Systems and methods for folding wings on an aircraft

A system for folding wings on an aircraft, the system comprising:

• a blended wing body, wherein the blended wing body comprises:
• a main body;
• and
• at least a wing comprising an outboard flight component;
• a hinge located on the blended wing body and configured to allow folding of the at least a wing, wherein the hinge is inboard relative to the outboard flight component;
• an actuation system configured to fold the at least a wing;
• a controller configured to control the at least an actuation system;
• and
• a transmission system comprising at least a service loop, wherein the transmission system is configured to communicate with the outboard flight component and permit folding of the at least a wing by the service loop not interfering with movement of the at least a wing during folding.