A fire suppression apparatus for fighting fires from a vehicle configured for flight is disclosed, comprising a foam and water held in separate containers aboard the vehicle that when mixed forms a fire retardant, a pump driven by an electric motor to pressurize the fire retardant, the pump includin
A fire suppression apparatus for fighting fires from a vehicle configured for flight is disclosed, comprising a foam and water held in separate containers aboard the vehicle that when mixed forms a fire retardant, a pump driven by an electric motor to pressurize the fire retardant, the pump including an air induction valve where air is drawn into a suction end of the pump and pressurized together with the fire retardant, and an aimable boom connected to the pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized fire retardant and air is dispensed toward a target.
대표청구항▼
1. A fire suppression apparatus for fighting fires from a helicopter, comprising: a tank assembly comprising (a) a foam tank for housing a foam and configured for attachment to the helicopter,(b) a water tank located downstream of the foam tank for housing water and configured for attachment to the
1. A fire suppression apparatus for fighting fires from a helicopter, comprising: a tank assembly comprising (a) a foam tank for housing a foam and configured for attachment to the helicopter,(b) a water tank located downstream of the foam tank for housing water and configured for attachment to the helicopter, wherein the water tank is configured to receive a foam from the foam tank that when mixed with water in the water tank forms a liquid fire retardant in the water tank, and(c) a tank assembly housing that encases the foam tank and the water tank;a centrifugal pump with a radial outflow impeller mountable to the helicopter and driven by an electric motor, the pump including an air induction valve with an electrically variable valve opening disposed at and connected to a suction end of the pump so as to form an air inlet, wherein air and the fire retardant are drawn into the suction end and pressurized by the pump; anda cannon assembly including an aimable boom mountable to the helicopter and connected to the pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized fire retardant and air is dispensed toward a target. 2. The fire suppression apparatus of claim 1, wherein the centrifugal pump is supported on a flat upper surface of a base, and the base is cantileverly mounted to the tank assembly via a pair of brackets. 3. The fire suppression apparatus of claim 2, wherein at least one of the brackets includes a surface defining a plurality of recesses for reducing weight of the at least one of the brackets. 4. The fire suppression apparatus of claim 1, wherein the centrifugal pump is configured to rotate at 9400 rotations, or more, per minute. 5. The fire suppression apparatus of claim 1, wherein the centrifugal pump has an axial inlet. 6. The fire suppression apparatus of claim 1, wherein the air reaching the centrifugal pump via the air induction valve does not pass through an air compressor. 7. The fire suppression apparatus of claim 6, wherein the air induction valve includes an inlet that directly receives unpressurized ambient air. 8. The fire suppression apparatus of claim 1, including one or more electronic controllers in operative communication with the electric motor and the air induction valve, wherein the one or more electronic controllers are configured to automatically open the air induction valve upon activation of the centrifugal pump. 9. The fire suppression apparatus of claim 1, including a foam pump configured to pump foam from the foam tank to the water tank, wherein the tank assembly housing encases the foam pump. 10. The fire suppression apparatus of claim 1, wherein each of the foam tank and the water tank have an interior volume for holding fluid and the interior volume of the foam tank is five to ten percent of the interior volume of the water tank. 11. The fire suppression apparatus of claim 1, wherein the boom is configured to extend at least one meter beyond an outer tip of a rotor of the helicopter. 12. The fire suppression apparatus of claim 11, including a primary power source for supplying electrical power to the cannon assembly and a separate battery for supplying backup electrical power to the cannon assembly. 13. The fire suppression apparatus of claim 1, wherein the cannon assembly includes a turret having a linear actuator, a rotary actuator, a gear belt connected to the rotary actuator, and a bearing supporting a turret housing. 14. The fire suppression apparatus of claim 13, wherein the cannon assembly includes a pivot arm connected to the linear actuator and one or more gas springs connected to the boom. 15. The fire suppression apparatus of claim 1, wherein the water tank includes an anti-cavitation device. 16. The fire suppression apparatus of claim 15, wherein the anti-cavitation device is mounted inside the water tank at a lowest point of the water tank. 17. The fire suppression apparatus of claim 1, including a retractable pump system configured to deploy and retract a flexible hose, wherein the retractable pump system includes a pump housing supporting a motorized reel and a reversible motor, and wherein the pump housing includes panels fastened to cage elements. 18. A fire suppression apparatus for fighting fires from a helicopter, comprising: a tank assembly comprising (a) a foam tank for housing a foam and configured for attachment to the helicopter,(b) a water tank located downstream of the foam tank for housing water and configured for attachment to the helicopter, wherein the water tank is configured to receive a foam from the foam tank that when mixed with water in the water tank forms a liquid fire retardant in the water tank, and(c) a tank assembly housing that encases the foam tank and the water tank;a centrifugal pump with a radial outflow impeller mountable to the helicopter and driven by an electric motor, the pump including an air induction valve with an electrically variable valve opening disposed at and connected to a suction end of the pump so as to form an air inlet, wherein air and the fire retardant are drawn into the suction end and pressurized by the pump, wherein the centrifugal pump is supported on a flat upper surface of a base cantilevered via a pair of brackets, and at least one of the brackets includes a surface defining a plurality of recesses for reducing weight of the at least one of the brackets; anda cannon assembly including an aimable boom mountable to the helicopter and connected to the pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized fire retardant and air is dispensed toward a target. 19. A fire suppression helicopter, comprising: a tank assembly comprising (a) a foam tank for housing a foam and configured for attachment to the helicopter,(b) a water tank located downstream of the foam tank for housing water and configured for attachment to the helicopter, wherein the water tank is configured to receive a foam from the foam tank that when mixed with water in the water tank forms a liquid fire retardant in the water tank, and(c) a tank assembly housing that encases the foam tank and the water tank;an axial inlet centrifugal pump with a radial outflow impeller mounted to the helicopter and driven by an electric motor, the pump including an air induction valve with an electrically variable valve opening disposed at and connected to a suction end of the pump so as to form an air inlet, wherein air and the fire retardant are drawn into the suction end and pressurized by the pump, and the air reaching the centrifugal pump via the air induction valve does not pass through an air compressor; anda cannon assembly including an aimable boom mounted to the helicopter and connected to the pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized fire retardant and air is dispensed toward a target, wherein the boom is configured to extend at least one meter beyond an outer tip of a rotor of the helicopter.
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