Abstract: Various examples of an aerial vehicle and/or aerial vehicle system are disclosed. In one example, an aerial vehicle configured to be coupled to a main aerial vehicle is disclosed. The aerial vehicle may include a propulsion unit coupled to the body to enable independent thrust generation by the aerial vehicle.

Abstract: A cooling system is disclosed. The cooling system can include a flow path including a main path and a secondary path. The secondary path can have an inlet and an outlet. The inlet can be in fluid communication with a first portion of the main path and the outlet can be in fluid communication with a second portion of the main path. The cooling system can include a passive fluid flow controller. The passive fluid flow controller can be positioned in the main path between the first portion and the second portion. The passive fluid flow controller can adjust an amount of a coolant that is routed to the secondary path from the main path through the inlet of the secondary path. The passive fluid flow controller can impede a particle from entering the secondary path via the inlet of the secondary path.

Abstract: A thermal system for a vehicle, including a first vent (202) and a second vent (206) connected to at least one air source corresponding to an HVAC unit, wherein each vent (202, 206) receives air from the at least one air source to produce a plane of air, the first and second vents (202, 206) are configured to respectively redirect a first plane of air and a second plane of air to intersect on or along a portion of a blending surface (204) to form a combined air jet which can be directed into a cabin of the vehicle and the 208 blending surface can be a flat, convex, or concave display or instrument panel.