Pressure assisted variable flow clean throat aerial retardant delivery system
View Patent ↗An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.
1. An aerial retardant delivery system for use with an aircraft having a pressurized fuselage, the system comprising:
a retardant tank mountable in the fuselage of the aircraft, the retardant tank including:
at least one pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the retardant tank; and
at least one outlet extending through a sidewall of the fuselage, through which retardant may be delivered to a target; and
at least one discharge gate operative to selectively open and close the outlet; and
a variable flow controller that (i) controls a discharge gate open position in order to provide retardant over a desired area of terrain and (ii) includes a pressure differential interlock whereby the at least one discharge gate is not opened if the difference in pressure between the pressure in the fuselage and ambient pressure exceeds a selected threshold level.
2. The aerial retardant delivery system of claim 1 , further comprising a one-way flapper disposed in the pressure opening operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.
3. The aerial retardant delivery system of claim 1 , further comprising an actuation mechanism disposed on the exterior of the tank operatively coupled to the at least one discharge gate.
4. The aerial retardant delivery system of claim 1 , wherein the tank is configured as a polygonal funnel.
5. The aerial retardant delivery system of claim 4 , wherein the tank includes a main portion having a top wall and a plurality of surrounding sidewalls extending from the top wall and a neck portion extending from the main portion of the tank and extending through the sidewall of the fuselage.
6. The aerial retardant delivery system of claim 5 , further comprising a one-way flapper disposed in the pressure opening operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.
7. An aircraft, comprising:
a fuselage having a surrounding sidewall;
a fuselage pressurization system operative to selectively pressurize at least a portion of the fuselage;
an engine;
a retardant tank disposed in the fuselage, the retardant tank including:
at least one pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the retardant tank; and
at least one outlet extending through the sidewall of the fuselage, through which retardant may be delivered to a target; and
at least one discharge gate operative to selectively open and close the outlet; and
a variable flow controller that (i) controls a discharge gate open position in order to provide retardant over a desired area of terrain and (ii) includes a pressure differential interlock whereby the at least one discharge gate is not opened if the difference in pressure between the pressure in the fuselage and ambient pressure exceeds a selected threshold level.
8. The aircraft of claim 7 , further comprising a one-way flapper disposed in the pressure opening operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.
9. The aircraft of claim 7 , further comprising an actuation mechanism disposed on the exterior of the tank operatively coupled to the at least one discharge gate.
10. The aircraft of claim 7 , wherein the tank is configured as a polygonal funnel.
11. The aircraft of claim 10 , wherein the tank includes a main portion having a top wall and a plurality of surrounding sidewalls extending from the top wall and a neck portion extending from the main portion of the tank and extending through a sidewall of the fuselage.
12. The aircraft of claim 11 , wherein the at least one pressure opening is formed through the top wall.
13. The aircraft of claim 12 , further comprising a one-way flapper disposed in the pressure opening operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.