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Patent # Description
2016/0176543 HELICOPTER LANDING PAD
A mobile helicopter landing pad comprises a platform with one or more elongate, concave guiding channels for aligning a helicopter on the landing pad by...
2016/0176542 IMAGE CAPTURE SYSTEMS AND METHODS AND ASSOCIATED MOBILE APPARATUSES
Described herein is a mobile apparatus for capturing images that includes a body, a propulsion device coupled to the body and actuatable to propel the body in...
2016/0176541 Aircraft Flight Control
The invention described herein provides a flight crew with an easier and more intuitive way to control and monitor flight-control surfaces. Specifically, the...
2016/0176540 METHOD FOR TESTING A COMPONENT IN A HIGH LIFT SYSTEM OF AN AIRCRAFT
A method for testing a component in a high lift system of an aircraft comprises the steps of activating a brake coupled with at least one hydraulic motor,...
2016/0176539 METHOD FOR DETERMINING A STATE OF A COMPONENT IN A HIGH LIFT SYSTEM OF AN AIRCRAFT
A method for determining a state of a component in a high lift system of an aircraft comprises the steps of extending at least one high lift surface, which is...
2016/0176538 SMART AVIONICS SYSTEM
An aircraft communication network comprises: avionics monitoring software in communication with aircraft avionics, the aircraft avionics including a flight...
2016/0176537 COMPONENT RACK CONSTRUCTION FOR USE IN AIRCRAFT
A component rack for use in an aircraft can include a stanchion having sides angularly offset relative to each other, with the sides widening at each opposite...
2016/0176536 FOOLPROOFING SYSTEM FOR PIPES BY MEANS OF AN OBSTACLE INSIDE A CONNECTOR IN AN AIRCRAFT DUCT
In an aircraft duct formed with pipes connected in pairs via connectors in which the pipes are mounted with the possibility of axial displacement, there exists...
2016/0176535 AIRCRAFT FUEL TANK INERTING ARRANGEMENT, METHOD OF INERTING ONE OR MORE AIRCRAFT FUEL TANKS, AIRCRAFT AND...
A method is provided of inerting one or more fuel tanks of an aircraft. The method comprises: providing a temperature value indicative of a temperature at the...
2016/0176534 EMERGENCY POWER SOURCES FOR PROPULSION SYSTEMS
A hybrid-electric propulsion system includes a motor drive and a rechargeable energy storage system electrically connected to the motor drive. The...
2016/0176533 REMOVABLE AUXILIARY POWER DEVICE FOR AIRCRAFT AND AIRCRAFT ADAPTED TO USE AT LEAST ONE SUCH DEVICE
An auxiliary power device may be exteriorly removably connected to an aircraft in order to allow the increase of the performance data of the aircraft, namely...
2016/0176532 PROPELLER FOR AN AIRCRAFT TURBOMACHINE, INCLUDING A BLADE RETAINING STRUCTURE THROUGH WHICH THE AERODYNAMIC...
A propeller for a turbomachine intended to be driven in rotation about a propeller rotation axis and including variable pitch blades. The propeller further...
2016/0176531 CARRIER SYSTEM FOR CARRYING OUT INTERCEPTION MANEUVERS OF A LOADBEARING PARAGLIDER AND METHOD FOR ADJUSTING THE...
A carrier system for carrying out interception maneuvers of a loadbearing paraglider which has a glider having a trailing edge for carrying out the maneuver...
2016/0176530 ACTIVE FROST FORECASTING, DETECTION AND WARNING SYSTEM AND METHOD
An active frost warning system for the forecasting and/or detection of active frost conditions by determining the surface or skin temperature of an active...
2016/0176529 AIRCRAFT AND AIRBORNE ELECTRICAL POWER AND THERMAL MANAGEMENT SYSTEM
One embodiment of the present disclosure is a unique airborne electrical power and thermal management system. Another embodiment is a unique aircraft. Other...
2016/0176528 Automatic Activation of a Fog Protection System Onboard a Vehicle
A method is provided that includes a number of operations performed in real-time during operation of a vehicle. That is, the method may include detecting fog...
2016/0176527 VEHICLE SEAT TUBING HAVING VARIABLE WALL THICKNESS
Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the...
2016/0176526 SELF SUFFICIENT GALLEY SYSTEM, METHOD FOR OPERATING ELECTRICAL GALLEY DEVICES, AND AIRCRAFT HAVING SUCH A...
A galley system comprising at least one electrically operated galley device, a galley frame having at least one compartment for housing the at least one galley...
2016/0176525 LAVATORY ARRANGEMENT FOR A VEHICLE CABIN AND VEHICLE HAVING A VEHICLE BODY, AND A CABIN HAVING A LAVATORY...
A lavatory arrangement for a vehicle cabin comprises a lavatory housing defining an inner space having an entrance opening, a floor and a first lateral...
2016/0176524 AERIAL DELIVERY SYSTEM WITH MUNITION ADAPTER AND LATCHING RELEASE
An aerial delivery system is configured to allow delivery of one or more releasable items after the system is extracted from an aircraft. One or more linear...
2016/0176523 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...
2016/0176522 METHOD AND A SYSTEM FOR DETERMINING AN ANGULAR VELOCITY IN TURNING FOR A ROTARY WING AIRCRAFT
A method and a system for determining an angular velocity in turning for a rotary wing aircraft in order to make turns that are coordinated relative to the...
2016/0176521 FLEXBEAM ROTOR ATTACHMENT TO ROTOR BLADE
A rotor blade assembly includes a flex-beam member and a torque tube surrounding the flex-beam member and extending partially along a rotor blade assembly...
2016/0176520 SELF-ENCLOSED AIR VEHICLE
Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight...
2016/0176519 FLOW RESTRICTION SYSTEM FOR REGULATING DYNAMIC PRESSURE LOSS
A vibration control system includes an outer housing, an inner housing carried within the outer housing, a fluid passage extending through the inner housing...
2016/0176518 BRAKE ACTUATOR FOR AIRCRAFT WHEEL HYDRAULIC BRAKE
The invention relates to a brake actuator for an aircraft hydraulic brake, which is intended to be added into one of the cavities of a brake ring, the actuator...
2016/0176517 COCKPIT CONTROL SYSTEM FOR CONTROLLING GROUND TRAVEL IN AIRCRAFT EQUIPPED WITH ENGINE-FREE ELECTRIC TAXI SYSTEM
A cockpit control system and method for efficiently controlling ground travel in an aircraft equipped with an engine-free electric taxi system are provided....
2016/0176516 AIRCRAFT LANDING GEAR
An aircraft landing gear including an axle and a wheel (5) that includes a rim (6) mounted to turn on the axle about a first rotation axis (X1), the landing...
2016/0176515 LANDING GEAR METHOD AND APPARATUS FOR BRAKING AND MANEUVERING
Aircraft landing gear comprised of a wheel hub motor/generator includes alternating rotors and stators mounted with respect to the wheel support and wheel. The...
2016/0176514 ROTARY WING DRONE
The drone comprises a body and a plurality of propulsion units, each provided with a propeller driven by a respective motor, the different motors being able to...
2016/0176513 AIRCRAFT NOSE PROVIDED WITH A CONNECTING FRAME BETWEEN THE LANDING GEAR HOUSING AND THE OUTER SKIN OF THE FUSELAGE
In order to assist fitting of doors to the landing gear housing and adjusting their position, an aircraft nose is provided comprising a connecting frame...
2016/0176512 MULTI CORE VEHICLE MANAGEMENT SYSTEM AND METHODS
A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS...
2016/0176511 ADJUSTABLE HEIGHT CYCLIC CONTROL ASSEMBLY AND METHOD
Adjustable height control stick assembly for dual control of aircraft includes a single control stick for longitudinal and lateral orientation of the aircraft...
2016/0176510 METHOD OF MANAGING DISCONTINUITIES IN VEHICLE CONTROL FOLLOWING A CONTROL TRANSITION, AND A VEHICLE
A method during which a current position of a pilot control is determined, an equivalent position is determined that the pilot control needs to reach following...
2016/0176509 Propeller blade for an aircraft engine
The disclosure refers to a propeller blade for an aircraft engine that includes an airbag system contained inside the blade and comprising at least one bag and...
2016/0176508 Cove Lip Door Slaved to Trailing Edge Control Device
Movement of an aerodynamic cove lip door is directly slaved to real time movement of a trailing edge control device operably secured to an aircraft wing. The...
2016/0176507 Trailing Edge Device with Bell Crank Mechanism
A bell crank mechanism is configured to at least indirectly link any movement of an aircraft wing spoiler-like hinge panel to the movement of an aircraft wing...
2016/0176506 LIFTING SURFACES AND ASSOCIATED METHOD
An arrangement of lifting surfaces including a primary lifting surface having a flexural axis extending in the spanwise direction of the lifting surface, a...
2016/0176505 TAILPLANE WITH POSITIVE CAMBER
Tailplanes and empennages for aircraft are disclosed. An exemplary tailplane disclosed includes a stabilizer having a fixed shape and an elevator movably...
2016/0176504 Wing Fold Controller
Illustrative embodiments may provide for an apparatus and method of controlling the folding of a wing. The apparatus may include a sensor, an actuator, and a...
2016/0176503 Mechanisms for Deploying and Actuating Airfoil-Shaped Bodies on Unmanned Aerial Vehicles
Deployment and control actuation mechanisms are incorporated in unmanned aerial vehicles having folding wings and/or folding canards and/or a folding vertical...
2016/0176502 Morphing Foil or Wing
Embodiments of the present invention relate to an adaptable wing having a variable geometry for influencing aerodynamic performance, the wing comprising a...
2016/0176501 DEVICE FOR PROTECTING THE FRONT SPAR STRUCTURE OF A CENTRAL CASING OF AN AIRCRAFT WING AND AT LEAST ONE PIECE...
A device for protecting a front spar structure of a central casing of an aircraft wing and at least one item of equipment situated in the wing, comprising: a...
2016/0176500 Stiffened composite panels
A stiffened panel comprises a composite panel, and a stiffener including a base flange on the composite panel. The base flange is tapered towards the panel....
2016/0176499 AIRCRAFT WING TORSION BOX, AIRCRAFT WING, AIRCRAFT AND SUPPORTING MEMBER FOR USE THEREIN
An aircraft wing torsion box having a front associated with a leading portion of the wing torsion box and a rear associated with a trailing portion of the wing...
2016/0176498 Method and System for Insulating Frame Member
An insulation system, for use with transport vehicle structural frame members, having at least a first structural frame member and adjacent structural frame...
2016/0176497 IMPROVED FUEL TANK ACCESS DOOR GASKET WITH REINFORCED SEAL
An annular elastomeric EMI shielding gasket includes a metallic mesh embedded in an elastomeric sheet for sealing and protecting aircraft fuel tanks and...
2016/0176496 DOOR FOR CLOSING OPENING IN STRUCTURE AND AIRCRAFT
The present invention relates to a door for closing an opening in a structure, including: a body arranged to be capable of abutting against a first side of the...
2016/0176495 Compacting Uncured Composite Members on Contoured Mandrel Surfaces
An uncured composite member is formed over a mandrel having a contour using a flexible compactor. Forming is performed outwardly from the apex of the contour.
2016/0176494 SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE
An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting dome shaped vehicle body has an apex/protrusion...
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