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Patent # Description
US-1,011,2732 Formatting container
A container for use in a scale or combination scale, for example, which is used as formatting container includes two or more side walls, whose position with...
US-1,011,2731 Truss structure optimization techniques
Design of a 3-D truss structure, including a plurality of coupling nodes and a plurality of struts, is optimized by performing a quantitative optimization of an...
US-1,011,2730 System and methods for remote monitoring drones and aerial vehicles for security and health monitoring purposes
One or more methods for remotely estimating a drone's weight during flying are contemplated. It is possible to utilize a long range laser Doppler Vibrometer or...
US-1,011,2729 Vibration absorbing device for flexbeams
A replacement vibration absorbing device for replacing a wear wrap on a flexbeam includes a sleeve having a plurality of layers of vibration absorbing material,...
US-1,011,2728 Drone charging stations
A charging system for a drone carrying a passenger pod has a base structure connected to a power grid, a row of substantially planar wireless charging pads...
US-1,011,2727 Actuator monitoring system using inertial sensors
An actuator monitoring and response system is disclosed. Sensor data is received from an inertial measurement unit on a vehicle. An observed attitude and an...
US-1,011,2726 Optical health monitoring for aircraft overheat and fire detection systems
Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic...
US-1,011,2725 Electrically heated filter screens
A heating body for an electrically heated filter screen includes a heater element having an outer surface and a metallic protective layer having an inner...
US-1,011,2724 Apparatus for preventing spark propagation
A hydraulic joint is disclosed. The hydraulic joint includes a tube, a hydraulic fitting, and a tip seal. The hydraulic fitting may be positioned around the...
US-1,011,2723 Method and a device for stopping a turboshaft engine in nominal operation
A method of stopping a turboshaft engine in flight. During a power reduction step, a current power of the engine for stopping is reduced to reach zero power,...
US-1,011,2722 Power control for propeller-driven aircraft
A method of controlling an engine for a propeller-driven aircraft, including setting an initial maximum power limit, wherein the initial maximum power limit is...
US-1,011,2721 Parachute deployment system for an unmanned aerial vehicle
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed...
US-1,011,2720 Method and apparatus for a homogeneous thermoplastic leg support
A leg support includes a support element. A reinforcing element is disposed on the support element. The support element is chemically compatible with the...
US-1,011,2718 Energy unit, cabin movement and vehicle, as well as a method for supplying the cabin of a vehicle with a...
The invention relates in particular to an energy unit (1) for producing an operating material on board a vehicle, comprising a fuel cell unit (2) with at least...
US-1,011,2717 Pivot bin assembly with two part pivot axle
An aircraft storage bin that includes an upper housing with first and second side panels, a bucket that includes a bottom and first and second sides, a first...
US-1,011,2716 Method, system, and executable program product for controlling lighting
A lighting control system includes a sensor to generate a signal representative of at least one of a position of a seat, a presence of passenger in the seat,...
US-1,011,2715 Signaling print substances
An example unmanned aerial vehicle includes an electromagnetic radiation (EMR) sensor. The EMR sensor detects a signal indicative of a substance to print. The...
US-1,011,2714 Signaling print locations
An example unmanned aerial vehicle includes an electromagnetic radiation (EMR) sensor. The EMR sensor detects a signal indicative of a direction of emission of...
US-1,011,2713 Back mounted flight machine
A back mounted flight machine comprises a frame comprising a connecting bracket, a pair of lateral arms extending from the connector bracket, and an engine...
US-1,011,2712 Multi-use UAV docking station systems and methods
Systems and methods for providing a series of multiuse UAV docking stations are disclosed. The docking stations can be networked with a central control and a...
US-1,011,2711 Aircraft deployment and retrieval of unmanned aerial vehicles
An aircraft system incorporates a first aircraft having a grappling device including a first gripper with a first actuator and a second gripper with a second...
US-1,011,2710 Motor vehicle with captive aircraft
A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on...
US-1,011,2709 Vibration control with active lag damper
A rotor system includes a hub assembly, a first, second, and third rotor blade rotatably attached to the hub assembly, a first, second, and third damper...
US-1,011,2708 Weight efficient servo attachment scheme for rigid coaxial rotor control system
A mounting assembly for connecting a first surface to a second surface and for holding a first servo which moves an adjacent first component is provided...
US-1,011,2707 Remotely controlled co-axial rotorcraft for heavy-lift aerial-crane operations
An unmanned rotorcraft has a lift module having a propulsion system and coaxial rotors driven in rotation by the propulsion system. The rotorcraft includes a...
US-1,011,2706 Unmanned aerial vehicles for collaboration
A mobile telepresence system may include a frame, a propulsion system operably coupled to the frame to propel the frame through a designated space, a screen...
US-1,011,2705 Off-board gyrocopter take-off systems and associated methods
Off-board gyrocopter take-off systems and associated methods are disclosed. A representative method includes restraining a gyrocopter from vertical and lateral...
US-1,011,2704 Electric braking system with power conservation and method of operating the same
A method of operating electric brakes (30, 32, 34) on an aircraft (10) in a low power mode of operation includes determining if the aircraft is in a first...
US-1,011,2703 Drive system for landing gear and drive system control method
A method for controlling a separation between rotational axes of a pair of meshing gears is disclosed. A parameter indicative of a transmission error through...
US-1,011,2702 Hard-landing detection system
A hard-landing detection system includes a wheel assembly, a shock strut mechanically coupled to the wheel assembly and to landing gear structure of the landing...
US-1,011,2701 Aircraft landing gear door actuation mechanism with integrated emergency actuation assembly
Landing gear doors may be opened in an emergency event, e.g., a failure of the normal landing gear actuation system that requires a gravity free-fall...
US-1,011,2700 Multi-mode mobility micro air vehicle
A multi-mode mobility micro air vehicle (MAV) accomplishes ground locomotion by hopping on a retractable leg. The hopping is translated into forward locomotion...
US-1,011,2699 Method of preloading an aircraft assembly, a preloading tool and an aircraft assembly
A method of preloading an aircraft assembly involving a step of operating an extendible preloading tool to move a landing gear strut to decrease the distance...
US-1,011,2698 Deployment mechanism
A deployment or hinge mechanism and, more particularly, a compact unmanned aerial vehicle (UAV) wing deployment mechanism is provided. The deployment mechanism...
US-1,011,2697 Aircraft with thrust vectoring tail
An aircraft is provided and includes an airframe having an upper section and a tail section, a main rotor assembly operably disposed at the upper section and...
US-1,011,2696 Stabilizer sacrificial surfaces
An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within the aft fuselage. A burst zone is defined about the turbine...
US-1,011,2695 Receptacle, payload assembly and related methods for an aircraft
An aircraft includes a support structure, an outer skin coupled to the support structure, and a port that defines a break in the support structure and extends...
US-1,011,2694 Self-righting aeronautical vehicle and method of use
A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right...
US-1,011,2693 Internal combustion engine
The invention provides an internal combustion engine comprising a piston mounted for reciprocating linear motion within a cylinder along a cylinder axis. The...
US-1,011,2692 System and method for controlling trim position of propulsion device on a marine vessel
A method of controlling trim position for a propulsion device on a marine vessel includes receiving a running trim position for the propulsion device, receiving...
US-1,011,2691 Releasable forward section of an underwater vehicle
An example underwater vehicle includes a first section detachably coupled to a second section that is positioned forward of the first section, and a hinge...
US-1,011,2690 Wheel attachment and towing system for a pontoon water bike
A system of brackets and rails for attaching wheels, towing, and accessory devices to a pontoon water bike to increase the transportability and utility of the...
US-1,011,2689 Watercraft positioning system
Modifications to the lifting structure of prior art boat lifts permit the addition of support and drive rollers and associated drive mechanisms that may be used...
US-1,011,2688 Surf wake forming system with dual actuated trim tab
A wakeboat has a hull, the hull forming a wake when moving forward in the water, with a port disturbance and a starboard disturbance in the wake. A trim tab is...
US-1,011,2687 System and method for conversion of floating drilling platform to floating production platform
The present disclosure provides a system and a method for efficiently converting the structure of a drilling floating platform into a structure for a production...
US-1,011,2686 System for the deployment of marine payloads
The present invention involves a system for the release of low relief, self-orienting deployable payloads from a platform such as an underwater vehicle and a...
US-1,011,2685 Buoyant structure
A buoyant structure having a hull, a main deck, an upper cylindrical side section extending downwardly from the main deck, an upper frustoconical side section,...
US-1,011,2684 Self supporting canopy
An inflatable canopy assembly includes an inflatable canopy cover, and a tunnel structural system integrated into the inflatable canopy cover. The tunnel...
US-1,011,2682 Method to sever and disengage a bicycle drivetrain between the crank axis and rear wheel axle, thereby enabling...
Employing a set of open gears in a bicycle drivetrain allows disengaging the connection between the crank arms and the driven wheel. When the fold axis passes...
US-1,011,2681 Bicycle sprocket supporting member and bicycle sprocket assembly
A bicycle sprocket assembly is basically provided with a bicycle sprocket supporting member and at least one sprocket. The bicycle sprocket supporting member...
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