Abstract: An injection system for polymer gel emulsion is powered to cause polymer gel emulsion to be injected into high energy water entering a scooping intake, such as that on a firefighting aircraft. To energize the polymer gel emulsion, an accumulator is interposed between a polymer gel emulsion injection line and the water scooping intake. High energy water is routed to one side of the accumulator where this high energy water acts on the accumulator to move a movable element within the accumulator which pressurizes and expels polymer gel emulsion into the polymer gel emulsion injection line for injection of the polymer gel emulsion through a junction and into a mixed supply line of water and polymer gel emulsion downstream of a junction. The mixed polymer gel emulsion and water are routed to a tank for storage until ready for use.

Abstract: A tank on a firefighting aircraft initially is loaded with water. A polymer gel emulsion vessel is provided on the aircraft, but is not activated and mixed with tank water until such polymer gel preparation is initiated by an operator. When initiated, a pump pulls water from the tank and doses it with gel emulsion. Double elbows and/or the pump impeller fully activates the polymer gel. The activated polymer gel is mixed within the tank by one of a variety of systems including mixing paddles or sparging with gas. In one embodiment, a hollow tower of telescoping form has a float to keep an upper end near a surface in the tank and a sparging gas entry is a controlled distance below the surface, such that gas of limited pressure, such as from a ram air inlet can sparge and mix the water and activated polymer gel emulsion effectively.

Abstract: The system includes a pod suspended beneath the aircraft and above a water fillable and emptyable bucket. Polymer gel emulsion preparation equipment is included at the bucket. The pod includes an elongate shaft for carrying structural loads between a cable extending down from the aircraft and the bucket. The pod also includes a polymer gel tank. A polymer gel pump delivers polymer gel to the polymer gel emulsion preparation equipment within the bucket when required. The pod is configured to include a pathway for routing of various lines from the aircraft down to the bucket, and past the polymer gel tank. Sub-systems for filling the polymer gel tank and for equalizing pressure within the polymer gel tank are also included with the pod, so that the pod provides a modular polymer gel storage for use with polymer gel emulsion preparation equipment within a bucket suspended beneath the aircraft.

Abstract: The system includes a snorkel leading from an intake up to a tank borne by an aircraft. A feed pump in the intake draws water up the snorkel to the tank. A polymer gel emulsion reservoir supplies polymer gel upstream of the feed pump for addition and activation of the polymer gel emulsion with the water. A separate pump within the tank provides for selectable recirculation within the tank and/or discharge out of the tank, such as out of a nozzle. Polymer gel emulsion can optionally be supplied at the tank pump rather than the feed pump for delayed addition of polymer gel emulsion to water carried by the aircraft.

Abstract: A tank on a firefighting aircraft initially is loaded with water. A polymer gel emulsion vessel is provided but gel emulsion is not activated and mixed with water in the tank until such polymer gel preparation is initiated by an operator. When initiated, a pump pulls water from the tank and returns water back to the tank with a dose of gel emulsion supplied therein. Double elbows and/or the pump impeller fully activates the polymer gel. The activated polymer gel is mixed within the tank by one of a variety of systems including sparging with air, routing of return water from the pump through nozzles and providing a baffle for generating circulatory mixing flow within the tank, or utilizing a mixer element which moves dynamically within the tank. Hydrodynamic forces associated with the aircraft passing over a body of water can power dosing of the water with polymer gel emulsion.

Abstract: The delivery system includes a blender assembly which can be fitted within a bucket or other container an aircraft. The blender assembly includes a combiner which receives water from within the container and gel concentrate from a gel inlet. The combiner brings the water and gel concentrate together upstream of a pump. The pump pressurizes and mixes the water and gel concentrate together to provide a hydrated fire suppression gel ready for application. An outlet of the pump leads through appropriate conduits to a nozzle. The nozzle includes a downwardly extending spout which sprays the hydrated gel down onto the ground beneath the aircraft. When the water within the container has been depleted, the aircraft is flown to a water source and the container is refilled. Then the blender can again be used to manufacture and deliver the fire suppression gel to an area to be treated.

Abstract: An injection system for polymer gel emulsion is powered to cause polymer gel emulsion to be injected into high energy water entering a scooping intake, such as that on a firefighting aircraft. To energize the polymer gel emulsion, an accumulator is interposed between a polymer gel emulsion injection line and the water scooping intake. High energy water is routed to one side of the accumulator where this high energy water acts on the accumulator to move a movable element within the accumulator which pressurizes and expels polymer gel emulsion into the polymer gel emulsion injection line for injection of the polymer gel emulsion through a junction and into a mixed supply line of water and polymer gel emulsion downstream of a junction. The mixed polymer gel emulsion and water are routed to a tank for storage until ready for use.

Abstract: Water is mixed with fire suppressant polymer in a mixer absent a power source. The mixer receives water through a water inlet with water exhibiting high velocity and associated hydrodynamic force. Such velocity is achieved by locating the water inlet connected to a float or other part of an aircraft so that when the aircraft flies over water with the float dipping into the water, water is driven through the opening and into the water inlet of the mixer. A polymer inlet passes into the mixer. A bend is located downstream of the water inlet and the polymer inlet. The bend exhibits sufficient resistance to fluid flow direction therethrough that the polymer is sheared and thoroughly mixed and activated with the water. A colorant inlet is optionally provided within the mixer and the water and polymer mixture is then discharged into a tank for later utilization at a firefighting location.

Abstract: Water is mixed with fire suppressant polymer in a mixer absent a power source. The mixer receives water through a water inlet with water exhibiting high velocity and associated hydrodynamic force. Such velocity is achieved by locating the water inlet connected to a float or other part of an aircraft so that when the aircraft flies over water with the float dipping into the water, water is driven through the opening and into the water inlet of the mixer. A polymer inlet passes into the mixer. A bend is located downstream of the water inlet and the polymer inlet. The bend exhibits sufficient resistance to fluid flow direction therethrough that the polymer is sheared and thoroughly mixed and activated with the water. A colorant inlet is optionally provided within the mixer and the water and polymer mixture is then discharged into a tank for later utilization at a firefighting location.

Abstract: The delivery system includes a blender assembly which can be fitted within a bucket or other container an aircraft. The blender assembly includes a combiner which receives water from within the container and gel concentrate from a gel inlet. The combiner brings the water and gel concentrate together upstream of a pump. The pump pressurizes and mixes the water and gel concentrate together to provide a hydrated fire suppression gel ready for application. An outlet of the pump leads through appropriate conduits to a nozzle. The nozzle includes a downwardly extending spout which sprays the hydrated gel down onto the ground beneath the aircraft. When the water within the container has been depleted, the aircraft is flown to a water source and the container is refilled. Then the blender can again be used to manufacture and deliver the fire suppression gel to an area to be treated.