Seaplane float propulsion system

1. A seaplane float propulsion system that is operable to provide movement of a seaplane in water wherein the seaplane float propulsion system comprises:

a first float member, said first float member having a first end and a second end, said first float member being hollow, said first float member being operably coupled to an aircraft;

a second float member, said second float member having a first end and a second end, said second float member being operably coupled to the aircraft wherein the second float member is parallel to said first float member;

a first propulsion assembly, said first propulsion assembly being mounted within said first float member, said first propulsion assembly being proximate said second end of said first float member, said first propulsion assembly configured to intake water thereinto and subsequently eject water therefrom;

said first propulsion assembly comprising an intake member, said intake member being mounted in a bottom of said first flotation member, said intake member configured to permit water to enter thereinto;

said first propulsion assembly further comprising a nozzle housing, said nozzle housing being operably coupled to said intake member, said nozzle housing being hollow allowing water to flow therethrough;

said first propulsion assembly further comprising a water movement member, said water movement member being disposed within said nozzle housing, said water movement member operable to facilitate intake of water through said intake member and discharge the water through an end member of said nozzle housing;

said first propulsion assembly further comprising a flow direction member, said flow direction member being movably coupled to said nozzle housing, said flow direction member being movable between and first position and a second position, said flow direction assembly configured to redirect water flow discharging from said end member in said second position

a second propulsion assembly, said second propulsion assembly being mounted within said second float member, said second propulsion assembly being proximate said second end of said second float member, said second propulsion assembly configured to intake water thereinto and subsequently eject water therefrom; and

wherein said first propulsion assembly and said second propulsion assembly are independently operable in order to provide water flow in opposite directions.

2. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 1 , wherein said second propulsion assembly includes an intake member, said intake member of said second propulsion assembly being mounted in a bottom of said second flotation member, said intake member of said second propulsion assembly configured to permit water to enter thereinto.

3. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 2 , wherein said second propulsion assembly further includes a nozzle housing, said nozzle housing of said second propulsion assembly being operably coupled to said intake member of said second propulsion assembly, said nozzle housing of said second propulsion assembly being hollow allowing water to flow therethrough.

4. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 3 , wherein said second propulsion assembly includes a water movement member, said water movement member of said second propulsion assembly being disposed within said nozzle housing of said second propulsion assembly, said water movement member of said second propulsion assembly operable to facilitate intake of water through said intake member of said second propulsion assembly and discharge the water through an end member of said nozzle housing of said second propulsion assembly.

5. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 4 , wherein said second propulsion assembly further includes a flow direction member, said flow direction member of said second propulsion assembly being movably coupled to said nozzle housing of said second propulsion assembly, said flow direction member of said second propulsion assembly being movable between and first position and a second position, said flow direction assembly of said second propulsion assembly configured to redirect water flow discharging from said end member of said second propulsion assembly in said second position.

6. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 5 , wherein said flow direction member of said second propulsion assembly includes a first end and a second end, said flow direction member being hollow between said first end and said second end thereof, said flow direction member being curved in shape so as to direct waterflow discharging therefrom towards said second float member when said flow direction member of said second propulsion assembly is in said second position.

7. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 6 , wherein said first propulsion assembly and said second propulsion assembly are independently operable.

8. The seaplane float propulsion system that is operable to provide movement of the seaplane in water as recited in claim 7 , wherein said flow direction member of said first propulsion assembly includes a first end and a second end, said flow direction member of said first propulsion assembly being hollow between said first end and said second end thereof, said flow direction member of said first propulsion assembly being curved in shape so as to direct waterflow discharging therefrom towards said first float member when said flow direction member of said first propulsion assembly is in said second position.

9. A seaplane propulsion system operably coupled to float members of a seaplane so as to provide directional movement of the seaplane in the water wherein the seaplane propulsion system comprises:

a first propulsion assembly, said first propulsion assembly being mounted within one of said float members of the seaplane, said first propulsion assembly configured to intake water thereinto and subsequently eject water therefrom, said first propulsion assembly includes an intake member, said intake member configured to provide intake of water in which the seaplane is floating, said first propulsion assembly including a nozzle housing, said nozzle housing being operably coupled to said intake member, said nozzle housing being hollow allowing water to flow therethrough, said first propulsion assembly further including a water movement member, said water movement member being disposed within said nozzle housing, said water movement member operable to facilitate intake of water through said intake member and discharge the water through an end member of said nozzle housing, said end member being tapered in form, said first propulsion assembly further having a flow direction member, said flow direction member being movably coupled to said nozzle housing, said flow direction member being movable between and first position and a second position, said flow direction assembly configured to direct water flow discharging from said end member in said second position towards the float members;

a second propulsion assembly, said second propulsion assembly being mounted within one of said float members of the seaplane opposite that of the float member in which said first propulsion assembly is mounted, said second propulsion assembly configured to intake water thereinto and subsequently eject water therefrom, said second propulsion assembly further including an intake member, said intake member of said second propulsion assembly configured to provide intake of water in which the seaplane is floating, said second propulsion assembly including a nozzle housing, said nozzle housing of said second propulsion assembly being operably coupled to said intake member of said second propulsion assembly, said nozzle housing of said second propulsion assembly being hollow allowing water to flow therethrough, said second propulsion assembly further including a water movement member, said water movement member of said second propulsion assembly being disposed within said nozzle housing of said second propulsion assembly, said water movement member of said second propulsion assembly operable to facilitate intake of water through said intake member of said second propulsion assembly and discharge the water through an end member of said nozzle housing of said second propulsion assembly, said end member of said second propulsion assembly being tapered in form, said first propulsion assembly further having a flow direction member, said flow direction member of said second propulsion assembly being movably coupled to said nozzle housing, said flow direction member of said second propulsion assembly being movable between and first position and a second position, said flow direction assembly of said second propulsion assembly configured to direct water flow discharging from said end member of said second propulsion assembly in said second position towards the float members; and

wherein the first propulsion assembly and second propulsion assembly are independently operable.

10. The seaplane propulsion system operably coupled to the float members of the seaplane as recited in claim 9 , wherein the flow direction member of the first propulsion assembly and the flow direction member of the second propulsion assembly have a first end and a second end and further being hollow therebetween.

11. The seaplane propulsion system operably coupled to the float members of the seaplane as recited in claim 10 , wherein the flow direction member of the first propulsion assembly and the flow direction member of the second propulsion assembly have a circumferential angle of one hundred and eighty degrees.

12. The seaplane propulsion system operably coupled to the float members of the seaplane as recited in claim 11 , wherein in said second position the flow direction member of the first propulsion assembly and the flow direction member of the second propulsion assembly is aligned with and adjacent to an opening of said end member of said nozzle housing of said first propulsion assembly and said second propulsion assembly.

13. The seaplane propulsion system operably coupled to the float members of the seaplane as recited in claim 12 , wherein in said first position the flow direction member of the first propulsion assembly and the flow direction member of the second propulsion assembly is above said nozzle housing of said first propulsion assembly and said second propulsion assembly.