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Patent # Description
2018/0305035 AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE AND PROVIDED WITH AN AIR FILTER AND WITH AN AIR FILTER BYPASS DUCT
An air intake unit for an engine of an aircraft and having: a housing, inside which a plenum is defined, which can be connected to the engine of the aircraft;...
2018/0305034 Segmented Acoustic Insert
An acoustic insert comprises a sleeve having a first end and a second end. The sleeve comprises segments between the first end and the second end. A first...
2018/0305033 METHOD FOR MANAGING IMBALANCE IN A DISTRIBUTED PROPULSION SYSTEM
A method for managing unbalanced thrusts caused by engine failures in an aircraft provided with a distributed propulsion system, the distributed propulsion...
2018/0305032 ENGINE ASSEMBLY FOR AN AIRCRAFT, COMPRISING A FRONT ENGINE MOUNT INCORPORATED WITH THE BOX OF THE MOUNTING PYLON
An engine assembly for an aircraft, comprising an engine mounting pylon comprising a primary structure forming a box closed by a front closing rib, a front...
2018/0305031 SEWN REINFORCEMENT FEATURES FOR PREVENTION OF STITCH BREAKAGE IN A PNEUMATIC DE-ICER
A de-icing assembly for a surface of an aircraft includes a carcass, seams, inflation passages, a manifold, and a reinforcement stitchline. The carcass...
2018/0305030 Unknown
Disclosed is a method and a device for thermally controlling a plurality of cabins of a vehicle from a mixing chamber supplied with air from at least one air...
2018/0305029 AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system (4) comprising: a temperature sensor (30) configured...
2018/0305028 MULTIPOSITION AIR INTAKE SYSTEM FOR AN AIRCRAFT
An air intake system for an aircraft having a ventral fairing and comprising a scoop having a ventral wall with a first coupling and an opening. The scoop is...
2018/0305027 AIRCRAFT CABIN MOISTURE CONTROL USING MOISTURE WICKING HEAT SHRINK TUBING
A moisture wicking heat shrink sleeve for aircraft cabin moisture control incorporates a heat shrinkable tube of predetermined length receivable over a...
2018/0305026 Increase the Airline Seat Comfort and Revenue via Track-based Elevated Seat
The present invention provides airlines with the track-based elevated seat arrangement for an improved passenger comfort and hence improved revenue. In our...
2018/0305025 Aircraft passenger cabin area comprising a restricted area
An aircraft passenger cabin area comprises a main aisle extending substantially parallel to a longitudinal axis of the aircraft passenger cabin area, a...
2018/0305024 Passenger seat having a displaceable seat element
A passenger seat comprises a carrier structure, a backrest and a seat element displaceably fastened to the carrier structure, relative to the backrest, in a...
2018/0305023 SEQUENTIALLY EXTENDING AND ROTATING TABLE MECHANISM
A passenger seat tray table mechanism that deploys by way of a controlled sequence of translational and rotational movements. Dependent on tray table mechanism...
2018/0305022 SEAT SUPPORT SYSTEM
Described is a passenger seat that includes a seat bottom assembly with a forward edge and a rear edge and a seat back assembly extending up from the rear edge...
2018/0305021 SCREEN SUPPORT CONFIGURED FOR ATTACHMENT TO A BACKREST OF A SEAT
A screen support configured to attach a screen to a seat equipped with a rear enclosure and including an attachment system configured to clamp the rods of a...
2018/0305020 Structural Panels for Exposed Surfaces
An apparatus includes a foam layer, a coating layer and an elastomer. The foam layer includes a first surface for coupling the apparatus to a surface exposed...
2018/0305019 FIXED-WING AIRCRAFT WITH INCREASED STATIC STABILITY
The invention relates to an aircraft having at least one wing (5) including, at each end thereof, a fin (6) forming an angle of between 0.degree. and...
2018/0305018 Transport drone
A transport drone includes: a drone body; a transport unit for carrying an object to be transported; a balancing unit comprising a balancing frame and a...
2018/0305017 DRONE DEVICE FOR NEWS REPORTING
A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the...
2018/0305016 AUTONOMOUS MOBILE DEVICE SECURITY SYSTEM
A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the...
2018/0305015 DRONE DEVICE SECURITY SYSTEM
A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the...
2018/0305014 DRONE DEVICE FOR REAL ESTATE
A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the...
2018/0305013 RECONFIGURABLE BATTERY-OPERATED VEHICLE SYSTEM
A quadrotor UAV including ruggedized, integral-battery, load-bearing body, two arms on the load-bearing body, each arm having two rotors, a control module...
2018/0305012 METHOD FOR CONTROLLING SMALL-SIZE UNMANNED AERIAL VEHICLE
A method for controlling a small-size unmanned aerial vehicle that sets a flight path based on a real-time state of the ground and that controls the small-size...
2018/0305011 ROTARY-WING AIR VEHICLE AND METHOD AND APPARATUS FOR LAUNCH AND RECOVERY THEREOF
A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in...
2018/0305010 DRONE-BASED SMOKE DETECTOR
One embodiment provides a method comprising receiving a request to release a utility holder detachably mounted to a surface mount. The utility holder maintains...
2018/0305009 AN AIR VEHICLE AND IMAGING APPARATUS THEREFOR
An air vehicle (10) comprising a main body (12) and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body (12) having...
2018/0305008 HYBRID MULTICOPTER AND FIXED WING AERIAL VEHICLE
An aerial vehicle is includes a wing, first and second rotors, and a movement sensor. The first and second multicopter rotors are rotatably coupled to the...
2018/0305007 CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES
A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream. At least one tail conduit is fluidly coupled to the...
2018/0305006 PITCH BEARING ASSEMBLY FOR ROTOR SYSTEM AND AIRCRAFT
A pitch bearing assembly includes an inboard pitch bearing including an inner race and an outer race, the outer race including a radially outwardly protruding...
2018/0305005 Vertical Take-Off and Landing Aircraft
Disclosed herein is a vertical take-off and landing (VTOL) aircraft having three lifting surfaces and separate lift and cruise systems. The VTOL aircraft may...
2018/0305004 A SHROUD FOR AN AIRCRAFT
A shroud for an aircraft having a noise reducing material on or in an inner surface of the shroud adjacent to one or more tips of the propeller. The noise...
2018/0305003 SEALS FOR ROTOR SYSTEM FAIRINGS
A fairing system, includes a hub fairing and a fixed fairing, such as a shaft fairing or a pylon fairing, both arranged about a rotation axis. A gap is defined...
2018/0305002 MULTI-COPTER WITH INTERMEDIATE SUPPORTING BAR FOR REDUCING FUSELAGE VIBRATION AND CONTROL METHOD OF REDUCING...
Provided is a multi-copter, including: a fuselage; three or more intermediate supporting bars which have one ends fixed to the fuselage and radially extend...
2018/0305001 AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT
An aircraft landing gear shock absorbing strut having an outer cylinder and a sliding tube coupled within the cylinder bore to move between compressed and...
2018/0305000 AIRCRAFT LANDING GEAR ASSEMBLY
An aircraft landing gear bogie beam including first and second ends and a mounting bearing for connection to an aircraft landing gear main strut between the...
2018/0304999 AIRCRAFT LANDING GEAR ASSEMBLY
An aircraft landing gear assembly having a main strut pivotally coupled to an aircraft, a bogie beam pivotally connected to the main strut, a first axle...
2018/0304998 TAIL SKID SHOCK ABSORBER AND INDICATOR
A tail skid shock absorber including an outer shock absorber canister, a crushable indicator cartridge disposed within the outer shock absorber canister, and...
2018/0304997 Split Winglet
A split winglet has a leading airfoil (LA) comprising a LA leading edge, a LA trailing edge, a LA upper surface, and a LA lower surface. The split winglet also...
2018/0304996 TRIAXIAL HELICOPTER
A triaxial helicopter includes a fuselage and an airframe, and three rotor modules and a driving source are installed to the airframe, and two turbofans are...
2018/0304995 FLIGHT CONTROL SYSTEM TRANSMISSION
An aircraft is provided. The aircraft includes fuselage, an aerodynamic element extending from the fuselage and including a main section and an adjustable...
2018/0304994 FLIGHT CONTROL COMPUTER OF AN AIRCRAFT
A flight control computer of an aircraft is likely to operate in a so-called incidence protection mode in which it is configured to compute the deflection...
2018/0304993 EMERGENCY CONTROL OF AN AIRCRAFT
An aircraft emergency control system comprises at least one sensor (104A, 104B, 104C) configured to output an electronic signal relating to detection of...
2018/0304991 FEEDBACK SYSTEM FOR PITCH-ADJUSTABLE BLADES OF AIRCRAFT BLADED ROTOR
Systems and methods for providing pitch position feedback for pitch-adjustable blades of an aircraft bladed rotor are disclosed. In one embodiment, the systems...
2018/0304990 PROPELLER BLADE INDENTATIONS FOR IMPROVED AERODYNAMIC PERFORMANCE AND SOUND CONTROL
Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation....
2018/0304989 FIBRE REINFORCED COMPOSITE AEROFOIL STRUCTURES
A composite component adapted to be formed into an aerofoil, a method of forming an aerofoil, an aerofoil, an aircraft wing and a forming jig. The method...
2018/0304988 MECHANICALLY ATTACHED THERMAL PROTECTION SYSTEM
A mechanically attached thermal protection system (MATPS) includes an insulating tile having a top surface, a bottom surface, and a plurality of access holes...
2018/0304987 ACOUSTIC TREATMENT PANEL COMPRISING CELLS WHICH EACH CONTAIN A PLURALITY OF CONDUITS
An acoustic treatment panel in which each cell includes a plurality of conduits which extend from the porous acoustically resistive structure to the reflective...
2018/0304986 ACOUSTIC TREATMENT PANEL COMPRISING A POROUS ACOUSTICALLY RESISTIVE STRUCTURE COMPRISING CONNECTING CANALS
An acoustic treatment panel including a porous acoustically resistive structure which includes at least one external layer which is in contact with the...
2018/0304985 Structural Panels for Exposed Surfaces
A method includes determining a target acoustic profile based on acoustic conditions at an exterior surface exposed to weather. The method further includes...
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