Enhanced aerial delivery system
An enhanced aerial delivery system addresses issues raised when large quantities of fluids, powders, and other agent materials are to be transported in and aerially dispersed by aircraft. Some aspects include positioning and securing of tanks aboard the aircraft to facilitate management and safety of the tanks and aircraft. Other aspects address coupling of the tanks and associated piping to lessen structural effects upon the aircraft. Further aspects deal with channeling, containing, and dumping stray agent materials that have escaped from the agent tanks on board the aircraft.
1. An aircraft, comprising:
a deck;
a lower outer wall portion located below the deck;
a plurality of agent tanks positioned on the deck, each of the plurality of agent tanks configured to hold a liquid to be dispersed from the aircraft;
a plurality of propellant tanks positioned on the deck, each of the plurality of propellant tanks configured to hold a pressurized gas and coupled to the agent tanks to expel the liquid from the agent tanks;
an outlet coupled to at least one of the agent tanks and extending below the deck and through the outer wall portion to direct liquid from the agent tanks out of the aircraft when expelled from the agent tanks in response to the pressurized gas supplied to the agent tanks by the propellant tanks;
a forward barrier positioned on the deck located forward of the agent tanks and forward of the outlet to inhibit forward migration beyond the forward barrier of liquid in the agent tanks that escapes therefrom and reaches the forward barrier;
an aft barrier positioned on the deck located aft of the agent tanks and aft of the outlet to inhibit rearward migration beyond the aft barrier of liquid in the agent tanks that escapes therefrom and reaches the aft barrier;
a middle barrier positioned on the deck located between the forward barrier and the aft barrier and between ones of the agent tanks, and forward of the outlet, to inhibit forward migration beyond the middle barrier of liquid in the agent tanks that escapes therefrom and reaches the middle barrier and to inhibit rearward migration beyond the middle barrier of liquid in the agent tanks that escapes therefrom and reaches the middle barrier;
a forward deck opening in the deck forward of and adjacent to the middle barrier to allow the passage of the liquid that escapes from the agent tanks and is forward of the middle barrier to pass downward through the deck to a location adjacent to the outlet;
an aft deck opening in the deck rearward of and adjacent to the aft barrier to allow the passage of the liquid that escapes from the agent tanks and is rearward of the aft barrier to pass downward through the deck to a location adjacent to the outlet;
a middle deck opening in the deck between the middle barrier and the aft barrier, and between the forward opening and the aft deck opening, to allow the passage of the liquid that escapes from the agent tanks and is between the middle barrier and the aft barrier to pass downward through the deck to a location adjacent to the outlet;
a forward guide wall extending from at least adjacent to the deck at a location forward of the forward deck opening to the lower outer wall portion at a location forward of the outlet for guiding liquid that escapes from the agent tanks and is forward of the middle barrier and passes downward through the forward deck opening to a location adjacent to the outlet; and
a rearward guide wall extending from at least adjacent to the deck at a location rearward of the aft deck opening to the lower outer wall portion at a location rearward of the outlet for guiding liquid that escapes from the agent tanks and is rearward of the aft barrier and passes downward through the aft deck opening to a location adjacent to the outlet.
2. The aircraft of claim 1 wherein a lower portion of the forward guide wall and a lower portion of the rearward guide wall define therebetween a liquid collection compartment for the liquid that escapes from the agent tanks and passes downward through the deck through the forward, middle and aft deck openings.
3. The aircraft of claim 2 wherein the outlet includes:
an outlet end portion located adjacent to the lower outer wall portion and having an opening therein above the lower outer wall portion in position for liquid communication with the liquid collection compartment; and
a member movably coupled to the outlet end portion, the member having a closed position and an open position, the member configured to be moved from the closed position to the open position through buoyant contact with a portion of the escaped liquid collected in the liquid collection compartment, in the closed position the member being oriented to block passage therethrough to the liquid collection compartment of liquid within the outlet being expelled from the agent tanks in response to the pressurized gas supplied to the agent tanks by the propellant tanks, and in the open position the member being oriented to allow access into the outlet to allow passage therethrough of the escaped liquid collected in the liquid collection compartment for draining the escaped liquid in the liquid collection compartment through the outlet to the exterior of the aircraft.
4. The aircraft of claim 3 wherein the member includes a shutter with a density less than the liquid so as to be buoyant relative to the liquid.
5. The aircraft of claim 3 wherein the member includes a door and a float having a combined density, the combined density of the door and the float being less than the liquid so as to be buoyant relative to the liquid.
6. The aircraft of claim 3 further including a pin and a track, the pin extending from the member and the track positioned to receive the pin to guide movement of the member between the open and closed positions.
7. The aircraft of claim 6 wherein track is shaped to direct movement by the pin in a linear direction.
8. The aircraft of claim 3 further including a stop attached to the outlet end portion and positioned to prevent travel of the member beyond a predetermined vertical height.
9. A system to be transported by an aircraft, the aircraft having a deck and a lower outer wall portion located below the deck, the deck having a forward deck opening providing a fluid passageway through the deck to the lower outer wall portion, an aft deck opening providing a fluid passageway through the deck to the lower outer wall portion, and a middle deck opening between the forward deck opening and the aft deck opening providing a fluid passageway through the deck to the lower outer wall portion, comprising:
a plurality of agent tanks positioned on the deck, each of the plurality of agent tanks configured to hold a liquid to be dispersed from the aircraft;
a plurality of propellant tanks positioned on the deck, each of the plurality of propellant tanks configured to hold a pressurized gas and coupled to the agent tanks to expel the liquid from the agent tanks;
an outlet coupled to at least one of the agent tanks and extending below the deck and through the outer wall portion to direct liquid from the agent tanks out of the aircraft when expelled from the agent tanks in response to the pressurized gas supplied to the agent tanks by the propellant tanks;
a forward barrier positioned on the deck located forward of the agent tanks and forward of the outlet to inhibit forward migration beyond the forward barrier of liquid in the agent tanks that escapes therefrom and reaches the forward barrier;
an aft barrier positioned on the deck located aft of the agent tanks, the outlet and the middle deck opening, and forward of and adjacent to the aft deck opening to inhibit rearward migration beyond the aft barrier of liquid in the agent tanks that escapes therefrom and reaches the aft barrier, and to divert the liquid that escapes from the agent tanks and is rearward of the aft barrier to pass downward through the aft deck opening to a location adjacent to the outlet;
a middle barrier positioned on the deck located between the forward barrier and the aft barrier and between ones of the agent tanks, forward of the outlet and the middle deck opening, and rearward of and adjacent to the forward deck opening to inhibit forward migration beyond the middle barrier of liquid in the agent tanks that escapes therefrom and reaches the middle barrier, and to inhibit rearward migration beyond the middle barrier of liquid in the agent tanks that escapes therefrom and reaches the middle barrier and to divert the liquid that escapes from the agent tanks and is forward of the middle barrier to pass downward through the forward deck opening to a location adjacent to the outlet, the aft barrier and the middle barrier positioned with the middle deck opening therebetween to allow the liquid that escapes from the agent tanks and is between the middle barrier and the aft barrier to pass downward through the middle deck opening to a location adjacent to the outlet;
a forward guide wall extending from at least adjacent to the deck at a location forward of the forward deck opening to the lower outer wall portion at a location forward of the outlet for guiding liquid that escapes from the agent tanks and is forward of the middle barrier and passes downward through the forward deck opening to a location adjacent to the outlet; and
a rearward guide wall extending from at least adjacent to the deck at a location rearward of the aft deck opening to the lower outer wall portion at a location rearward of the outlet for guiding liquid that escapes from the agent tanks and is rearward of the aft barrier and passes downward through the aft deck opening to a location adjacent to the outlet.
10. The system of claim 9 wherein a lower portion of the forward guide wall and a lower portion of the rearward guide wall define therebetween a liquid collection compartment for the liquid that escapes from the agent tanks and passes downward through the deck through the forward, middle and aft deck openings.
11. The system of claim 10 wherein the outlet includes:
an outlet end portion located adjacent to the lower outer wall portion and having an opening therein above the lower outer wall portion in position for liquid communication with the liquid collection compartment; and
a member movably coupled to the outlet end portion, the member having a closed position and an open position, the member configured to be moved from the closed position to the open position through buoyant contact with a portion of the escaped liquid collected in the liquid collection compartment, in the closed position the member being oriented to block passage therethrough to the liquid collection compartment of liquid within the outlet being expelled from the agent tanks in response to the pressurized gas supplied to the agent tanks by the propellant tanks, and in the open position the member being oriented to allow access into the outlet to allow passage therethrough of the escaped liquid collected in the liquid collection compartment for draining the escaped liquid in the liquid collection compartment through the outlet to the exterior of the aircraft.
12. The system of claim 11 wherein the member includes a shutter with a density less than the liquid so as to be buoyant relative to the liquid.
13. The system of claim 11 wherein the member includes a door and a float having a combined density, the combined density of the door and the float being less than the liquid so as to be buoyant relative to the liquid.
14. The system of claim 11 further including a pin and a track, the pin extending from the member and the track positioned to receive the pin to guide movement of the member between the open and closed positions.
15. The system of claim 14 wherein track is shaped to direct movement by the pin in a linear direction.
16. The system of claim 11 further including a stop attached to the outlet end portion and positioned to prevent travel of the member beyond a predetermined vertical height.
17. A system to be transported by an aircraft, the aircraft having a deck and a lower outer wall portion located below the deck, the deck having a first deck opening providing a fluid passageway through the deck to the lower outer wall portion, and a second deck opening rearward of the first deck opening and providing a fluid passageway through the deck to the lower outer wall portion, comprising:
a plurality of agent tanks positioned on the deck, each of the plurality of agent tanks configured to hold a liquid to be dispersed from the aircraft;
a plurality of propellant tanks positioned on the deck, each of the plurality of propellant tanks configured to hold a pressurized gas and coupled to the agent tanks to expel the liquid from the agent tanks;
an outlet coupled to at least one of the agent tanks and extending below the deck and through the outer wall portion to direct liquid from the agent tanks out of the aircraft when expelled from the agent tanks in response to the pressurized gas supplied to the agent tanks by the propellant tanks;
a forward barrier positioned on the deck located forward of the agent tanks and the first deck opening to inhibit forward migration beyond the forward barrier of liquid in the agent tanks that escapes therefrom and reaches the forward barrier;
an aft barrier positioned on the deck located aft of the agent tanks and the second deck opening to inhibit rearward migration beyond the aft barrier of liquid in the agent tanks that escapes therefrom and reaches the aft barrier;
a forward guide wall extending from at least adjacent to the deck at a location forward of the first deck opening to the lower outer wall portion at a location forward of the outlet for guiding liquid that escapes from the agent tanks and passes downward through the first deck opening to a location adjacent to the outlet; and
a rearward guide wall extending from at least adjacent to the deck at a location rearward of the second deck opening to the lower outer wall portion at a location rearward of the outlet for guiding liquid that escapes from the agent tanks and passes downward through the second deck opening to a location adjacent to the outlet.
18. The system of claim 17 further including a middle barrier positioned on the deck located between the forward barrier and the aft barrier and between ones of the agent tanks to inhibit forward migration beyond the middle barrier of liquid in the agent tanks that escapes therefrom and reaches the middle barrier, and to inhibit rearward migration beyond the middle barrier of liquid in the agent tanks that escapes therefrom and reaches the middle barrier.
19. The system of claim 17 wherein a lower portion of the forward guide wall and a lower portion of the rearward guide wall define therebetween a liquid collection compartment for the liquid that escapes from the agent tanks and passes downward through the deck through the forward, middle and aft deck openings.
20. The system of claim 19 wherein the outlet includes:
an outlet end portion located adjacent to the lower outer wall portion and having an opening therein above the lower outer wall portion in position for liquid communication with the liquid collection compartment; and
a member movably coupled to the outlet end portion, the member having a closed position and an open position, the member configured to be moved from the closed position to the open position through buoyant contact with a portion of the escaped liquid collected in the liquid collection compartment, in the closed position the member being oriented to block passage therethrough to the liquid collection compartment of liquid within the outlet being expelled from the agent tanks in response to the pressurized gas supplied to the agent tanks by the propellant tanks, and in the open position the member being oriented to allow access into the outlet to allow passage therethrough of the escaped liquid collected in the liquid collection compartment for draining the escaped liquid in the liquid collection compartment through the outlet to the exterior of the aircraft.