B64U10/17

Autonomous Package Delivery System
20190079509 · 2019-03-14 ·

The present disclosure is directed to systems and methods for enabling unmanned and optionally-manned cargo delivery to personnel on the ground. For example, an aircraft may be used to provide rapid response cargo delivery to widely separated small units in demanding and unpredictable conditions that pose unacceptable risks to both ground resupply personnel and aircrew. Together with a ground vehicle, packages from the aircraft may be deployed to ground personnel in disbursed operating locations without exposing the ground personnel to the aircraft's open landing zone.

SYSTEM AND METHOD FOR MONITORING A PROPERTY USING DRONE BEACONS
20190066485 · 2019-02-28 ·

Methods, systems, and apparatus, including computer programs encoded on a storage device, for monitoring a property using drone beacons. In one aspect, a monitoring system is disclosed that includes a drone, a drone beacon, a component, a processor, and a computer storage media storing instructions that, when executed by the processor, cause the processor to perform operations. The operations may include obtaining drone beacon data generated by the drone beacon, determining a location of the drone beacon based on the drone beacon data, after determining the location of the drone beacon, transmitting, to the drone, a first instruction to navigate towards the location of the drone beacon, after deploying the drone, obtaining component data generated by the component, and after obtaining the component data, transmitting, to the drone, a second instruction to navigate towards a different location than the location of the drone beacon based on the component data.

Hybrid Powered Unmanned Aircraft System

An unmanned aircraft system has a vertical takeoff and landing flight mode and a forward flight mode. The unmanned aircraft system includes an airframe, a rotor assembly rotatably coupled to the airframe and a propeller rotatably coupled to the airframe. The rotor assembly including at least two rotor blades having tip jets that are operably associated with a compressed gas power system. The propeller is operably associated with an electric power system. In the vertical takeoff and landing flight mode, compressed gas from the compressed gas power system is discharged through the tip jets to rotate the rotor assembly and generate vertical lift. In the forward flight mode, the electric power system drives the propeller to generate forward thrust and autorotation of the rotor assembly generates vertical lift.

RESONANT OPERATING ROTOR ASSEMBLY

The present embodiments disclose a torque dependent and resonant operating thrust-generating rotor assembly including a cyclic pitch control system for controlling tilting moments about a longitudinal rotor blade axis of one or more rotor blades, in order to control the pitch angle of the rotor blades and thereby also the horizontal movements of a helicopter vehicle or a rotary wing aircraft. A rotor torque assembly of the rotor assembly is further configured to operate in resonance, thereby providing a resonant gain effecting a rotational offset in relation to changes in torque generated by the motor.

SPRING SYSTEM VARYING STIFFNESS WITH APPLIED FORCE FOR USE IN A TORQUE DEPENDENT ROTOR OF A ROTARY WING AIRCRAFT

Embodiments disclosed herein present a spring system for use in a torque dependent rotor assembly designed to operate in resonance, where changes in applied torque controls the blade pitch angle and ultimately the movements of a rotary wing aircraft. More specifically, the present invention relates to a spring system used in such a rotor assembly where the stiffness of an associated spring member is allowed to vary in response to the torque applied from a motor to the assembly.

Vehicle system and method for providing services
10185320 · 2019-01-22 · ·

A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

Helicopter rotor icing detection system and method

A system includes a signal monitor to monitor a time rate of change of a revolutions per minute (RPM) trim signal that is received from an RPM command path to control a velocity of a helicopter rotor. An icing detector detects for the presence of ice accumulation on the helicopter rotor by comparing the time rate of change of the RPM trim signal to a predetermined threshold for the time rate of change.

SHELF SPACE ALLOCATION MANAGEMENT DEVICE AND SHELF SPACE ALLOCATION MANAGEMENT METHOD
20190009986 · 2019-01-10 ·

A shelf space allocation management device manages products allocated on shelves aligned in a store by use of an image captured by an imaging device. The shelf space allocation management device acquires an image including a position assumed to be changed in allocation status of each product on each shelf; it determines whether the type and the allocation status of each product reflected in the image match the predetermined type and the predetermined allocation status; then, it determines whether to execute a product allocation inspection based on the determination result. Herein, the shelf space allocation management device specifies a position at which a person conducts a behavior to cause any change in the allocation status of each product on each shelf, and therefore it may control the imaging device to capture an image including the position. It is possible to carry out a product allocation inspection for each period determined in advance depending on the type of each product, or it is possible to carry out a product allocation inspection being triggered by a customer purchasing each product.

SHELF SPACE ALLOCATION MANAGEMENT DEVICE AND SHELF SPACE ALLOCATION MANAGEMENT METHOD
20190009987 · 2019-01-10 ·

A shelf space allocation management device manages products allocated on shelves aligned in a store by use of an image captured by an imaging device. The shelf space allocation management device acquires an image including a position assumed to be changed in allocation status of each product on each shelf; it determines whether the type and the allocation status of each product reflected in the image match the predetermined type and the predetermined allocation status; then, it determines whether to execute a product allocation inspection based on the determination result. Herein, the shelf space allocation management device specifies a position at which a person conducts a behavior to cause any change in the allocation status of each product on each shelf, and therefore it may control the imaging device to capture an image including the position. It is possible to carry out a product allocation inspection for each period determined in advance depending on the type of each product, or it is possible to carry out a product allocation inspection being triggered by a customer purchasing each product.

MOBILE SELF-LEVELING LANDING PLATFORM FOR SMALL-SCALE UAVS

A mobile self-leveling landing platform vehicle is disclosed that includes a landing surface and one or more wheel assemblies. Each wheel assembly includes a wheel, a control arm coupled with the wheel and the body of the landing platform vehicle, and an actuator coupled with the control arm and the body of the platform vehicle. Methods for self-leveling the landing platform vehicle are also disclosed.