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Patent # Description
2018/0057180 DRONE WITH MAGNET FLUID SEALED BEARING UNIT AND DRIVE MOTOR HAVING THE BEARING UNIT
One object is to provide a drone capable of achieving desired performance by preventing entry of foreign matter such as water droplets or dust particularly...
2018/0057179 AN AIRCRAFT
An aircraft comprises at least first and second gas turbine engines arranged in a line extending generally normally to an aircraft longitudinal axis (A), each...
2018/0057178 ILLUMINATED ROPE AS AN AIRCRAFT EMERGENCY EGRESS AID
In some implementations, in an emergency in the vehicle, an emergency evacuation path is illuminated using the light emitted from the emergency evacuation rope...
2018/0057177 Deicing Apparatuses Comprising at least one standoff
Apparatuses for and methods of deicing aircraft surfaces, engine inlets, windmill blades and other structures. Deicing apparatuses can comprise at least one...
2018/0057176 Electrically Conductive Materials for Heating and Deicing Airfoils
Composite airfoils of the present disclosure comprise a root section including a first surface. The airfoils comprise an intermediate section having a first...
2018/0057175 Operating-phase-dependently controllable aircraft air conditioning system and method for operating such an...
An aircraft air conditioning system comprises an ambient air line which is configured have ambient air flow therethrough and is connected to a mixer of the...
2018/0057174 Aircraft air conditioning system and method for operating such an aircraft air conditioning system
An aircraft air conditioning system comprises an ambient air line configured to have ambient air flow therethrough and being connected to a mixer of the air...
2018/0057173 HYBRID METHOD AND AIRCRAFT FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM USING A POWER GENERATOR FOUR WHEEL...
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air...
2018/0057172 ADVANCED METHOD AND AIRCRAFT FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM USING A DUAL COMPRESSOR FOUR WHEEL...
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air...
2018/0057171 ADVANCED METHOD AND AIRCRAFT FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM USING A THREE WHEEL TURBO-MACHINE
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air...
2018/0057170 ENHANCED METHOD AND AIRCRAFT FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM USING A TWO WHEEL TURBO-MACHINE...
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air...
2018/0057169 STOWABLE REVERSIBLE SEAT
A stowable reversible seat for a vehicle includes a first member pivotally coupled to a floor for supporting a seat base, a second member releasably secured to...
2018/0057168 Lateral linear moving curtain rail
A vehicle cabin curtain rail attachment comprising a guiding rail configured to be mounted fixedly within a cabin and a movable curtain rail section to receive...
2018/0057167 DIRECTED FRAGMENTATION FOR UNMANNED AIRBORNE VEHICLES
Directed fragmentation of an unmanned aerial vehicle (UAV) is described. In one embodiment, the UAV includes various components, such one or more motors,...
2018/0057166 Pressure Activated Release for Deployment of Surface, Aerial and Subsea Payloads
A pressure activated release system and method are disclosed for deployment of surface, aerial and subsea payloads. The system and method include a payload...
2018/0057165 SYSTEM FOR RECHARGING REMOTELY CONTROLLED AERIAL VEHICLE, CHARGING STATION AND RECHARGEABLE REMOTELY CONTROLLED...
A system including an aerial vehicle having an airframe and a power source onboard the aerial vehicle, wherein the aerial vehicle includes a landing gear...
2018/0057164 UNMANNED AERIAL VEHICLE
An unmanned aerial vehicle (UAV) including a vehicle body and an airflow thruster is provided. The vehicle body has a center hub, an airflow guiding structure...
2018/0057163 UNMANNED AERIAL VEHICLE
A vertical take-off and landing ("VTOL") unmanned aerial vehicle ("UAV") system and a method of controlling the same, wherein such method controls the...
2018/0057162 Aircraft having Rotor-to-Wing Conversion Capabilities
A tail sitter aircraft includes a fuselage having a forward portion and an aft portion. The forward portion of the fuselage includes first and second rotor...
2018/0057161 Aircraft having Dual Rotor-to-Wing Conversion Capabilities
A tail sitter aircraft includes a fuselage having a forward portion and an aft portion. The forward portion of the fuselage includes first and second rotor...
2018/0057160 Aircraft Generating a Triaxial Dynamic Thrust Matrix
A tri-wing aircraft includes a fuselage having a longitudinally extending fuselage axis. Three wings extend generally radially outwardly from the fuselage axis...
2018/0057159 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...
2018/0057158 ROTORCRAFT HAVING A ROTARY WING AND AN ORIENTABLE PROPELLER, AND A METHOD APPLIED BY THE ROTORCRAFT
A rotorcraft having a fuselage surmounted by a main rotor. The rotorcraft has a first propeller and a second propeller driven in rotation respectively about a...
2018/0057157 Tilting Ducted Fan Aircraft Generating a Pitch Control Moment
In some embodiments, an aircraft includes a fuselage having a forward portion and an aft portion. First and second ducted fans are supported by the forward...
2018/0057156 AIRCRAFT PROVIDED WITH A SET OF SWASHPLATES AND WITH AT LEAST ONE SERVO-CONTROL THAT IS INCLINED
An aircraft provided with a rotor that is provided with blades and a set of swashplates. The set of swashplates comprises both a rotary swashplate and also a...
2018/0057155 MULTICOPTER WITH WIDE SPAN ROTOR CONFIGURATION
A multicopter aircraft with a wide span rotor configuration is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage and a...
2018/0057154 AIRCRAFT LANDING GEAR SHOCK ABSORBER ASSEMBLY
An aircraft landing gear shock absorber assembly having an outer casing having a bore which extends through the outer casing. The bore has a first opening and...
2018/0057153 AIRCRAFT WITH AN EMERGENCY FLOATATION SYSTEM
An aircraft with an emergency flotation system, the emergency flotation system being activated upon an emergency landing of the aircraft on water, for...
2018/0057152 FLOAT DUCTS AND FLOOR PANEL
An aircraft includes a float which provides buoyancy when the aircraft floats on a surface of water. The aircraft also includes a rotor where the rotor is...
2018/0057151 AIRCRAFT WHEEL WITH A SEPARABLE BEARING BOX
The invention relates to an aircraft wheel comprising a hub (52) for mounting the wheel on a landing gear axle to enable the wheel to rotate about an axis of...
2018/0057150 DEPLOYABLE ASSEMBLY FOR A PROPULSOR
An aircraft includes a fuselage extending between a forward end and an aft end. The aircraft additionally includes a propulsor mounted to the fuselage at the...
2018/0057149 ACTUATORS FOR HIGH LIFT DEVICES ON AIRCRAFT
Actuators for high lift devices on aircraft are disclosed herein. An example apparatus includes an actuator for a high lift device of an aircraft including a...
2018/0057148 Tiltrotor Aircraft having Active Wing Extensions
A tiltrotor aircraft includes a fuselage supporting first and second wings each having an outboard end. First and second nacelles are respectively coupled to...
2018/0057147 AIRCRAFT HAND CONTROLLER WITH DECOUPLED THROTTLE
An aircraft hand controller is disclosed. The hand controller includes a set of finger controls on a single hand grip structure, the set of finger controls...
2018/0057146 PROPELLER PITCH CONTROL ACTUATION SYSTEM
A propeller pitch control actuation system includes a relatively lightweight, relatively inexpensive means for selectively preventing the propeller pitch...
2018/0057145 Nose Cone
Disclosed here are systems for detachable airframe components including detachable nose cones, propeller assemblies and motors. In some example embodiments,...
2018/0057144 LATCHING AND LOCKING MECHANISM FOR A FOLDABLE WING ARRANGEMENT
A wing arrangement for an aircraft including a latching arrangement (29, 29', 29'') having a latching member (31, 31', 31'') and an engagement device (33),...
2018/0057143 AIRFOIL EXTENSION FOR AN AIRCRAFT WING
An airfoil extension for a wing of an aircraft, the airfoil extension including an upper surface wall and a lower surface wall, the upper surface wall and the...
2018/0057142 Wing and Method of Manufacturing
A wing includes a wing box including interconnected spars, an interior system installed within the wing box, an opposed pair of skins fastened to and covering...
2018/0057141 BIOMIMETIC AIRFOIL BODIES AND METHODS OF DESIGNING AND MAKING SAME
An airfoil body may include a plurality of tubercles along a leading edge of the airfoil body and a plurality of crenulations along a trailing edge of the...
2018/0057140 Heat Shield Flange Sliding Joint
A thermal expansion joint is disclosed. In one non-limiting example the thermal expansion joint includes a bottom portion extending between a support structure...
2018/0057139 FIRE RETARDANT AVIATION LAMINATE
An aviation laminate includes a plurality of wooden elements, and an adhesive disposed between the plurality of wooden elements, wherein the adhesive includes...
2018/0057138 AIRCRAFT WITH CABIN ACOUSTIC SYSTEMS HAVING QUARTER WAVELENGTH ABSORBERS
An aircraft includes a fuselage, a cabin surface, and a first chamber. The cabin surface is disposed within the fuselage and defines a first aperture and at...
2018/0057137 Methods and Components for Wing-to-Fuselage Integration
A method for wing-to-fuselage integration is disclosed. The method includes attaching a fitting to a wing box assembly of an aircraft at an early stage of...
2018/0057136 WING LOCK AND DISCONNECT MECHANISMS FOR A RC AIRCRAFT
Remote control aircraft may benefit from airframes with components that are easy to connect and disconnect. For example, during repair, storage, or transport,...
2018/0057135 SELF-RIGHTING AERONAUTICAL VEHICLE AND METHOD OF USE
A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to...
2018/0057134 OUTBOARD MOTOR
An outboard motor includes an engine having an output portion. A lower gear mechanism drives a propeller disposed below the engine. A transmission includes an...
2018/0057133 SYSTEMS AND METHODS FOR CONTROLLING VESSEL SPEED WHEN TRANSITIONING FROM LAUNCH TO CRUISE
A method for controlling a speed of a marine vessel includes accelerating the marine vessel in response to a launch command. The method then includes holding...
2018/0057131 TROLLING MOTOR WITH WIND SENSOR
A wind sensor, such as a sonic anemometer, may be utilized to cause a trolling motor to activate to propel a watercraft toward a virtual anchor location,...
2018/0057130 IMPROVED MOUNTING AND ACTUATION DEVICE
In at least one embodiment the present invention provides an improved mounting and actuation device having a mounting body defining a stowage cavity and an...
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