Dynamic energy absorbing seat
Embodiments relate to dynamic stroking seats for vertical take-off and landing (VTOL) aircraft. Seat ballast tanks are attached to aircraft seats. The seats are sprung by a fixed or variable load energy absorption system. The weight of a user is determined and assigned to a corresponding seat of the user. Based on the weight of the user, the fluid level in the ballast tank is monitored and adjusted to achieve a target weight range.
1 . A cooling system comprising:
a seat;
a battery;
a fluid line in fluid communication with the seat and the battery;
a valve coupled with the seat and in fluid communication with the fluid line; and
a controller operatively coupled with the valve and the battery, the controller configured to perform actions comprising:
monitoring a state of the battery;
controlling the valve to allow a flow of fluid in a first direction from the seat to the battery via the fluid line based on the state of the battery, wherein the flow of the fluid in the first direction from the seat to the battery allows for heat dissipation from the battery; and
controlling the valve to allow the flow of fluid in a second direction opposite the first direction to the seat.
2 . The cooling system of claim 1 , wherein the state of the battery is one of a charging state or a discharging state.
3 . The cooling system of claim 1 , further comprising:
a ballast tank coupled to the seat, the ballast tank defining a cavity for receiving the fluid;
a reservoir in fluid communication with the ballast tank; and
a pump operatively coupled with the reservoir and the ballast tank.
4 . The cooling system of claim 3 , wherein the controller is further configured to activate the pump to allow for the flow of the fluid back to the seat from the battery to dissipate heat from the battery.
5 . The cooling system of claim 3 , further comprising a return line in fluid communication with the valve and the reservoir.
6 . The cooling system of claim 3 , wherein the fluid is one of coolant or fire suppressant.
7 . The cooling system of claim 3 , wherein the ballast tank is coupled to a seat portion of a seat frame of the seat.
8 . The cooling system of claim 3 , wherein the ballast tank is coupled to a back portion of a seat frame of the seat.
9 . A method for controlling a cooling system comprising a seat, a battery, a fluid line in fluid communication with the seat and the battery, a valve coupled with the seat and in fluid communication with the fluid line, and a controller operatively coupled with the valve and the battery, the method comprising:
monitoring a state of the battery;
controlling the valve to allow a flow of fluid in a first direction from the seat to the battery via the fluid line based on the state of the battery, wherein the flow of the fluid in the first direction from the seat to the battery allows for heat dissipation from the battery; and
controlling the valve to allow the flow of fluid in a second direction opposite the first direction to the seat.
10 . The method of claim 9 , wherein the state of the battery is one of a charging state or a discharging state.
11 . The method of claim 9 , wherein the cooling system further comprises:
a ballast tank coupled to the seat, the ballast tank defining a cavity for receiving the fluid;
a reservoir in fluid communication with the ballast tank; and
a pump operatively coupled with the reservoir and the ballast tank.
12 . The method of claim 11 , wherein the method further comprises activating the pump to allow for the flow of the fluid back to the seat from the battery to dissipate heat from the battery.
13 . The method of claim 11 , wherein the cooling system further comprises a return line in fluid communication with the valve and the reservoir.
14 . The method of claim 11 , wherein the fluid is one of coolant or fire suppressant.
15 . The method of claim 11 , wherein the ballast tank is coupled to a seat portion of a seat frame of the seat.
16 . The method of claim 11 , wherein the ballast tank is coupled to a back portion of a seat frame of the seat.