a stabilizer and an anti-oxidant is used as well as from about 2 percent to about 4 percent of Hydroxypropyl Cellulose and from about 0.5 percent to about 1 percent of a polymeric processing aid.
The particle size of RDX is directly proportional to its burning rate. The RDX particles used in the present invention are small in nature in order to select the proper burning rate for the propellant and are selectable by one skilled in the art. A preferable range of sizes of the RDX particles comprises from about 2 microns to about 12 microns, with a particle size of about 7 microns being most preferable.
The use of from about 2 percent to about 4 percent of Hydroxypropyl Cellulose is important to the operation and physical properties of the invention. In the most preferable embodiment of the invention, about 3 percent Hydroxypropyl Cellulose is used. The Hydroxypropyl Cellulose, along with the polymeric processing aid described more fully below, are designed to replace the Nitrocellulose normally used in LOVA type propellants. Nitrocellulose was a critical element of those LOVA propellants as a binder and processing aid. However, when used as an airbag propellant, the Nitrocellulose causes the propellant to have very poor shelf life because of its tendency to decompose when exposed to the extreme heat requirements of airbag propellant thermal testing. When the Nitrocellulose breaks down, the properties of the propellant change. This has an adverse affect upon the operation of the propellant, and, due to the safety impact related to the above described use, it is unacceptable for such use. The Hydroxypropyl Cellulose and polymeric processing aid are designed to replace the Nitrocellulose in function and provide a propellant with excellent shelf life.
FIG. 1
shows how the properties of the present invention remain nearly constant, even when exposed to dramatic heat and pressure changes over time.
FIG. 1
shows three curves. The first, relates to the ballistic properties of the present invention initially. The second, relates to the present invention after subjecting it to 200 cycles of increasing temperature to 107 degrees C. and decreasing the temperature to −40 degrees C. for thirty minutes each. The third relates to the present invention after it was exposed to 107 degrees C. for 400 hours. As one can see, all three curves are nearly identical, showing the excellent performance of the present invention after being exposed to thermal stresss.
As noted above, from about 0.5 percent to about 1 percent of a polymeric processing aid is used in the present invention. The most preferred embodiment of the invention uses approximately 0.675 percent of a polymeric processing aid. Without a polymeric processing aid, the propellant is difficult to mix and extremely difficult to extrude. The polymeric processing aid also improves the strand integrity of the propellant, which makes it easier to handle during the cutting process. The most preferred polymeric processing aid for the present invention is Vestenamer 6213, which is a polyoctena
Hardee John
Homer Mark
The United States of America as represented by the Secretary of
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