Aerially transportable tank for storing a composition for discharging in flight
View Patent ↗An aerially transportable tank ( 20 ) for storing a composition for discharging in flight, the tank including a neck ( 23 ) terminated by a composition discharge opening ( 24 ), and having a wall ( 21 ) extending the neck that is sufficiently deformable to be received in part or in full within the neck.
1. A tank ( 20 ) for storing a fluid composition and for discharging the stored fluid composition in flight, the tank comprising:
a configuration releasably installable inside a fuselage of an aircraft,
when installed inside the fuselage of an aircraft, the tank having i) a collapsed-folded position and ii) an unfolded position,
from bottom to top, the configuration comprising
i) a lower rigid discharge opening,
ii) movable flaps located within said discharge opening and having a first position closing said discharge opening to fluid discharge and a second position opening said discharge opening, the second position operative for discharging the fluid composition during flight from the tank via said discharge opening,
iii) a lower neck connected to and above said discharge opening, said lower neck configured for installation in a ventral portion of the fuselage through an upper opening within a cabin floor inside a cabin of the fuselage, said lower neck defining a main compartment of a first volume for collapsing through the upper opening,
iv) a flexible wall with a wall portion protruding under the cabin floor, wherein the flexible wall a) in the unfolded position of the tank, extends upward from said lower neck inside the fuselage and forms a secondary compartment of a second volume for storing the fluid composition to be discharged, and b) in the collapsed-folded position, is folded inside said first volume within the lower neck,
v) a plurality of superposed inflatable belts that, in the unfolded position of the tank, extend inside the fuselage, said belts being outside and around said flexible wall and supporting upright said flexible wall in the unfolded position, upon at least a part of a height vertical dimension of said secondary compartment,
vi) a central top wall integral with the flexible wall, and, in the collapsed-folded position of the tank, forming a mattress closing the upper opening within the cabin floor and in collapsed-folded position of the tank also providing continuity for the cabin floor inside the fuselage, and
vii) an internal suction pipe located within said central top wall, said internal suction pipe configured for introduction of the fluid composition into the tank.
2. The tank according to claim 1 , wherein the second volume is greater than the first volume.
3. The tank according to claim 2 , wherein the flexible wall is separable from the neck and the neck and wall are connected via a flange.
4. The tank according to claim 1 , wherein a capacity of the tank is in the range of about 0.5m 3 to about 20m 3 , and the flexible wall includes a material having at least one layer of plastics material.
5. The tank according to claim 1 , further comprising a partition separating the main and secondary compartments.
6. The tank according to claim 1 , further comprising a leaktight partition that separates the main compartment from the secondary compartment, wherein the secondary compartment does not communicate with said discharge opening.
7. The tank according to claim 6 , wherein the secondary compartment includes a secondary orifice and the secondary compartment communicates outside the tank via the secondary orifice.
8. The tank according to claim 6 , wherein the secondary compartment receives a secondary composition having a density less than a density of the fluid composition for discharging in flight.
9. The tank according to claim 8 , wherein the secondary composition is air.
10. The tank according to claim 6 , wherein the secondary compartment covers the neck when the main compartment is housed inside the neck.
11. The tank according to claim 1 , wherein the aircraft is a rotocraft,
the tank further comprising a holding structure running along the cabin floor and, in the unfolded position of the tank, holding a generally horizontal portion of the flexible wall inside the cabin.
12. The tank according to claim 11 , wherein the holding structure includes an inclination-maintaining structure that supports the generally horizontal portion of the flexible wall in an inclined position such that any stored fluid composition flows towards the neck.
13. The tank according to claim 12 , wherein the inclination-maintaining structure comprises a wedge-forming structure that extends between the floor of the cabin and the wall of the tank, adjacent to the neck.
14. The tank according to claim 12 , wherein the inclination-maintaining structure is inflatable at least in part and surrounds at least a portion of the neck of the tank.
15. The tank according to claim 12 , wherein the inclination-maintaining structure includes one or more blocks of cellular material.
16. The tank according to claim 11 , wherein the holding structure further includes a belt that surrounds at least a portion of the tank, wherein the belt rest on the floor of the cabin.
17. The tank according to claim 16 , wherein the belt are inflatable and comprise a plurality of superposed leaktight compartments.
18. The tank according according to claim 11 , wherein the tank further includes an inflatable secondary compartment that covers the neck and the opening in the floor of the cabin when the wall is housed inside the neck.
19. A rotorcraft in combination with the tank of claim 1 releasably installed therein.
20. The rotorcraft according to claim 19 , further comprising an external suction pipe fitted with a pump, an internal tank-filler pipe connecting the external suction pipe to a filler orifice provided in a deformable wall of the tank, and an overflow pipe that connects to the tank.