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Patent # Description
2016/0297548 SYSTEM AND METHOD FOR MAGNETICALLY LAUNCHING PROJECTILES OR SPACECRAFT
A system and method for magnetically launching projectiles or spacecraft includes an electromagnetic launcher including a launch tube, and a launch craft. The...
2016/0297547 AUTONOMOUS CRAWLING ASSEMBLY SYSTEM
An automated motorized device may be configured to move on a structure for use in assembling of the structure. The automated motorized device may comprise an...
2016/0297546 Self Transportable Aerostat System
A self transportable aerostat system comprising: a first motorized mooring truck; a mooring tower removable attached to a base assembly of the first mooring...
2016/0297545 MOBILE TERMINAL AND METHOD FOR CONTROLLING THE SAME
A mobile terminal including a wireless communication unit configured to transceive data with a drone via wireless communication; a display unit; a memory...
2016/0297544 ELECTRIC POWER SUPPLY SYSTEM HAVING ACTIVE POWER CONTROL DEVICE
As a component of an aerial vehicle, a power management system having an active power control device is provided. The system includes a solar cell converting...
2016/0297543 VOICE ROUTER
A voice router for a vehicle and a method for operating a voice router are provided. The voice router, for example, may include, but is not limited to, an...
2016/0297542 LIGHTNING DAMAGE RESISTANT AIRCRAFT SKIN FASTENERS
A fastener providing protection against damage to an aircraft resulting from lightning strikes includes an elongated shaft having a head disposed at an upper...
2016/0297541 AIRCRAFT WING SLAT SKEW DETECTION SYSTEMS AND METHODS
An apparatus for detecting skew in a slat of an aircraft wing includes an elongated track moveably supported in the wing for longitudinal movement toward and...
2016/0297540 Aircraft Position Display System
A method for managing navigation of an aircraft. Positions for the aircraft are identified from position information from sensors. Graphical indicators are...
2016/0297539 ADJUSTABLE ENGINE SUSPENSION FOR POSITIONING THE ENGINE RELATIVE TO THE MOUNT THEREOF
The invention relates to a method for mounting an engine module (1) in a support comprising a first structure (3) and a second structure (2) that is offset...
2016/0297538 AIRCRAFT FUEL SYSTEM WITH HEATING OF STORED FUEL
An aircraft fuel system comprises a fuselage tank and wing fuel tanks each connected to the fuselage fuel tank by a respective fuel line. A first fuel line...
2016/0297537 RIGIDIZED ASSISTED OPENING SYSTEM FOR HIGH ALTITUDE PARAFOILS
A parafoil for operation at high altitudes, in low density air, or at low airspeeds, and methods for opening same. Some versions of the parafoil comprise...
2016/0297536 HYBRID SEAT PAN AND DIAPHRAGM
A hybrid seat pan and diaphragm apparatus includes a seat pan that has a concave portion and a diaphragm positioned at an occupant-facing side of the seat pan...
2016/0297535 REVERSIBLE UPHOLSTERY DRESS COVER
A reversible upholstery dress cover article includes a fabric web, an obverse finish layer covering an obverse face of the web, a reverse finish layer covering...
2016/0297534 Convertible seating unit
A convertible seating unit (100, 200) is disclosed as including a first seat (104a, 204a) including a first backrest (106a) and a first seat base (108a), and a...
2016/0297533 AIRCRAFT SEATING ASSEMBLY
Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more...
2016/0297532 DEPLOYABLE DINING TABLE
A deployable table assembly including a table, first and second non-parallel static rails, and first and second hinges attaching the table to the first and...
2016/0297531 ARTICULATING FOOT WELL DIVIDER FOR ADJACENT PARALLEL PASSENGER SEATS
Disclosed is a foot well divider for adjacent parallel passenger seats, having a movable structure adapted to be hinged to a static structure positioned...
2016/0297530 PRIVACY DIVIDER FOR ADJACENT PARALLEL PASSENGER SEATS
A suite divider for a passenger suite seating arrangement including separate first and second panels adapted to be deployed along a top of a partition wall...
2016/0297529 HIGH END BUSINESS CLASS SEATING ARRANGEMENT
Described are seating arrangements having at least one aisle column with at least one high bed seating unit and at least one low bed seating unit, and at least...
2016/0297528 Crown Cabin Configuration for an Aircraft
An aircraft configuration having a crown cabin above a main cabin, with the crown cabin having a hanging floor structure. This enables a fuselage design that...
2016/0297527 CONTROLLING IN FLIGHT ENTERTAINMENT SYSTEM USING POINTING DEVICE INTEGRATED INTO SEAT
An entertainment system includes a video display unit facing a passenger seat and a track pad assembly integrated with an armrest of the passenger seat. The...
2016/0297526 VIDEO DISPLAY UNIT CASSETTE ASSEMBLIES FOR AIRCRAFT SEATS ANDENHANCED IN FLIGHT ENTERTAINMENT USER EXPERIENCE
A video display unit cassette assembly includes a cassette frame, a display coupled to the cassette frame, one or more electronic components between the...
2016/0297525 SYSTEMS AND METHODS FOR POSITIONING A SECTION DIVIDER ASSEMBLY WITHIN A VEHICLE
A section divider system is configured to separate sections within an internal cabin of a vehicle. The section divider system may include a first rail secured...
2016/0297524 PRIVACY DIVIDER WITH VIDEO MONITOR FUNCTION FOR VEHICLE PASSENGER SEATING UNIT
A vehicle passenger seating unit of the type having at least first and second seats facing each other. A privacy divider is provided that includes first and...
2016/0297523 OVERHEAD STOWAGE BIN ASSEMBLY FOR A VEHICLE
A stowage bin assembly is configured to be positioned above at least a portion of one or more seats within a vehicle. The stowage bin assembly may include a...
2016/0297522 DRONE IMMERSION-PILOTING SYSTEM
The system comprises a drone and a ground station with a console adapted to be directed towards the drone, and virtual reality glasses rendering images taken...
2016/0297521 SYSTEMS, METHODS, AND DEVICES FOR UNMANNED AERIAL VEHICLE DISPATCH AND RECOVERY
A service unmanned aerial vehicle (UAV) includes a flight system, a status component, a navigation system, and a recovery component. The flight system is for...
2016/0297520 MODULAR NACELLES TO PROVIDE VERTICAL TAKEOFF AND LANDING (VTOL) CAPABILITIES TO FIXED WING AERIAL VEHICLES, AND...
Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed-wing aerial vehicles, and associated systems and methods are disclosed. A...
2016/0297519 SYSTEM FOR CONTROLLING A ROTOCRAFT ROTOR, A ROTORCRAFT FITTED WITH SUCH A SYSTEM, AND AN ASSOCIATED CONTROL METHOD
A control system for controlling a rotorcraft rotor, to a rotorcraft fitted therewith, and to a corresponding control method. The system comprises selector...
2016/0297518 METHOD FOR STATIC BALANCING OF AIRCRAFT ROTOR BLADES
A method of assembling a rotor blade includes determining first spanwise and chordwise moments of a first component of the blade and comparing the first...
2016/0297517 Flexible Wheel Drive for Aircraft Onboard Taxi Systems
A flexible wheel drive for aircraft onboard taxi systems is provided. In association with an aircraft wheel assembly there is provided a drive gear assembly...
2016/0297516 AXLE SLEEVE
The present disclosure describes an axle sleeve. The axle sleeve may be insertable over a portion of an axle, such as a mid-journal surface between an inner...
2016/0297515 AMORPHOUS METAL RIBLETS
An array of aerodynamic riblets is created by a plurality of high stiffness tips with a layer supporting the tips in predetermined spaced relation and adhering...
2016/0297514 NO-BACK DEVICE FOR FLIGHT CONTROL SURFACE ACTUATOR
Disclosed is an actuator for varying the position of a flight control surface on an aircraft, wherein the actuator comprises a no-back device including a...
2016/0297513 High-Positioned 2-Postion Variable Camber Krueger
A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a...
2016/0297512 Bonded and Tailorable Composite Assembly
An all-composite assembly such as a composite laminate aircraft empennage has vertical and horizontal stabilizers with differing sets of interlaminar fracture...
2016/0297511 RIB STRUCTURE AND METHOD OF FORMING THEREOF
A rib structure for use in an aircraft is provided. The rib structure includes a web portion, a plurality of hat stiffener portions coupled to the web portion,...
2016/0297510 AIRCRAFT REAR STRUCTURE
An aircraft rear structure comprising a substantially flat rear pressure bulkhead, with a first side and a second side, opposite to the first side. The...
2016/0297509 SANDWICH PANEL FOR AN AIRCRAFT
A sandwich panel for an aircraft includes a lower top layer, an upper top layer and a core layer, wherein the core layer in turn includes pins. The pins extend...
2016/0297508 METHOD FOR MANAGING THE SPEED OF A VESSEL
A method for managing the speed of at least one first vessel in a seismic survey. The first vessel sails at a current speed and performing a series of shots...
2016/0297507 JET PROPULSION WATERCRAFT
A jet propulsion watercraft includes a vessel body, a steering nozzle, and a bucket. The steering nozzle includes a jet port from which a jet of water is...
2016/0297506 System and Method for Subsea Propulsion and Energy Harvesting Using Current Shear
A subsea system for exploiting an oceanic current shear includes a first vehicle positionable in a first oceanic current and tethered to a second vehicle...
2016/0297505 DIVING MASK HAVING A BUILT-IN SNORKEL
The invention concerns a diving mask (10) comprising a faceplate (18) secured to a frame (12), a flexible skirt having a partition delimiting an upper viewing...
2016/0297504 FLEXIBLE JOINT
A constant volume flexible joint system includes a flexible membrane for coupling across a joint and spaced radial support ribs fitted to the membrane. Axial...
2016/0297503 MOUNTING SYSTEM AND ASSOCIATED APPARATUS
A mounting system is provided. Such a system includes at least one "C" channel adapted to be mounted to a surface, and a mountable accessory device. An...
2016/0297502 Device for Launching a Subsurface Mining Vehicle Into a Water Mass and Recovering the Same from the Water Mass
A device for launching subsurface mining vehicle into a water mass from a docking well of a floating vessel, and/or recovering said vehicle from the water mass...
2016/0297501 BICYCLE CONTROL DEVICE FOR OPERATING A BICYCLE COMPONENT
A bicycle control device is provided for operating a bicycle component. The bicycle control device includes a base member, an operating member, a take-up...
2016/0297500 Electric Drive Unit
A lightweight, compact electric drive unit provides high reduction ratios for a bicycle, light electric vehicle or autonomous device. A cycloid gear reducer...
2016/0297499 ELECTRIC VEHICLE
An electric vehicle includes a vehicle body, an electric motor, a wheel, an operator operated by a user to drive the wheel to rotate by power from the electric...
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