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Patent # Description
2016/0200457 SMALL SATELLITE PROPULSION SYSTEM
A small satellite propulsion system using a gaseous oxidizer and a gaseous fuel as primary propellants with a liquid as a film coolant for the inner surface of...
2016/0200456 ASSEMBLY FOR AIMING AN INSTRUMENT
An aiming assembly comprising an instrument and aiming device, the aiming device comprises: a frame, a mobile part comprising a plate, the instrument being...
2016/0200455 LINE REPLACEMENT UNIT (LRU) REPLACEMENT PROCESS
An improved integrated avionics system having a plurality of line replacement units (LRUs) is disclosed. At least one LRU stores in its memory software and...
2016/0200454 DUAL FUNCTION MOVEMENT COMPONENT FOR AUTOMATED ASSEMBLY SYSTEMS
A pneumatic device may be configured and used to provide multiple movement related functions, such as in an automated assembly system. The pneumatic device may...
2016/0200453 AIRCRAFT LANDING GEAR ASSEMBLY STOP MEMBER
An aircraft landing gear assembly stop member is arranged to be coupled to a first part of an aircraft landing gear assembly and includes a pair of projections...
2016/0200452 WIRELESS ROTATING INSTRUMENTATION SYSTEM AND METHODS FOR DATA COLLECTION ON HELICOPTER ROTOR SYSTEMS
The application relates to a wireless rotating instrumentation package for collecting data from a spinning rotor head of a rotary wing aircraft. The...
2016/0200451 DISPLAY SYSTEMS AND METHODS FOR GENERATING A DISPLAY PROVIDING RUNWAY ILLUSION ALLEVIATION
Display systems and methods for generating a display providing runway illusion alleviation are disclosed herein. An exemplary method for generating a display...
2016/0200450 DIRECT POSITION MEASUREMENT FOR AIRCRAFT FLIGHT CONTROL SURFACES
A method and apparatus for determining a discrete position of a first surface of an aircraft is disclosed. The first surface and a second surface movable...
2016/0200449 SYSTEM AND METHOD FOR DAMAGE TRACKING AND MONITORING DURING GROUND HANDLING OF AIRCRAFT
A system for damage tracking and monitoring during ground handling of aircraft includes a ground service communication network configured to transmit...
2016/0200448 METHODS AND DEVICES FOR ASSISTING THE PILOTING OF AN AIRCRAFT DURING AT LEAST ONE FLIGHT PHASE HAVING A...
A method and device for aiding piloting of an aircraft, during at least one flight phase including piloting steps. The device includes a unit for real-time...
2016/0200447 Fuel Cell System for an Aircraft and Method for Providing an Inert Gas in an Aircraft
A fuel cell system for an aircraft includes at least one fuel cell having a first inlet for providing a fuel, a second inlet for providing an oxidant, an...
2016/0200446 ON-BOARD AIRCRAFT NITROGEN ENRICHED AIR AND COOLING FLUID GENERATION SYSTEM AND METHOD
An on-board aircraft nitrogen enriched air and cooling fluid generation system and method are disclosed. In one embodiment, the system includes a first heat...
2016/0200445 AIRCRAFT SAFETY DEVICE SYSTEMS
An aircraft system comprising a deflector assembly including, a base having mounting apertures; an inner ring concentrically positioned within an outer ring,...
2016/0200444 ROTORCRAFT HAVING ELECTRICAL EQUIPMENT FOR REGULATING ELECTRICAL POWER SUPPLY TO AN ENGINE ON STARTING
A rotorcraft having at least one turboshaft engine with an electric starter powered from the onboard network that makes use of a battery and of a discharge...
2016/0200443 ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT
The invention relates to a bypass turbojet comprising an exhaust housing having a central hub (13) and connecting means (11) that can transmit the forces...
2016/0200442 ANTI-ICING SYSTEMS
A bleed air pressure regulation system for an aircraft anti-icing system comprises a first, upstream pressure regulating valve and a second, downstream...
2016/0200441 COOLING SYSTEM HAVING A WATER SEPARATOR, AND METHOD FOR OPERATING A COOLING SYSTEM
A cooling system with a heat exchanger, which is designed or configured for through-flow of a coolant and a fluid to be cooled, a fluid line, which is designed...
2016/0200440 CONVEYING DEVICE AND AIRCRAFT SYSTEM WITH A CONVEYING DEVICE OF SUCH A TYPE
A conveying device for conveying a fluid stream comprising a mechanical unit, including a movable conveying element, and an electrical unit comprising a...
2016/0200439 AIRCRAFT AND METHOD OF SERVING PASSENGERS
The invention relates to an aircraft (1) having a passenger cabin (8) and a plurality of passenger seats (11) arranged in this passenger cabin (8), in which...
2016/0200438 PACKAGE DELIVERY BY MEANS OF AN AUTOMATED MULTI-COPTER UAS/UAV DISPATCHED FROM A CONVENTIONAL DELIVERY VEHICLE
Methods and associated systems for autonomous package delivery utilize a UAS/UAV, an infrared positioning senor, and a docking station integrated with a...
2016/0200437 Tethered Flight Control System for Small Unmanned Aircraft
A tethered flight control system for a small unmanned aircraft. The tethered flight control system can have a mobile base, a tether arm, a tether spout, and a...
2016/0200436 Tri-Rotor Aircraft Capable of Vertical Takeoff and Landing and Transitioning to Forward Flight
Systems, methods, and devices provide a vehicle, such as an aircraft, with rotors configured to function as a tri-copter for vertical takeoff and landing...
2016/0200435 SWASHPLATE APPARATUS
A swashplate apparatus is provided and includes a first swashplate including outer and inner bodies and an intermediate portion defining a major groove between...
2016/0200434 ROTOR HEAD FOR A VERTICAL TAKEOFF AND LANDING AIRCRAFT
An apparatus is provided for a vertical take-off and landing aircraft. The apparatus includes a rotor head with a rotor hub and a plurality of rotor blade...
2016/0200433 ROTORCRAFT ROTOR COMPRISING A HUB MADE OF COMPOSITE MATERIALS OBTAINED FROM CARBON FIBER FABRIC DUSTED IN A...
A rotorcraft rotor comprising a hub made up of a monolithic body of composite material obtained by stacking successive layers of carbon fiber fabric dusted...
2016/0200432 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...
2016/0200431 COMPOSITE STIFFENED RIGID PROPELLER SHAPED MAIN ROTOR HUB
A rotor includes a blade retention cuff configured to receive a rotor blade; a yoke coupled to the blade retention cuff; and a rigid propeller shaped hub...
2016/0200430 Tail Rotor Actuation System
In some embodiments, an actuation system includes a an actuator assembly, a yoke, and a control rod. The actuator assembly comprises a first actuator. The...
2016/0200429 DAMPING DEVICE FOR A SUPERCRITICAL TRANSMISSION SHAFT
A damping device for a shaft in rotation around an axis of rotation parallel to a direction (A). The said damping device includes a support, a plate, a collar,...
2016/0200428 AIRCRAFT AUTONOMOUS PUSHBACK
The invention provides methods and systems for controlling speed of an aircraft during an autonomous pushback manoeuvre, i.e. under the aircraft's own power...
2016/0200427 BI-STABLE CLUTCH WITH PERMANENT MAGNET ARRAY
A park brake actuator ("PBA") may comprise a shaft having a friction hub disposed about the shaft, the friction hub fixed against rotation with respect to the...
2016/0200426 LANDING GEAR DRIVE SYSTEM FLEXIBLE INTERFACE
Known autonomous taxi systems for aircraft include a rigid connection between the aircraft wheel and a gear which is used to drive it. Such arrangements have...
2016/0200425 Torque Transmission in an Aircraft Drive Wheel Drive System
A torque transmission system is provided for an aircraft drive wheel drive system mounted on nose or main landing gear wheels to move the aircraft autonomously...
2016/0200424 TIRE SPINNING ASSEMBLY
A tire spinning assembly for includes a tire that may be coupled to landing gear of an aircraft. A plurality of vanes is coupled to the tire. The vanes are...
2016/0200423 NOSE LANDING GEAR ARRANGEMENTS INCLUDING A FLEXIBLE SHEET AND METHODS FOR MAKING THE SAME
Nose landing gear arrangements for aircrafts, aircrafts including such nose landing gear arrangements, and methods for making such nose landing gear...
2016/0200422 Multiple Controllable Airflow Modification Devices
An active wing extension includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is...
2016/0200421 CLEAN FUEL ELECTRIC MULTIROTOR AIRCRAFT FOR PERSONAL AIR TRANSPORTATION AND MANNED OR UNMANNED OPERATION
Methods and systems for a full-scale vertical takeoff and landing manned or unmanned aircraft, having an all-electric, low-emission or zero-emission lift and...
2016/0200420 SYSTEM AND METHOD FOR UNWANTED FORCE REJECTION AND VEHICLE STABILITY
An aircraft comprising a fuselage and a plurality of wings. The fuselage may be positioned between a first wing and a second wing, wherein said first wing and...
2016/0200419 METHODS AND APPARATUS TO CONTROL AIRCRAFT HORIZONTAL STABILIZERS
Methods and apparatus to control aircraft horizontal stabilizers are described herein. One described method includes calculating, using a processor, a desired...
2016/0200418 SELF-TIGHTENING ROTOR
Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object...
2016/0200417 FLOOR ARRANGEMENT WITH CURVED FLOOR PANELS FOR AN AIRCRAFT
A floor arrangement for a passenger cabin of an aircraft or spacecraft includes mounting rails for mounting cabin outfitting components, wherein each mounting...
2016/0200416 ARRANGEMENT FOR MOVING A DOOR IN SWINGING AND SLIDING MOTIONS
The present invention aims at providing an arrangement for moving a door in both a swinging and a sliding manner, in which a pivoting means allows the rotation...
2016/0200415 MULTI-ROTOR SAFETY SHIELD
The Multi-Rotor Safety Shield (MRSS) provides a complete and substantial encasement system which can be secured about a Drone, protecting a multitude of...
2016/0200414 SYSTEM FOR AUTOMATICALLY MODIFYING THE LEAN OF A CATAMARAN DURING A TURN
A system for automatically modifying the lean of a catamaran during a turn includes a pair of fins, each substantially permanently affixed to the inside edge...
2016/0200413 LUBRICATION FOR MARINE DRIVE SYSTEMS
An oil return circuit for a marine drive system, is provided. The oil return circuit includes an oil collection chamber, a first drive shaft with a first...
2016/0200412 Ergonomic Water Paddle for Watercraft
An ergonomic water paddle for a watercraft includes left-hand and right-hand arms, a cross piece, and left and right paddle bodies. The left-hand arm extends...
2016/0200411 PADDLE FOR WATERCRAFT OR FLOTATION DEVICE
A paddle for a waterdraft or flotation device has a pair of shaft mounted blades connected by a core member. A right hand drive grip and a left hand drive grip...
2016/0200410 WATERCRAFT WITH STERNDRIVE AND HULL WITH VENTED TUNNEL
A watercraft includes a sterndrive comprising an inboard engine and an outdrive that extends through the transom. The aft end of the hull includes a stepped...
2016/0200409 APPARATUS AND METHOD FOR NEUTRALIZING UNDERWATER MINES
A mine neutralizing device that includes a buoy. The buoy includes a mine neutralizing device capable of swimming to an undersea mine to neutralize it. A...
2016/0200408 CHARGE DEPLOYMENT SYSTEM FOR ORDNANCE NEUTRALISATION
A charge deployment system for ordnance neutralisation. The system is suited to deploying multiple disposal charges to neutralise multiple items of ordnance,...
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