US 11,993,397 B1 · System and a method for preconditioning a power source of an electric aircraft

Abstract

A system and a method for preconditioning a power source of an electric aircraft are disclosed. The system may include a ground service equipment, wherein the ground service equipment may be configured to precondition a power source of an electric aircraft. The ground service equipment may include a positive pressure pump configured to pump a coolant into the power source and a negative pressure pump configured to pump the coolant out of the power source. The system may include a controller communicatively connected to the ground service equipment. The controller may be configured to control the positive pressure pump and control the negative pressure pump.

Claims19

Dependent claims

A system for preconditioning a power source of an electric aircraft, wherein the system comprises:

a ground service equipment, wherein the ground service equipment is configured to precondition a power source of an electric aircraft and comprises:
a positive pressure pump configured to pump a coolant into the power source;
and
a negative pressure pump configured to pump the coolant out of the power source;
and
a controller communicatively connected to the ground service equipment, wherein the controller is configured to:
control the positive pressure pump to pump the coolant into the power source;
and
control the negative pressure pump to pump the coolant out of the power source.

6 more elements

Dependencies are inferred from the claim text.

System and a method for preconditioning a power source of an electric aircraft

Life of this patent

System and a method for preconditioning a power source of an electric aircraft

Life of this patent

Abstract

Claims19