초록 ▼

A propane fueled combustor for providing a controlled heat flux environment of twenty to two hundred kilowatts per square meter. The combustor has the capability of generating a repeatable and quantifiable environment in which to evaluate a response of an energetic material to a fast cook off hazard

A propane fueled combustor for providing a controlled heat flux environment of twenty to two hundred kilowatts per square meter. The combustor has the capability of generating a repeatable and quantifiable environment in which to evaluate a response of an energetic material to a fast cook off hazard, such as a liquid fuel fire.

대표청구항 ▼

1. A combustion apparatus for providing a controlled heat flux for testing a test specimen containing an energetic material comprising: (a) a source of air for providing a stream of air at a fixed mass flow rate;(b) an air inlet duct having said source of air positioned at one end thereof;(c) a mani

1. A combustion apparatus for providing a controlled heat flux for testing a test specimen containing an energetic material comprising: (a) a source of air for providing a stream of air at a fixed mass flow rate;(b) an air inlet duct having said source of air positioned at one end thereof;(c) a manifold positioned at the other end of said air inlet duct, said manifold having a fuel injection system comprising a plurality of equally spaced apart fuel injectors located within said manifold which form a ring around said manifold, wherein said plurality of fuel injectors of said fuel injection system inject a liquid fuel into said stream of air forming a flammable mixture;(d) a combustion chamber having one end thereof connected to said manifold to receive said flammable mixture, said combustion chamber having an inside diameter that is larger than an inside diameter for said air inlet duct, wherein the inside diameter of said combustion chamber is eighteen inches and the inside diameter of said air inlet duct is approximately five inches; and(e) a fuel ignition device positioned in proximity to said flammable mixture, said fuel ignition device igniting said flammable mixture generating said controlled heat flux within said combustion chamber to test said test specimen which includes said energetic material. 2. The combustion apparatus of claim 1 wherein said source of air comprises a five horsepower fan motor and fan located within a fan and motor housing, said fan motor and fan delivering said stream of air through said air inlet duct at a mass flow rate of approximately one pound per second. 3. The combustion apparatus of claim 1 wherein said air inlet duct is fabricated from five inch diameter stainless steel and said combustion chamber is fabricated from eighteen inch diameter stainless steel. 4. The combustion apparatus of claim 1 further comprising a layer of insulation mounted on the outer side of said combustion chamber, said layer of insulation enhancing temperature control of said flammable mixture within said combustion chamber. 5. The combustion apparatus of claim 1 wherein said combustion chamber has an overall length of six feet. 6. The combustion apparatus of claim 1 wherein said controlled heat flux for said combustion apparatus at a mass flow rate of 0.45 kg/s ranges from 20 kW/m2 at 1000 degrees Kelvin to 384 kW/m2 at 1500 degrees Kelvin. 7. A combustion apparatus for providing a controlled heat flux for testing a test specimen containing an energetic material comprising: (a) a source of air for providing a stream of air at a mass flow rate of 0.5 kg/sec, said source of air comprising a fan motor and fan, said fan, when driven at 3870 RPM, generating said mass flow rate of 0.5 kg/sec;(b) an air inlet duct having said source of air positioned at one end thereof;(c) a manifold positioned at the other end of said air inlet duct, said manifold having a fuel injection system comprising equally eight spaced apart fuel injectors located within said manifold which form a ring around said manifold, wherein the eight fuel injectors of said fuel injection system inject propane fuel into the stream of air forming a flammable mixture;(d) a combustion chamber having one end thereof connected to said manifold to receive said flammable mixture, wherein said combustion chamber has an inside diameter that is larger than an inside diameter for said air let duct resulting in a substantial increase in area from said air inlet duct to said combustion chamber which allows for flame stabilization within a reaction region in said combustion chamber; and(e) a fuel ignition device positioned in proximity to said flammable mixture, said fuel ignition device igniting said flammable mixture generating said controlled heat flux within said combustion chamber to test said test specimen which includes said energetic material, wherein said controlled heat flux for said combustion apparatus at said mass flow rate of 0.5 kg/s ranges from 20 kW/m2 at 1000 degrees Kelvin to 38 kW/m2 at 1500 degrees Kelvin. 8. The combustion apparatus of claim 7 wherein the inside diameter of said combustion chamber is approximately eighteen inches and the inside diameter of said air inlet duct is approximately five inches. 9. The combustion apparatus of claim 7 wherein said combustion chamber and said air duct are each fabricated from stainless steel. 10. The combustion apparatus of claim 7 further comprising a layer of insulation mounted on the outer side of said combustion chamber, said layer of insulation enhancing temperature control of said flammable mixture within said combustion chamber. 11. The combustion apparatus of claim 7 wherein said combustion chamber has an overall length of approximately six feet. 12. A method for providing a controlled heat flux for testing a test specimen containing an energetic material comprising the steps of: (a) generating a stream of air at a fixed mass flow rate;(b) providing an inside diameter for a combustion chamber which is larger than an inside diameter for an air inlet duct resulting in a substantial increase in area from said air inlet duct to said combustion chamber which allows for flame stabilization within a reaction region in said combustion chamber;(c) delivering said stream of air at said fixed mass flow rate through said air inlet duct to said combustion chamber;(d) injecting propane fuel into said stream of air at a location in proximity to said combustion chamber to form a flammable mixture for said combustion chamber; and(e) igniting said flammable mixture when said flammable mixture is within said combustion chamber, said flammable mixture when ignited within said combustion chamber generating a controllable heat flux for testing said specimen containing said energetic material. 13. The method of claim 12 further comprising the step of providing a manifold which includes eight equally spaced apart nozzles forming a ring around said manifold, wherein said manifold is positioned in proximity to said combustion chamber which allows the eight nozzles within said manifold to inject said propane fuel into said stream of air forming said flammable mixture within said combustion chamber. 14. The method of claim 12 wherein said fixed mass flow rate is approximately 0.5 kg/sec. 15. The method of claim 14 further comprising the step of providing a source of air positioned at end of said air duct opposite said combustion chamber, wherein said source of air comprises a five horsepower fan motor and fan located within a fan and motor housing, said fan motor and fan delivering said stream of air through said air inlet duct at said fixed mass flow rate of 0.5 kg/sec. 16. The method of claim 12 further comprising the step of providing a layer of insulation mounted on the outer side of said combustion chamber, said layer of insulation enhancing temperature control of said flammable mixture within said combustion chamber. 17. The method of claim 12 further comprising the step of providing said controlled heat flux for said combustion apparatus at a mass flow rate of 0.45 kg/s which ranges from 20 kW/m2 at 1000 degrees Kelvin to 38 kW/m2 at 1500 degrees Kelvin.