Wing-in-ground effect vehicles and uses thereof
Wing-in-ground effect (WIG) vehicles are disclosed herein. Hovercraft takeoff and landing modes are disclosed herein. Uses of WIG vehicles, including for maritime monitoring, are disclosed herein.
1 . A vehicle having a hovercraft mode and a flight mode, the vehicle comprising:
at least an aerodynamically-modifiable airfoil comprising:
an upper surface;
a lower surface;
at least one channel extending from the upper surface to the lower surface for introducing fluid underneath the lower surface of the airfoil; and
a moveable flap configured to capture fluid introduced through the at least one channel when the moveable flap is deployed, thereby generating a cushion of fluid underneath the lower surface of the airfoil and providing a hovercraft mode for the vehicle, and the moveable flap configured to avoid generating the cushion of fluid underneath the lower surface of the airfoil when the moveable flap is undeployed, thereby providing a flight mode for the vehicle, wherein each airfoil of the at least an airfoil further comprising a nozzle extending downward from the lower surface of the airfoil in fluidic communication with the channel of the airfoil.
2 . The vehicle of claim 1 , further comprising one or more blowers operably connected to the at least one channel and configured to selectively introduce fluid underneath the lower surface of the airfoil.
3 . The vehicle of claim 1 , wherein the moveable flap is configured to parallel the lower surface of the airfoil when the moveable flap is undeployed.
4 . The vehicle of claim 1 , wherein the moveable flap is configured to tuck against the lower surface of the airfoil when not deployed.
5 . The vehicle of claim 1 , wherein the moveable flap is configured to at least partially block openings of the one or more channels in the lower surface of the airfoil.
6 . The vehicle of claim 1 , wherein the moveable flap comprises a flexible material.
7 . The vehicle of claim 1 , wherein the moveable flap comprises a rigid material.
8 . The vehicle of claim 1 , wherein deployment of the moveable flap is at least partially controlled by a pressure differential on opposing surfaces of the moveable flap.
9 . The vehicle of claim 1 , wherein:
the airfoil has a forward edge and a rearward edge; and
the moveable flap is attached to the rearward edge.
10 . The vehicle of claim 1 , wherein:
the airfoil has a forward edge and a rearward edge;
the channel has an opening in the lower surface; and
the opening is oriented toward the rearward edge.
11 . The vehicle of claim 1 , wherein the nozzle for each airfoil is extendable and retractable.
12 . The vehicle of claim 1 , wherein the channel of each airfoil channel comprises a straight tube.
13 . The vehicle of claim 1 , wherein the channel of each airfoil channel comprises a swept tube wherein a lower orifice of the channel is offset relative to an upper orifice of the channel.
14 . The vehicle of claim 1 , wherein the at least an airfoil further comprises a plurality of airfoils.
15 . The vehicle of claim 14 , wherein the plurality of airfoils further comprises three airfoils.
16 . A vehicle having a hovercraft mode and a flight mode, the vehicle comprising:
at least an aerodynamically-modifiable airfoil comprising:
an upper surface;
a lower surface;
at least one channel extending from the upper surface to the lower surface for introducing fluid underneath the lower surface of the airfoil; and
a moveable flap configured to capture fluid introduced through the at least one channel when the moveable flap is deployed, thereby generating a cushion of fluid underneath the lower surface of the airfoil and providing a hovercraft mode for the vehicle, and the moveable flap configured to avoid generating the cushion of fluid underneath the lower surface of the airfoil when the moveable flap is undeployed, thereby providing a flight mode for the vehicle, wherein each airfoil includes a selectively openable vent located in the upper surface of the airfoil and rearward of an upper orifice of the channel and wherein the vent is in fluidic communication with the channel, whereby when the vent is in an open position, fluid provided by the one or more blowers into the channels exits at least partially through the vent and over the upper surface of the airfoil and thereby generates lift for the vehicle.
17 . The vehicle of claim 16 , wherein each airfoil of the at least an airfoil further comprising a nozzle extending downward from the lower surface of the airfoil in fluidic communication with the channel of the airfoil.
18 . The vehicle of claim 17 , wherein the nozzle for each airfoil is extendable and retractable.
19 . A method of hovering a vehicle, the method comprising:
providing at least an aerodynamically modifiable airfoil, wherein the at least an airfoil comprises:
an upper surface;
a lower surface;
at least one channel extending from the upper surface to the lower surface for introducing fluid underneath the lower surface of the airfoil; and
a moveable flap configured to capture fluid introduced through the at least one channel when the moveable flap is deployed, thereby generating a cushion of fluid underneath the lower surface of the airfoil and providing a hovercraft mode for the vehicle, and the moveable flap configured to avoid generating the cushion of fluid underneath the lower surface of the airfoil when the moveable flap is undeployed, thereby providing a flight mode for the vehicle, wherein each airfoil of the at least an airfoil further comprising a nozzle extending downward from the lower surface of the airfoil in fluidic communication with the channel of the airfoil; and
blowing a fluid through a channel extending from an upper surface to a lower surface of an airfoil with sufficient volume and pressure to lift the vehicle off of a surface.
20 . The vehicle of claim 19 , wherein the nozzle for each airfoil is extendable and retractable.