Patent classifications
B64F1/22
VEHICLE TOP STRUCTURE
A vehicle includes, on its roof, a first autonomous driving sensor, a second autonomous driving sensor, and a takeoff and landing assist device. The first autonomous driving sensor is disposed adjacent to the front of the vehicle for sensing conditions ahead of the vehicle. The second autonomous driving sensor is disposed adjacent to the rear of the vehicle for sensing conditions behind the vehicle. The takeoff and landing assist device includes a takeoff and landing surface where a flying device takes off and lands. The takeoff and landing assist device is disposed between the first autonomous driving sensor and the second autonomous driving sensor.
TAKEOFF/LANDING ASSIST DEVICE
A position correcting mechanism sandwiches, from both sides, a horizonal leg portion of a flying vehicle that has landed on a takeoff/landing surface of a stage, and moves the flying vehicle on the takeoff/landing surface to a position along a centerline. A grip mechanism grips a supporting leg portion of the flying vehicle. The flying vehicle is moved toward a securing device provided at an edge part of the stage, and an end portion of the horizontal leg portion is inserted into an insertion hole of an insertion part. The flying vehicle is thereby secured on the takeoff/landing surface.
TAKEOFF/LANDING ASSIST DEVICE
A position correcting mechanism sandwiches, from both sides, a horizonal leg portion of a flying vehicle that has landed on a takeoff/landing surface of a stage, and moves the flying vehicle on the takeoff/landing surface to a position along a centerline. A grip mechanism grips a supporting leg portion of the flying vehicle. The flying vehicle is moved toward a securing device provided at an edge part of the stage, and an end portion of the horizontal leg portion is inserted into an insertion hole of an insertion part. The flying vehicle is thereby secured on the takeoff/landing surface.
CABLE SYSTEM FOR A RECHARGING STATION FOR ELECTRIC AIRCRAFTS AND A METHOD OF ITS USE
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.
Vertical takeoff and landing (VTOL) aircraft and system
A VTOL aircraft system includes a first unit having a cockpit, at least one propeller, at least two landing legs and at least two locking mechanisms. A second unit has a housing with a base portion, a first unit engaging portion, and at least two lock mechanism-engaging structure, each corresponding to one of the at least two locking mechanisms of the first unit. The housing of the second unit defines at least one interior cavity with at least one cargo area, a central passage providing access between the first and second unit, and a fuel cell configured around the central passage.
UNMANNED AERIAL VEHICLE MANAGEMENT
A base module may be used to receive and house one or more unmanned aerial vehicles (UAVs) via one or more cavities. The base module receives commands from a manager device and identifies a flight plan that allows a UAV to execute the received commands. The base module transfers the flight plan to the UAV and frees the UAV. Once the UAV returns, the base module once again receives it. The base module then receives sensor data from the UAV from one or more sensors onboard the UAV, and optionally receives additional information describing its flight and identifying success or failure of the flight plan. The base module transmits the sensor data and optionally the additional information to a storage medium locally or remotely accessible by the manager device.
Ground support station for aerial vehicles
A ground station for aerial vehicles including a protective casing, at least one charging mechanism, and an extendable landing pad. The extended landing pad is operable to transition between a closed configuration having dimensions suitable to be contained within said protective casing, and an open configuration having dimensions suitable to land the aerial vehicle.
Apparatus, Systems and Methods for Unmanned Aerial Vehicles
The disclosed inventions include personal Unmanned Aerial Vehicles (UAV's) and UAV universal docking ports “docking ports” to be incorporated into and/or attached to headwear, including helmets, hard hats and hats and face masks, as well as footwear including boots and shoes, clothing and outerwear, devices, gear and equipment, land, air, water and space vehicles, buildings, wireless towers and other mobile or stationary objects and surfaces referred to collectively as “docking stations”. A docking station may have one or more docking ports for docking, networking and charging or refueling compact personal UAVs, and for providing data communications between said UAVs and other electronic devices that remain with the person while the UAV is in flight or driving or landed on terrain. Said docking ports may also incorporate wireless power transmission for remote wireless charging of one or more UAV's. Supplemental power for recharging said UAVs when docked may be supplied by integrated battery(s) in said docking port or me be provided directly from the docking station or other connected power source.
System and method for collision avoidance
A method implemented using at least one processor includes receiving a plurality of images acquired from a plurality of image sensors disposed on a vehicle configured to engage an aircraft for ground operations. The method further includes determining at least one parameter about a potential obstacle based on the plurality of images and a machine vision algorithm. The method also includes generating an alert signal based on the at least one parameter, useful for avoiding collision of the aircraft.
Modular collapsible and portable drone in a box
A ground station for an unmanned aerial vehicle (UAV) includes a box assembly, a hatch assembly, and a landing pad assembly. The hatch assembly is pivotably coupled to the box assembly. The landing pad assembly is movably coupled to the box assembly and is movably coupled to the hatch assembly.