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Patent # Description
2018/0273206 METHOD AND APPARATUS FOR FABRICATION OF LATTICE COMPOSITE FUSELAGE FOR COMMERCIAL AIRCRAFT EMPLOYING STEERED...
A system for fabrication of an aerospace structure incorporates a mold having a surface and at least one unidirectional SFL head adapted to lay down a...
2018/0273205 Precision approach path indicator with a novel reflector arrangement
A compact PAPI having a semiconductor light source and finely distribution of lights is herein proposed. The novel PAPI includes two artificial light sources...
2018/0273204 SYSTEMS AND METHODS FOR RECOVERING AND CONTROLLING POST-RECOVERY MOTION OF UNMANNED AIRCRAFT
Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for...
2018/0273203 UNMANNED AERIAL VEHICLE, IMAGE PHOTOGRAPHING APPARATUS AND GIMBAL THEREOF
The present application relates to a gimbal configured to mount a photographing device. The gimbal includes a main body, a mounting shaft connected to the main...
2018/0273202 FLIGHT INDICATION APPARATUSES, SYSTEMS AND ASSOCIATED METHODS
Systems, apparatuses and methods for indicating a moveable device such as an unmanned aerial vehicle (UAV) are disclosed herein. The present technology...
2018/0273201 CONTROL DEVICE, CONTROL METHOD, AND FLIGHT VEHICLE DEVICE
[Object] To provide a control device which enables a flight vehicle device to obtain a highly precise image. [Solution] Provided is the control device including an...
2018/0273200 AVIONIC DISPLAY SYSTEMS AND METHODS FOR GENERATING VERTICAL SITUATION DISPLAYS INCLUDING INSTABILITY PREDICTION...
Avionic display systems and methods are provided for generating avionic displays including instability prediction and avoidance symbology, such as...
2018/0273199 AERODYNAMIC CONTROL SURFACE MOVEMENT MONITORING SYSTEM FOR AIRCRAFT
Actuator systems and methods for controlling aerodynamic control surfaces of aircraft including a first actuator receiving a first input and a first linear...
2018/0273198 HOT-SWAPPABLE HYBRID APU FOR AIRCRAFT
A distributed auxiliary-power-unit (APU) system for an aircraft includes one or more battery modules for storing electrical power, and a plurality of racks...
2018/0273197 HYBRID AUXILIARY POWER UNIT FOR AIRCRAFT
An auxiliary power unit (APU) for aircraft is provided. The APU includes one or more battery modules for storing electrical power and an integrated controller...
2018/0273196 METHOD FOR AUTOMATIC SHUTDOWN OF ENGINES OF A TWIN-ENGINED AIRCRAFT
A method to automatically shutdown engines of a twin-engine aircraft where each engine is controlled by a control unit (4, 5) and an interface device (6)...
2018/0273195 A VEHICLE COMPRISING AN ENGINE RESTART SYSTEM
A vehicle (100) comprising: an engine (102); a system for starting the engine (102); a fault detection module (120); an electrical power source (110); and a...
2018/0273194 AERIAL VEHICLE
The disclosure relates to an unmanned aerial vehicle, wherein the fuel cell provides a structural component of the vehicle.
2018/0273193 ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AIRPLANE TAKEOFF, LANDING OR IN-FLIGHT...
Electrically operated propellant thrust assist supplements an airplane's takeoff, landing or inflight maneuvers. Unlike conventional SRM propellants, the burn...
2018/0273192 REUSABLE EVACUATION SYSTEM RESTRAINT
A releasable restraint for an inflatable slide is disclosed, in accordance with various embodiments. The releasable restraint may comprise a first mating...
2018/0273190 DUAL CONFIGURATION EVACUATION ASSEMBLY
An evacuation assembly of an aircraft may include an evacuation slide and a sheet coupled to the evacuation slide. The sheet may be deployable in a negative...
2018/0273189 LIGHT WEIGHT VARIABLE FORCE RESTRAINT
An evacuation system may comprise an evacuation slide configured to be deployed from an aircraft, a first strap coupled to the evacuation slide, a second strap...
2018/0273188 ASYMMETRIC YOKE
An evacuation assembly may comprise an evacuation slide and a first yoke coupled to the evacuation slide. The first yoke may comprise a first strap and a...
2018/0273187 AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
An aircraft with a fuselage that comprises at least one hollow beam element, wherein the at least one hollow beam element accommodates at least one hollow duct...
2018/0273186 ENVIRONMENTAL CONTROL SYSTEM PACK WITH AN AIR SUPPLY MANIFOLD
An air supply manifold includes an outer duct, a first inner duct, and a second inner duct. The outer duct is configured to transfer a fluid from the outer...
2018/0273185 AIRCRAFT CABIN ARRANGEMENT OPTIMISED FOR THE INSTALLATION OF SEATS FOR THE FLIGHT CREW
The invention relates mainly to an aircraft cabin (10) arrangement comprising: at least one cabin attendant seat, called a high-comfort seat (11), which can...
2018/0273184 Method and System for Homogenous Thermoplastic Seat Back Assembly
A seat back assembly that includes a composite seat back cover. The composite seat back cover includes at least one composite layer, that includes a layer of...
2018/0273183 INERTIA REEL INTERFACE FOR STOWABLE SEATS
An inertia reel interface for stowable seats is provided. The inertia reel interface may allow for simple access and replacement of inertia reels during...
2018/0273182 GALLEY MONUMENT WITH PASSENGER FOOT WELLS
A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories...
2018/0273181 SYSTEM AND METHOD FOR PROVIDING AN INTEGRATED USER INTERFACE SYSTEM AT A SEAT
A light-weight and low-power integrated system module suitable for installation at a passenger seat disposed aboard a passenger vehicle and methods for...
2018/0273180 MULTIFUNCTIONAL CONTAINER SYSTEM FOR PRODUCING A CONTAINER UTILIZABLE IN A CARGO COMPARTMENT OF AN AIRCRAFT
A multifunctional container system for producing a container for a cargo compartment of an aircraft includes a first lateral container component, which forms a...
2018/0273179 SYSTEM FOR THE EMERGENCY OXYGEN SUPPLY OF PASSENGERS IN AN AIRCRAFT
A system for the emergency oxygen supply of passengers in an aircraft includes at least one primary oxygen mask and at least one secondary oxygen mask arranged...
2018/0273178 CARPET DISPLAY SYSTEMS AND METHODS
A carpet display system includes a plurality of carpet modules. Each of the plurality of carpet modules includes a translucent support panel, a carpet layer...
2018/0273177 SEMI-AUTOMATED LOCK ASSEMBLY
A semi-automated lock assembly is provided and includes a housing, a pawl rotatably coupled to the housing to occupy and rotate between retracted and erected...
2018/0273176 SYSTEMS AND METHODS FOR IN-FLIGHT RETRIEVAL OF UNMANNED AERIAL VEHICLES
Presently disclosed systems and methods are configured for in-flight retrieval of unmanned aerial vehicles (UAVs). Such systems generally include a retrieval...
2018/0273175 DRONE WITH TARGET TRACKING AND SIGNAL OUTPUT
An unmanned aircraft is described. The unmanned aircraft includes a signal output unit and a control unit. The control unit receives at least one signal to be...
2018/0273174 DISPOSABLE AIR VEHICLE AND METHOD OF DELIVERING AID
An unmanned disposable air vehicle (1) comprising a structural part (3) that has an outer structure (17) and an inner structure (15) located inside the outer...
2018/0273173 AUTONOMOUS INSPECTION OF ELONGATED STRUCTURES USING UNMANNED AERIAL VEHICLES
Devices and methods of autonomously inspecting elongated structures, such as blades of wind turbines, are disclosed. An unmanned aerial vehicle (UAV) is guided...
2018/0273172 Methods and Systems for Transitioning an Aerial Vehicle Between Hover Flight and Crosswind Flight
A method includes operating an aerial vehicle in a hover-flight orientation. The aerial vehicle is connected to a tether that defines a tether sphere having a...
2018/0273171 AIRCRAFT, RADIO NETWORK, AND METHOD FOR TRANSMITTING INFORMATION
The invention relates, among others, to an aircraft (10) comprising at least one electromotive drive (11a, 11b) and a controller (12) with which the aircraft...
2018/0273170 TRANSFORMABLE UNMANNED AERIAL VEHICLE
An unmanned aerial vehicle (UAV) including wing sections and hinge assemblies. Each wing section includes an airfoil and a propulsion unit. The wing sections...
2018/0273169 Tiltrotor Aircraft having Rotatable Wing Extensions
A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is...
2018/0273168 VERTICAL TAKEOFF AND LANDING AIRCRAFT
An aircraft for use in fixed wing flight mode and rotor flight mode while maintaining a horizontal fuselage is provided. The aircraft can include a fuselage,...
2018/0273167 ROTORCRAFT ANTI-TORQUE AND DIRECTIONAL CONTROL USING A CENTRIFUGAL BLOWER
In one embodiment, a rotorcraft comprises a fuselage, a tail boom, a rotor system, and a centrifugal blower system. The centrifugal blower system comprises a...
2018/0273166 ROTARY WING VEHICLE
A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with...
2018/0273165 MULTIROTOR UNMANNED AERIAL VEHICLE
The present disclosure relates to a multirotor unmanned aerial vehicle, comprising a fuselage, being provided with at least one support arm in a transverse...
2018/0273164 MULTIROTOR FLYING VEHICLE
A multirotor flying vehicle including at least one rotor support frame organized on a geometric grid, with a plurality of rotor assemblies coupled to the at...
2018/0273163 ADAPTABLE ROTOR BLADE DESIGN FOR PERFORMANCE FLEXIBILITY
In one embodiment, a rotor blade may comprise a blade body, a spar structure, and a blade nose. The blade body may comprise a skin, wherein the skin is...
2018/0273162 DUAL-STAGE, PRESSURE-ACTIVATED, MIXED FLUID GAS SHOCK STRUT SERVICING MONITORING SYSTEM
A monitoring system for a dual-stage, pressure-activated, mixed fluid gas shock strut, may comprise a controller, and a tangible, non-transitory memory...
2018/0273161 WING FOR AN AIRCRAFT
A wing for an aircraft including a slat, and a connection assembly for movably connecting the slat to the main wing. The connection assembly includes a first...
2018/0273160 High Stiffness Hub Assembly for Proprotor Systems
A high stiffness hub assembly for a proprotor system operable to rotate with a mast of a tiltrotor aircraft having helicopter and airplane flight modes. The...
2018/0273159 AIRCRAFT WING SPACE FRAME
Aircraft wings have an interior volume that incorporates a space frame as a primary supporting structure of the wing, and enables securement of an aircraft...
2018/0273158 Multi-Architecture Modular Unmanned Aerial System
Disclosed herein is a modular aerial vehicle system having a fuselage module configured to couple with a plurality of lift generation modules. The modular...
2018/0273157 GALLEY TROLLEY COMPARTMENT DOORS
Embodiments of the present disclosure relate generally to galley trolley compartment doors that replace traditional trolley retainer latches used to secure...
2018/0273156 OPENING SYSTEM AND METHOD FOR AN AIRCRAFT EMERGENCY DOOR
The invention proposes a simple system, with small space requirement, without hinge arms or sealing skirt, while providing secure and effective opening. To...
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