Aerial fire suppression system

1. A fire suppression apparatus for fighting fires from a helicopter, comprising:

a tank assembly configured for attachment to an underside of the helicopter, comprising

a foam tank for housing a foam,

a water tank located downstream of the foam tank for housing water, wherein the water tank is configured to receive the foam from the foam tank that when mixed with water in the water tank forms a liquid fire retardant in the water tank, and

a tank assembly housing that encloses the foam tank and the water tank;

a powerpack configured for attachment to a side of the helicopter, comprising

a liquid fire retardant pump configured to pump the liquid fire retardant comprising the foam and water, the liquid fire retardant pump driven by a first electric motor, the liquid fire retardant pump including a pump inlet and an air induction valve positioned at the pump inlet, the air induction valve including an electrically variable valve opening, wherein air and the liquid fire retardant are drawn together into the pump inlet and pressurized by the liquid fire retardant pump to form a pressurized water/foam/air fire retardant solution;

a liquid primer pump driven by a second electric motor, the liquid primer pump configured to prime the pump inlet with the liquid fire retardant from the water tank;

an inverter connected to the first electric motor, the inverter configured to slowly and controllably start the first electric motor to minimize startup current draw by the first electric motor;

a cannon assembly configured for attachment to an opposite side of the helicopter, comprising

an aimable boom connected to the liquid fire retardant pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized water/foam/air fire retardant solution is dispensed toward a target,

wherein the powerpack and the cannon assembly are each supported by a pair of brackets cantileverly extending from respective vertical mount plates that are each attachable on opposite sides of a fuselage of the helicopter, and

wherein each vertical mount plate is configured to attach to structural hardpoints located on an exterior surface of the helicopter; and

including a pair of adjustable length connecting members including a clevis on each opposing end of the connecting members for directly attaching each vertical mount plate to a pair of structural hardpoints of the helicopter.

2. The fire suppression apparatus of claim 1 , wherein the liquid fire retardant pump and the liquid primer pump are each supported on a flat upper surface of a horizontal base.

3. The fire suppression apparatus of claim 1 , including a ball valve positioned downstream and adjacent a discharge opening of the liquid fire retardant pump.

4. The fire suppression apparatus of claim 1 , wherein a primer pump discharge conduit connects a primer pump discharge outlet with a suction conduit positioned upstream of the pump inlet of the liquid fire retardant pump to fill the suction conduit with the liquid fire retardant from the water tank before the first electric motor is commanded to rotate.

5. The fire suppression apparatus of claim 1 , including a conduit extending from an inlet of the primer pump to a sump area of the water tank.

6. The fire suppression apparatus of claim 1 , wherein the boom includes a carbon fiber composite impregnated with copper mesh.

7. The fire suppression apparatus of claim 6 , wherein the boom includes an outboard boom portion, an inboard boom portion, a coupler portion, wherein the coupler portion joins the inboard boom portion to the outboard boom portion.

8. The fire suppression apparatus of claim 7 , wherein the coupler portion includes an outer collar, a spring, and a receiver.

9. The fire suppression apparatus of claim 8 , wherein the outer collar engages with an annular groove of the receiver, and wherein the spring is in compression when the coupler portion is connected to the inboard boom portion and to the outboard boom portion.

10. The fire suppression apparatus of claim 1 , wherein the air induction valve includes an inlet that directly receives unpressurized ambient air.

11. The fire suppression apparatus of claim 1 , including one or more electronic controllers in operative communication with the first 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 liquid fire retardant pump.

12. The fire suppression apparatus of claim 1 , including a foam pump configured to pump the foam from the foam tank to the water tank, wherein the tank assembly housing encases the foam pump.

13. The fire suppression apparatus of claim 1 , wherein the foam tank and the water tank each 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.

14. The fire suppression apparatus of claim 1 , wherein the inverter provides electrical current to the first electric motor linearly from zero amps to approximately 65 amps over a period of 2 to 3 seconds.

15. A fire suppression apparatus for fighting fires from a helicopter, comprising:

a tank assembly configured for attachment to an underside of the helicopter, comprising

a tank assembly housing defining an enclosure for holding water,

at least one foam tank for holding a foam, the at least one foam tank positioned inside the enclosure, the at least one foam tank displacing the water held by the enclosure,

wherein the enclosure is configured to receive at least a portion of the foam from the at least one foam tank that when mixed with the water in the enclosure forms a liquid fire retardant in the enclosure;

a powerpack configured for attachment to a fuselage of the helicopter, comprising

a liquid fire retardant pump configured to pump from the enclosure the liquid fire retardant, the liquid fire retardant pump driven by a first electric motor, the liquid fire retardant pump including a pump inlet and an air induction valve positioned at the pump inlet, the air induction valve including an electrically variable valve opening, wherein air and the liquid fire retardant are drawn together into the pump inlet and pressurized by the liquid fire retardant pump to form a pressurized water/foam/air fire retardant solution,

a liquid primer pump driven by a second electric motor, the liquid primer pump configured to prime the pump inlet with the liquid fire retardant from the enclosure, and

an inverter connected to the first electric motor, the inverter configured to slowly and controllably start the first electric motor to minimize startup current draw by the first electric motor;

a cannon assembly configured for attachment to an opposite side of the helicopter, comprising

an aimable boom connected to the liquid fire retardant pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized water/foam/air fire retardant solution is dispensed toward a target, and

wherein the powerpack and the cannon assembly are each supported by a pair of brackets cantileverly extending from respective vertical mount plates that are each attachable on opposite sides of the fuselage of the helicopter, and

wherein each vertical mount plate is configured to attach to structural hardpoints located on an exterior surface of the helicopter; and

including a pair of adjustable length connecting members including a clevis on each opposing end of the connecting members for directly attaching each vertical mount plate to a pair of structural hardpoints of the helicopter.

16. A fire suppression apparatus for fighting fires from a helicopter, comprising:

a tank assembly configured for attachment to an underside of the helicopter, comprising

a foam tank for housing a foam,

a water tank located downstream of the foam tank for housing water, wherein the water tank is configured to receive the foam from the foam tank that when mixed with water in the water tank forms a liquid fire retardant in the water tank, and

a tank assembly housing that encloses the foam tank and the water tank;

a powerpack configured for attachment to a side of the helicopter, comprising

a liquid fire retardant pump configured to pump the liquid fire retardant comprising the foam and water, the liquid fire retardant pump driven by a first electric motor, the liquid fire retardant pump including a pump inlet and an air induction valve positioned at the pump inlet, the air induction valve including an electrically variable valve opening, wherein air and the liquid fire retardant are drawn together into the pump inlet and pressurized by the liquid fire retardant pump to form a pressurized water/foam/air fire retardant solution;

a liquid primer pump driven by a second electric motor, the liquid primer pump configured to prime the pump inlet with the liquid fire retardant from the water tank;

an inverter connected to the first electric motor, the inverter configured to slowly and controllably start the first electric motor to minimize startup current draw by the first electric motor; and

a cannon assembly configured for attachment to an opposite side of the helicopter, comprising

an aimable boom connected to the liquid fire retardant pump by a conduit, the boom including a nozzle on a distal end of the boom from which the pressurized water/foam/air fire retardant solution is dispensed toward a target,

wherein the boom includes a carbon fiber composite impregnated with copper mesh, wherein the boom includes an outboard boom portion, an inboard boom portion, a coupler portion, wherein the coupler portion joins the inboard boom portion to the outboard boom portion, and wherein the coupler portion includes an outer collar, a spring, and a receiver.

17. The fire suppression apparatus of claim 16 , wherein the outer collar engages with an annular groove of the receiver, and wherein the spring is in compression when the coupler portion is connected to the inboard boom portion and to the outboard boom portion.