Pyrotechnic device
AssigneeSafran Helicopter Engines
InventorsFrançois Danguy, Laurent Paul Lattanzio Fabbri, Romain Maurice Henri Yannick Gauthier, Didier Paul Saucereau
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Abstract
A pyrotechnic device comprising a main pyrotechnic charge, a firing device for firing the main pyrotechnic charge, a discharge passage for discharging the gas generated by firing the main pyrotechnic charge, and an injector device configured to inject a cooling fluid into said gas discharge passage, so as to deliver gas, specifically for driving turbines, at temperatures that are relatively low, and a method of cooling gas generated by firing the main pyrotechnic charge by injecting the cooling fluid.
Claims20
A pyrotechnic device comprising a main pyrotechnic charge, a firing device for firing the main pyrotechnic charge, a discharge passage for discharging the gas generated by firing the main pyrotechnic charge, wherein the gas is discharged from the discharge passage to a turbine of a turbomachine, a tank containing a cooling fluid, in communication with the discharge passage, a pressurizing device comprising an auxiliary pyrotechnic charge in communication with the tank for pressurizing the tank solely with gas generated by firing the auxiliary pyrotechnic charge, and an injector device configured to inject the cooling fluid into said gas discharge passage;
- wherein the firing device for the main pyrotechnic charge and the auxiliary pyrotechnic charge are communicably coupled to a control unit, wherein the control unit is configured to fire the auxiliary pyrotechnic charge before the main pyrotechnic charge, and wherein the auxiliary pyrotechnic charge is dimensioned so as to spread out the injection of the cooling fluid over a duration that is longer than that for which the gas generated by firing the main pyrotechnic charge is discharged.
A method of cooling gas generated by firing a main pyrotechnic charge of a pyrotechnic device, wherein a cooling fluid is pressurized solely by gas generated by firing an auxiliary pyrotechnic charge, and injected by an injector device into a discharge passage in which the gas generated by firing the main pyrotechnic charge flows, wherein the gas is discharged from the discharge passage to a turbine of a turbomachine, wherein a firing device for the main pyrotechnic charge, and the auxiliary pyrotechnic charge, are communicably coupled to a control unit, wherein the control unit fires the auxiliary pyrotechnic charge before the main pyrotechnic charge, and wherein the injection of the cooling fluid is spread out over a duration that is longer than that for which the gas generated by firing the main pyrotechnic charge is discharged.
Dependencies are inferred from the claim text.