Patent classifications
B64F1/36
System and method for communicating a pre-charging package stream of an electric aircraft
A system for communicating at least a pre-charging datum for an electric vehicle, the system including an electric aircraft, wherein the electric aircraft comprises, a sensor, wherein the sensor is configured to detect a connection with a charging connector, at least a battery pack, wherein the at least a battery pack including a plurality of battery cells, an aircraft recharging component, the aircraft recharging component including an aircraft side recharging component, wherein the aircraft side recharging component is configured to form a charge connection with the charging connector, a controller, wherein the controller is configured to generate a battery parameter set as a function of the connection with the charging connector, and transmit the battery parameter set to the charging connector.
Iteratively mapping-and-approaching an urban area
Systems and methods to iteratively map-and-approach an urban area using flying drones. Each of the iterations includes drones flying over the urban area using terrain-following techniques in conjunction with a 3D model that was updated in previous iterations, in which flight paths are defined in conjunction with the 3D model so as to stay away of ground-related features appearing in the 3D model. As the iteration processes progresses, the model becomes increasingly accurate with additional details about the ground related features, thereby allowing the drones to safely approach the ground related features. The iterations converge into a low altitude flight over roads in the urban area, as flying at low altitudes over roads allows the drones to gather information of interest about buildings, infrastructure and assets, in which such information would be difficult to obtain using other techniques. Close proximity to ground related features allows drone delivery functions as well.
GPU FOR THE PROVISION OF ELECTRICAL ENERGY FOR AIRCRAFT
A ground power unit provides electrical energy for aircraft and a method maintains and operates the ground power unit. The ground power unit includes a base frame, a cable system formed in the base frame, at least one rectifier module for converting an input alternating voltage applied to a rectifier module input side into an intermediate direct voltage output at a rectifier module output side, wherein the rectifier module output side is coupled to an intermediate circuit conductor and at least one inverter module for converting the intermediate direct voltage applied to an inverter module input side into an output alternating current output at an inverter module output side, wherein the inverter module input side is coupled to an intermediate circuit conductor. The rectifier module and the inverter module are each realized as structurally-independent units, which can be replaced individually and independently of the base frame.
Spraying device for liquid means of chemical treatment with replaceable liquid subsystem and spraying systems on the basis thereof
The invention is intended for the organization of an automated process for spraying of liquid means of chemical treatment from unmanned vehicles, for example, in precise farming systems. The invention provides the use of a replaceable, marked and hermetically sealed liquid subsystem with integrated pumping chambers in a spraying device together with an integrated self-diagnosis system allowing to ensure personnel safety and the accounting of the resources of main components of the spraying device. All this in combination enables to create fully automated spraying systems.
Spraying device for liquid means of chemical treatment with replaceable liquid subsystem and spraying systems on the basis thereof
The invention is intended for the organization of an automated process for spraying of liquid means of chemical treatment from unmanned vehicles, for example, in precise farming systems. The invention provides the use of a replaceable, marked and hermetically sealed liquid subsystem with integrated pumping chambers in a spraying device together with an integrated self-diagnosis system allowing to ensure personnel safety and the accounting of the resources of main components of the spraying device. All this in combination enables to create fully automated spraying systems.
NOVEL AIRPORT CAPABLE OF SAVING ENERGY AND RESOURCES AND IMPROVING TAKE-OFF AND LANDING SAFETY OF AIRPLANE
The present invention discloses an integrated airport design. The runways are designed in an elevated curved shape. The middles of landing runways and take-off runways are designed as an overhead parking apron, and the terminal building is below the runways. Therefore, the usable area of the whole airport is increased. The length of each elevated curved runway is lengthened comparing to the traditional straight runway within the same area. In addition, the downhill take-off runway can enhance take-off operation and reduce the fuel consumption. Thus, the existing land resources can be used to the maximum extent.
NOVEL AIRPORT CAPABLE OF SAVING ENERGY AND RESOURCES AND IMPROVING TAKE-OFF AND LANDING SAFETY OF AIRPLANE
The present invention discloses an integrated airport design. The runways are designed in an elevated curved shape. The middles of landing runways and take-off runways are designed as an overhead parking apron, and the terminal building is below the runways. Therefore, the usable area of the whole airport is increased. The length of each elevated curved runway is lengthened comparing to the traditional straight runway within the same area. In addition, the downhill take-off runway can enhance take-off operation and reduce the fuel consumption. Thus, the existing land resources can be used to the maximum extent.
High Efficiency Flight Line Cooling, Heating, and Dehumidification System
An HVAC system has a duct with an inlet and an outlet. A first supercharger is disposed in the duct. A second supercharger is disposed in the duct in parallel with the first supercharger. A gearbox has a first output shaft coupled to the first supercharger and a second output shaft of the gearbox coupled to the second supercharger. A first evaporation coil is disposed in the duct between the supercharger and inlet. A second evaporation coil is disposed in the duct between the supercharger and outlet. A heater is disposed in the duct between the supercharger and outlet.
COMMAND CENTER FOR DRONE MANAGEMENT
An operations platform includes a structure configured to house and transport drones and a storage facility configured to store the drones within the structure. The operations platform includes a lift or conveyor configured to move the plurality of drones to/from a launching area. In some implementations, the operations platform may also include at least one robotic element configured to move the drones to and from the storage facility.
COMMAND CENTER FOR DRONE MANAGEMENT
An operations platform includes a structure configured to house and transport drones and a storage facility configured to store the drones within the structure. The operations platform includes a lift or conveyor configured to move the plurality of drones to/from a launching area. In some implementations, the operations platform may also include at least one robotic element configured to move the drones to and from the storage facility.