Abstract: Aspects relate to a connector and methods of use for charging an electric aircraft. An exemplary connector includes a housing configured to mate with a port of an electric aircraft, where the housing includes a fastener for removable attachment with the electric aircraft port, at least a high-voltage conductor configured to conduct a high-voltage electrical power, at least a low-voltage conductor, configured to conduct a low-voltage electrical power, at least a control signal conductor configured to conduct a control signal, at least a ground conductor configured to conduct to a ground, at least a cooling channel configured to contain a flow of a coolant, and at least a proximity signal conductor configured to conduct a proximity signal indicative of attachment with the electric aircraft port when the housing is mated with the port.

Abstract: A system and method for a recharging station including a landing pad, a rechargeable component coupled to the landing pad, a power delivery unit configured to deliver powerfrom a power supply unit or power storage unit to the recharging component, and a support component coupled to the bottom of the landing pad.

Abstract: The present disclosure is generally related to a system and method for a recharging station for an electric aircraft. The system may include a landing pad and a recharging component coupled to the landing pad. Further, the system may include a power delivery unit configured to deliver stored power from a power supply unit to the recharging component and wherein the floating platform is in direct contact with a body of water.

Abstract: A system and method for a recharging station including an elevated landing pad, a rechargeable component coupled to the elevated landing pad, a power delivery unit configured to deliver power from a power supply unit or power storage unit to the recharging component, and a support component coupled to the bottom of the elevated landing pad.

Abstract: An assembly for minimizing the disengagement of a chain from a chain ring is disclosed. The assembly includes a bracket and a chain guide assembly. The chain guide assembly includes a chain guide, a first lock and a second lock. The first lock and the second lock are capable of being actuated separately to lock the chain guide into a position in each of a first and second orientation relative to the bracket.

Abstract: An assembly for minimizing the disengagement of a chain from a chain ring is disclosed. The assembly includes a bracket and a chain guide assembly. The chain guide assembly includes a chain guide, a first lock and a second lock. The first lock and the second lock are capable of being actuated separately to lock the chain guide into a position in each of a first and second orientation relative to the bracket.