B64U20/10

Aircraft system for reduced observer visibility

An aircraft apparatus is disclosed that has a fuselage boom having proximal and distal ends, a wing coupled to a proximal end of the fuselage boom and at least one transparent stabilizer coupled to a distal end of the fuselage boom.

LAW ENFORCEMENT DRONE
20180037321 · 2018-02-08 ·

A law enforcement drone system is provided. The system features an unmanned aerial vehicle, having a wireless transceiver, an airframe, a propulsion system, a navigation mechanism, a processor, a memory, a power source, and at least one fuel tank. The system also features a control system having a wireless transceiver, an input device, capable of receiving a user's input and converting the user's input to electrical signals, a processor, and a memory. The control system is in wireless communication with the vehicle such that the control system is capable of utilizing the propulsion system in substantially real-time.

Post-type apparatus for containing and charging unmanned vertical take-off and landing aircraft and method of containing and charging unmanned vertical take-off and landing aircraft using the same

An apparatus and method for containing and charging an unmanned VTOL aircraft are disclosed. The apparatus for containing and charging an unmanned VTOL aircraft includes a post, an extended member, a cover, a fastening unit, and a charging unit. The post is placed on a ground. The extended member is connected to the post. The cover is provided on the extended member, and is configured to be opened or closed in order to contain and protect the unmanned VTOL aircraft. The fastening unit is provided in the cover, and is configured to fasten the unmanned VTOL aircraft. The charging unit is provided in the fastening unit, and is configured to charge the unmanned VTOL aircraft.

ROTOR CRAFT NOISE CANCELLATION SYSTEM AND METHOD
20250022451 · 2025-01-16 ·

Rotor noise cancellation through the use of mechanical means for a personal aerial drone vehicle. Active noise cancellation is achieved by creating an antiphase amplitude wave by modulation of the propeller blades, by utilizing embedded magnets through an electromagnetic coil encircling the propeller blades. A noise level sensor signals the rotor control system to adjust the frequency of the electromagnetic field surrounding the rotor and control the speed of the rotor. An additional method comprises of incorporating a phase lock loop within the control system configured to determine the frequencies corresponding to the rotors and generate corrective audio signals to achieve active noise cancellation.

DRONE DEVICE SECURITY SYSTEM FOR PROTECTING A PACKAGE
20170293301 · 2017-10-12 ·

A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the information by comparing the information with source information. The social networking fact checking system automatically monitors information, processes the information, fact checks the information and/or provides a status of the information, including automatically modifying a web page to include the fact check results. The fact checking system is able to be implemented utilizing a drone device. The drone device is able to be implemented in conjunction with a security system.

DRONE COORDINATED SHIELDING, CAMOUFLAGING, AND DECOYING
20250044802 · 2025-02-06 · ·

Methods, Systems, and Apparatus for coordinating drones to communicate with reduced signal to noise, harvest energy, provide camouflage, provide decoying, or provide protective shielding.

DRONE DEVICE SECURITY SYSTEM
20170203840 · 2017-07-20 ·

A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the information by comparing the information with source information. The social networking fact checking system automatically monitors information, processes the information, fact checks the information and/or provides a status of the information, including automatically modifying a web page to include the fact check results. The fact checking system is able to be implemented utilizing a drone device.

DRONE DEVICE SECURITY SYSTEM
20170203841 · 2017-07-20 ·

A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the information by comparing the information with source information. The social networking fact checking system automatically monitors information, processes the information, fact checks the information and/or provides a status of the information, including automatically modifying a web page to include the fact check results. The fact checking system is able to be implemented utilizing a drone device.

High-Speed Aircraft and Aircraft Having Greater Lift
20170197697 · 2017-07-13 ·

Disclosed in the present invention is a high-speed aircraft, comprising a shell and an engine, an outer fluid channel and an inner fluid channel being arranged in succession within the shell, the outer fluid channel and the inner fluid channel respectively connecting to the exterior by means of their own air vent; the outer fluid channel is connected to an air suction port of the engine, such that the pressure difference produced by the flow rate within the outer fluid channel being greater than the flow rate within the inner fluid channel acts as the driving force source of the aircraft. Also disclosed in the present invention is an aircraft having greater lift. The present invention provides an innovative method and apparatus for a driving force source obtained from fluid resistance, thus changing the mutual contradiction of a traditional driving apparatus directing external force to itself whilst also needing to use more driving force to overcome fluid resistance. The present invention changes the direction of fluid pressure, altering the condition that the amount of pressure dictates the size of the driving force source obtained; on this basis, a novel greater first and second lift source and driving force source are produced for use in an aircraft.

POST-TYPE APPARATUS FOR CONTAINING AND CHARGING UNMANNED VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND METHOD OF CONTAINING AND CHARGING UNMANNED VERTICAL TAKE-OFF AND LANDING AIRCRAFT USING THE SAME

An apparatus and method for containing and charging an unmanned VTOL aircraft are disclosed. The apparatus for containing and charging an unmanned VTOL aircraft includes a post, an extended member, a cover, a fastening unit, and a charging unit. The post is placed on a ground. The extended member is connected to the post. The cover is provided on the extended member, and is configured to be opened or closed in order to contain and protect the unmanned VTOL aircraft. The fastening unit is provided in the cover, and is configured to fasten the unmanned VTOL aircraft. The charging unit is provided in the fastening unit, and is configured to charge the unmanned VTOL aircraft.