System and method for adjustable ballast
A movable ballast system for an aircraft includes first and second ballast docks secured to the aircraft. The first ballast dock includes a first housing and a first ballast tray secured within the first housing. The first ballast tray includes a plurality of channels. The second ballast dock is positioned aft of a CG of the aircraft and includes a second housing and a second ballast tray secured within the second housing. The second ballast tray includes a plurality of channels. The movable ballast system includes a plurality of movable ballasts, each movable ballast of the plurality of movable ballasts being configured to fit within at least one channel of each of the plurality of channels of the first and second ballast trays.
1. A ballast dock comprising:
a housing;
a first ballast tray secured within the housing and comprising a plurality of channels; and
a plurality of movable ballasts, each movable ballast of the plurality of movable ballasts comprising a side configured to fit within at least one channel of the plurality of channels.
2. The ballast dock of claim 1 , comprising:
a second ballast tray secured within the housing and comprising a plurality of channels; and
wherein opposing channels of the first and second ballast trays form bays configured to receive a movable ballast of the plurality of movable ballasts.
3. The ballast dock of claim 1 , wherein the first ballast tray is made of a material selected from the group consisting of rubbers, plastics, and polymers.
4. The ballast dock of claim 1 , wherein the first ballast tray is coated with a material selected from the group consisting of rubbers, plastics, and polymers.
5. The ballast dock of claim 1 , wherein each channel of the plurality of channels comprises a different width and depth so that only one movable ballast of the plurality of movable ballasts fits within a particular channel of the plurality of channels.
6. The ballast dock of claim 1 , comprising a mounting plate configured to secure the ballast dock to an aircraft.
7. The ballast dock of claim 1 , comprising:
a pin; and
wherein each of the housing and the plurality of movable ballasts include a bore through which the pin extends.
8. The ballast dock of claim 1 , wherein the housing comprises a cut out configured to expose a portion of the plurality of movable ballasts when the plurality of movable ballasts are inserted into the ballast dock.
9. The ballast dock of claim 1 , wherein the plurality of movable ballasts comprises a first, second, and third ballast.
10. The ballast dock of claim 9 , wherein the first and second ballasts have a first weight and the third ballast has a second weight.
11. The ballast dock of claim 1 , wherein each movable ballast of the plurality of movable ballasts has a different weight.
12. A movable ballast system for an aircraft comprising:
a first ballast dock secured to the aircraft and comprising a first housing and a first ballast tray secured within the first housing, the first ballast tray comprising a plurality of channels;
a second ballast dock secured to the aircraft and positioned aft of a CG of the aircraft, the second ballast dock comprising a second housing and a second ballast tray secured within the second housing, the second ballast tray comprising a plurality of channels; and
a plurality of movable ballasts, each movable ballast of the plurality of movable ballasts being configured to fit within at least one channel of each of the plurality of channels of the first and second ballast trays.
13. The movable ballast system of claim 12 , comprising:
wherein the first ballast dock comprises a third ballast tray secured within the first housing and comprising a plurality of channels;
wherein the second ballast dock comprises a fourth ballast tray secured within the second housing and comprising a plurality of channels; and
wherein opposing channels of the first and third ballast trays and opposing channels from the second and fourth ballast trays form bays configured to receive a movable ballast of the plurality of movable ballasts.
14. The movable ballast system of claim 12 , wherein the first and second ballast trays are made of a material selected from the group consisting of rubbers, plastics, and polymers.
15. The movable ballast system of claim 12 , wherein the first and second ballast trays are coated with a material selected from the group consisting of rubbers, plastics, and polymers.
16. The movable ballast system of claim 12 , wherein each channel of the plurality of channels of the first and second ballast trays comprises a different width and depth so that only one movable ballast of the plurality of movable ballasts fits within a particular channel of the plurality of channels.
17. The movable ballast system of claim 12 , wherein the first ballast dock comprises a mounting plate configured to secure the first ballast dock to the aircraft.
18. The movable ballast system of claim 12 , comprising:
wherein the first ballast dock comprises a first pin and the second ballast dock comprises a second pin;
wherein the first housing and the plurality of movable ballasts comprise bores configured be coaxially aligned when the plurality of movable ballasts are inserted into the first housing and the second housing and the plurality of movable ballasts comprise bores configured to be coaxially aligned when the plurality of movable ballasts are inserted into the second housing; and
wherein the first pin is configured to extend through the bore of the first housing and the second pin is configured to extend through the bore of the second housing.
19. The movable ballast system of claim 12 , wherein each of the first and second housings comprise a cut out configured to expose a portion of the plurality of movable ballasts when the plurality of movable ballasts are inserted into the ballast dock.
20. The movable ballast system of claim 12 , wherein each movable ballast of the plurality of movable ballasts has a unique weight.