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Patent # Description
2017/0313452 BOTTLE CARRIER AND CASE PACKAGING MACHINE
A device, system, and method for loading empty and formed six-pack bottle carriers into a larger case (i.e. a multi-pack) is provided. The packaging device...
2017/0313451 METHOD AND APPARATUS FOR FILLING BOXES
A device, system, and method for loading empty and formed six-pack bottle carriers into a larger case (i.e. a multi-pack) is provided. The packaging device...
2017/0313450 PACK FILLING MACHINE WITH OFFSET PATHS
A device, system, and method for loading empty and formed six-pack bottle carriers into a larger case (i.e. a multi-pack) is provided. The packaging device...
2017/0313449 Apparatus and Method for Manufacturing a Smoking Article Pack
A method of manufacturing a pack of smoking articles. The method comprises providing a planar blank of an inner support frame comprising a front panel and a...
2017/0313448 Method for Applying an Underlayment Layer to Trucking Cargo
A method for applying an underlayment layer to trucking cargo includes providing a roll of underlayment layer that is independent of the trucking cargo and a...
2017/0313447 SPACE DEBRIS INTERCEPTION
A vehicle for intercepting a target object orbiting in space is provided, comprising a launching portion for driving the vehicle into an orbit, and an...
2017/0313446 Craft Using an Inertial Mass Reduction Device
A craft using an inertial mass reduction device comprises of an inner resonant cavity wall, an outer resonant cavity, and microwave emitters. The electrically...
2017/0313445 SMALL SCALE REACTION WHEEL ASSEMBLIES
Reaction wheel assemblies having relatively compact and lightweight form factors (referred to as "small scale" RWAs) are disclosed. Such small scale RWAs are...
2017/0313444 SELF-CONSUMING SATELLITE
A CubeSat satellite has a solar cell and an arc propulsion system. The arc propulsion system includes a power source, a first lead coupled to the power source...
2017/0313443 SPACE SHUTTLE ORBITER AND RETURN SYSTEM
A launch system comprises a nose section comprising a nose coupling surface, a tail section comprising a tail coupling surface facing the nose coupling surface...
2017/0313442 AERIAL VEHICLE LAUNCHER
An aerial vehicle launcher including a rail having a first end and a longitudinal axis and a piston movable in a passageway formed in the rail, the piston...
2017/0313441 UNMANNED AERIAL VEHICLE
An unmanned aerial vehicle includes a housing, at least one driving module, and at least one driving module. The housing includes an outer structure made of...
2017/0313440 METHODS AND APPARATUS FOR REDUCING ANXIETY DURING TRAVEL
In some embodiments, a system is provided that includes a portable electronic device; and an application executable on the portable electronic device, the...
2017/0313439 METHODS AND SYSTSTEMS FOR OBSTRUCTION DETECTION DURING AUTONOMOUS UNMANNED AERIAL VEHICLE LANDINGS
Systems and methods for obstruction detection during autonomous unmanned aerial vehicle landings, including unmanned aerial vehicles equipped with at least one...
2017/0313438 Charge Control System to Reduce Risk of an Aircraft-Initiated Lightning Strike
System for reducing likelihood of an aircraft-induced lightning strike on an aircraft. The system includes a plurality of electric field sensors distributed on...
2017/0313437 MAGNETIC CARBON NANOTUBE CLUSTER SYSTEMS AND METHODS
Techniques are disclosed for systems and methods to provide magnetic carbon nanotube clusters configured to form electrically conductive coatings. A magnetic...
2017/0313436 METHOD OF MONITORING A COMPOSITE MATERIAL
The method allows to monitor a composite material comprising an epoxy resin tilled with electrically conductive nanoparticles, wherein at least one electrical...
2017/0313435 FUEL TANK INERTING SYSTEMS FOR AIRCRAFT
Aircraft air separation systems having a compressed air source arranged to supply compressed air, an air separation module arranged to receive air from the...
2017/0313434 Rotorcraft Fuel System having Enhanced Crash Resistance
A rotorcraft includes a fuselage having a fuel tank receiving assembly with a fuel tank positioned therein. The fuel tank including a plurality of...
2017/0313433 HELICOPTER
A multicopter (100) having a plurality of propellers (1) is configured to be electrically operated. The multicopter (100) is provided with electric motors (2),...
2017/0313432 SYSTEM FOR INSTALLING AND REMOVING A PROPULSION UNIT ON A PYLON OF AN AIRCRAFT
The present disclosure concerns a system for installing and removing a propulsion unit on a pylon of an aircraft, a propulsion unit of the type including a...
2017/0313431 AIRCRAFT PROPULSION ASSEMBLY WITH A FILTERED CRADLE
The invention provides an aircraft propulsion assembly comprising a gas generator coupled by a coupling mechanism to a thrust generator having a structural...
2017/0313430 AIRCRAFT ENGINE ASSEMBLY COMPRISING A PYLON LEADING EDGE INCORPORATED WITH AN ANNULAR ROW OF UNFAIRED...
To reduce the overall mass of an engine assembly for aircraft, this assembly comprises a part of the fuselage of an aircraft, a turbomachine comprising an...
2017/0313429 METHOD AND APPARATUS OF DETECTING LIQUID WATER IN A CLOUD
Apparatus and associated methods relate to determining liquid-water concentration in a cloud atmosphere based on a frequency of resonance of a magnetostrictive...
2017/0313428 SYSTEMS AND METHODS FOR PREVENTING ICE FORMATION ON PORTIONS OF AN AIRCRAFT
An ice prevention system is configured to prevent ice from forming and/or melt ice with respect to one or more portions of an aircraft. The ice prevention...
2017/0313427 LOCK MECHANISM FOR AIRCRAFT PASSENGER SEAT
In order to improve ease of maintenance of an aircraft passenger seat, the aircraft passenger seat 100 is adapted to be changeable between an upright position...
2017/0313426 IN-VEHICLE POSITION DETECTION AND CONFIGURATION OF VEHICLE COMPONENTS
There is described herein a method and system for the configuration of vehicle management components using in-vehicle position detection. The in-vehicle...
2017/0313425 Avionics system for assisting implementation of security measures onboard an aircraft, aircraft comprising such...
Avionics system for assisting implementation of security measures onboard an aircraft, aircraft comprising such a system, and associated method are provided....
2017/0313423 SYSTEM FOR MOVING LOADS COMPRISING A DRIVEN TRANSPORT VEHICLE
A system for moving loads comprising a cargo compartment floor, at least one roller track comprising rollers arranged one behind the other in the cargo...
2017/0313422 UNMANNED AERIAL VEHICLE PICK-UP AND DELIVERY SYSTEMS
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV...
2017/0313421 UNMANNED AERIAL VEHICLE INCLUDING A REMOVABLE PARCEL CARRIER
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV...
2017/0313420 AUTONOMOUS SPRAY SHIP AND METHOD
An airship and method of providing thrust to an airship are shown. Examples include a number of turbine thrusters coupled to a number of electric...
2017/0313419 POWER MANAGEMENT METHOD AND SYSTEM FOR AN UNMANNED AIR VEHICLE
Power management method and system for an unmanned air vehicle, wherein the unmanned air vehicle comprises a plurality of power demanding subsystems and a...
2017/0313418 UNMANNED VEHICLE
An unmanned vehicle is provided. The unmanned vehicle includes: a base; a driving unit including an actuator and a propeller rotating by using power of the...
2017/0313417 UNMANNED AERIAL VEHICLE
An embodiment of the present disclosure provides an unmanned aerial vehicle, An unmanned aerial vehicle, with a double-layered structure formed by stacking a...
2017/0313416 Imaging Using Multiple Unmanned Aerial Vehicles
An aerial imaging system and method of aerially capturing an image including a first unmanned aerial vehicle (UAV) and a second UAV. The first UAV includes a...
2017/0313415 KITE WITH RIGID SPAR ARRANGEMENT
A kite for use in a system for extracting energy from the wind comprises: a wing (1) having a roll neutral point or zone when the kite is in flight; a tether...
2017/0313414 ROD END
A rod end of an actuator assembly is disclosed. The rod end may comprise a rod piston end having an outer profile, and a rod joint end opposite the rod piston...
2017/0313413 Shock Wave Modification Method and System
A system for modifying a shock wave formed in a fluid by a body to modify effects of the shock wave on information transferred to or from the body. The system...
2017/0313412 DEVICE FOR REDUCING AERODYNAMIC DISTURBANCES IN THE WAKE OF AN AERODYNAMIC PROFILE BY VARIABLE-DISTRIBUTION...
A device for reducing aerodynamic disturbances in the wake of an aerodynamic profile. The device comprises a first air ejection nozzle arranged on the top side...
2017/0313411 SYNCHRONIZATION OF FLUIDIC ACTUATORS
A fluidic system is disclosed. The system comprises a plurality of fluidic oscillatory actuators, and at least one synchronization conduit connecting two or...
2017/0313410 AERIAL VEHICLE WITH UNCOUPLED HEADING AND ORIENTATION
An aerial vehicle includes a hull containing the main processor, energy storage, support components such as sensors, wireless communication, and landing gear....
2017/0313409 AIRCRAFT ACTUATOR WITH NO-BACK, LOAD DETENT ASSEMBLY
A load detent assembly for restricting creep of a rotating assembly of an actuator used to actuate an aircraft flight control surface. The load detent assembly...
2017/0313408 AUTOPILOT SYSTEM, AND RELATED COMPONENTS AND METHODS
A device for releasably mounting an autopilot control circuit to a flight control component of an aircraft, includes a frame that holds a component of an...
2017/0313407 ALIGNMENT DEVICE FOR A SELECTOR LEVER
A selector lever includes a detent pin that travels along a shaft for being positioned within a detent slot of a detent plate for securing the selector lever...
2017/0313406 HYDRAULIC ACTUATION SYSTEMS
An hydraulic actuation control module is provided for installation in a pitch change actuator of a propeller assembly. The module comprises a flow metering...
2017/0313405 BLADE PITCH CONTROL
A blade pitch adjustment system comprising a yoke arranged to be moved in a first direction in response to an actuator; a plurality of trunnion pins arranged...
2017/0313404 PROPELLER FOR AN AIRCRAFT TURBO ENGINE, INCLUDING SAFETY MEANS FOR CONTROLLING BLADE ANGLE OF ATTACK
In order to simplify the design of an aircraft turbo engine propeller while enhancing the safety function thereof related to control of the blade angle of...
2017/0313403 PROPELLER RING COMPRISING RADIAL HOUSINGS WITH AN OVOID CROSS-SECTION
The invention relates to a propeller ring (10) of a turbomachine (1), with variable-pitch blades (P), the propeller ring (10) comprising a substantially...
2017/0313402 QUICK CONNECTION ASSEMBLIES ESPECIALLY USEFUL FOR COUPLING AIRCRAFT ANTENNA FAIRINGS TO AIRFRAME STRUCTURES
Aircraft antenna fairing assemblies include a fairing shell and connection components for positionally fixing the fairing shell to airframe structure of an...
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