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Patent # Description
2016/0185469 METHOD AND SYSTEM FOR AIRCRAFT APPEARANCE INSPECTION
An aircraft appearance inspection method includes an initial data acquisition step of acquiring initial data at an initial time, an inspection data acquisition...
2016/0185468 FLIGHT TEST HINGE ASSEMBLY
A system for calculating forces exerted into an aircraft component may include a test hinge assembly and a monitoring system. The test hinge assembly may be a...
2016/0185467 APPARATUS FOR AUTOMATICALLY MOUNTING AND DISMOUNTING AIRCRAFT FUSELAGE
An apparatus for automatically mounting and dismounting an aircraft fuselage includes stages disposed to be spaced apart from each other, positioners disposed...
2016/0185466 SYSTEM AND METHOD FOR ENHANCING DISTRIBUTION LOGISTICS AND INCREASING SURVEILLANCE RANGES WITH UNMANNED AERIAL...
A system and method for enhancing distribution logistics and surveillance ranges with unmanned aerial vehicles (UAV) and at least one dock in a dock network....
2016/0185465 DEVICE FOR A PROPELLER BLADE
A self-destruction device adapted to be installed in a propeller blade, the self-destruction device including a detector adapted to detect a release of the...
2016/0185464 METHOD AND APPARATUS FOR MONITORING THE WING ANTI-ICING VALVE
The present invention relates to a system for monitoring the wing anti-icing valve, comprising: time record device configured to record the time for opening or...
2016/0185463 SYSTEM AND METHOD OF INTEGRITY CHECKING DIGITALLY DISPLAYED DATA
System and method of integrity checking digitally displayed data in a display system having a display comprising a pixel array with a viewable area, including...
2016/0185462 AIRCRAFT ELECTRICAL SYSTEM OPERATING METHOD
A method of controlling an aircraft electrical system (40). The electrical system (40) comprises an alternating current electrical machine (56, 58) comprising...
2016/0185461 INTEGRATED AUXILIARY POWER UNIT, STARTER-GENERATOR-MOTOR, AND VAPOR CYCLE COOLING SYSTEM FOR AN AIRCRAFT
A system for an aircraft includes a compressor for a vapor cycle cooling system (VCCS) for providing cabin air conditioning; an APU for mechanically driving...
2016/0185460 AIRCRAFT WITH COUNTER-ROTATING TURBOFAN ENGINES
An aircraft including a frame, a first turbofan engine coupled to the frame, and a second turbofan engine coupled to the frame is disclosed. The first turbofan...
2016/0185459 Auxiliary Device for High-Flying Aircraft
An auxiliary device is provided for a high-altitude airplane. The auxiliary device includes a drive, which is independent of the airplane, for the ascent of...
2016/0185458 Electro-Expulsive De-Icing System for Aircraft and Other Applications
An apparatus for removing ice from an object (e.g., in-flight ice removal from the skin of an aircraft) includes an actuator assembly that forms an elongated...
2016/0185457 DEVICE FOR REMOVING DEBRIS FROM AN AERODYNAMIC STRUCTURE
A device for removing debris, such as insects and ice, from an aerodynamic structure of an aircraft and in which the aerodynamic structure has upper and lower...
2016/0185456 POWER AND DATA TRANSMISSION OVER THIN CONDUCTOR FOR UNMANNED AERIAL VEHICLE
A system for tethered unmanned aerial vehicle having an unmanned aerial vehicle platform capable of flight. At least one propeller is mounted on the platform....
2016/0185455 Electromagnetic Actuator System
A novel electromagnetic actuator designed to operate at system resonance, used in the construction of a unique vehicle system, is presented herein. An...
2016/0185454 UNMANNED AERIAL VEHICLE
Systems and methods are described herein related to an unmanned aerial vehicle, the unmanned aerial vehicle includes: a frame portion, two rear arms extending...
2016/0185453 AIRCRAFT LANDING GEAR ASSEMBLY
An aircraft landing gear includes an axle on which wheel and brake assemblies are mounted. An adaptor member is mounted on the axle and arranged to define a...
2016/0185452 Clutch Driven Aircraft Electric Taxi System and Method
A clutch driven aircraft electric taxi system is provided with a clutch assembly designed to be automatically selectively engaged or disengaged as required to...
2016/0185451 LANDING GEAR WELL ROOF
An aircraft landing gear well roof including a first reinforced main structure and a second reinforced main structure spaced from each other in a transverse...
2016/0185450 AIRCRAFT WINGLET DESIGN HAVING A COMPOUND CURVE PROFILE
An improved winglet design is presented for aircraft wherein the winglet configuration is well suited for aircraft wings having moderate to no aft swept, or...
2016/0185449 FLUID-VECTORING SYSTEM
A jet aircraft includes an aircraft integrated, fluid vectoring, exhaust nozzle system. Implementation of this disclosure may eliminate or reduce the size of...
2016/0185448 CONTROL SYSTEM AND METHOD FOR AN AIRCRAFT
A control system and method for an aircraft configured to operate according to a first mode of operation corresponding to an automatic piloting of the aircraft...
2016/0185447 UNMANNED AERIAL VEHICLE ANGULAR REORIENTATION
A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to...
2016/0185446 TRIM ADJUSTMENT DEVICE, AIRCRAFT, AND METHOD OF PERFORMING TRIM ADJUSTMENT
Trim adjustment devices 20, 30, 40 at least include trim control switches 21, 31, 41 for performing a trim adjustment; acquisition sections 22, 32, 42 for...
2016/0185445 ELEVON CONTROL SYSTEM
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted...
2016/0185444 MANUAL WING-FOLD MECHANISM
A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed...
2016/0185443 DUAL-RIB MORPHING LEADING EDGE
A mechanism for changing a shape of a leading edge of an airfoil may include a first rib and a second rib. The first rib may include a plurality of first rib...
2016/0185442 METHOD AND APPARATUS FOR REDUCING STRUCTURAL VIBRATION AND NOISE
A conjugate damper for a structural panel includes a constraining sheet extending between a first edge and a second edge. Each of the first edge and the second...
2016/0185441 CONTROL METHOD AND DEVICE FOR AIRCRAFT DOOR AND AIRCRAFT DOOR INCORPORATING SAME
A device and a control method are described for a swinging aircraft door (3), mobile around a swinging axis (21) substantially parallel to the longitudinal...
2016/0185440 AIRCRAFT COMPRISING A HATCH AND A FALL-PROTECTION DEVICE
An aircraft including a hatch and a fall-protection device. The aircraft includes a structure exhibiting a roof pierced with an opening, a cover plate, and a...
2016/0185439 AIRCRAFT REAR STRUCTURE
An aircraft rear structure that comprises a rear pressure bulkhead, and a lifting surface located at both sides of the fuselage of the aircraft. The lifting...
2016/0185438 JOINT ASSEMBLY AND METHOD CONNECTING AN AIRCRAFT BELLY FAIRING TO THE FUSELAGE PROVIDED WITH A PARTICULARLY...
A joint assembly in an aircraft connecting a belly fairing to the fuselage of the aircraft. The belly fairing has a sewing angle connected to a main belly...
2016/0185437 TAIL CONE OF AN AIRCRAFT
A tail cone of an aircraft, more specifically a tail cone made of composite materials comprising an internal skin, an external skin surrounding the internal...
2016/0185436 Skin Impact Snubber
In some embodiments, an aircraft includes a structural assembly, a skin, and a snubber. The structural assembly comprises a first rigid element and a second...
2016/0185435 MULTIFUNCTIONAL BALLOON MEMBRANE
Disclosed herein is a lighter-than-air (LTA) device and method of making the same. In an embodiment, the LTA device may include a membrane having a flexible...
2016/0185434 DYNAMIC POSITIONING VESSEL WITH A PLURALITY OF REDUNDANCY ZONES
The invention relates to a high reliability vessel where redundancy zones are provided. It is an objective of the present invention to provide an improved...
2016/0185433 OUTBOARD MOTOR
Disclosed is an outboard motor including a drive shaft that transmits rotational power from an engine, a shift unit provided in the middle of the drive shaft,...
2016/0185432 OUTBOARD MOTOR
An outboard motor includes a drive shaft that transmits rotational power from an engine, a shift unit provided in the middle of the drive shaft, and a water...
2016/0185431 ROTATING ELECTRICAL MACHINE APPARATUS
In a rotating electrical machine apparatus, a rotor portion provided in a cylindrical portion and a stator portion provided in a recessed portion in which the...
2016/0185430 Powered Hydrofoil Board
A passively stable personal hydrofoil watercraft that has a flotation device, wherein a user can ride in a prone, kneeling, or standing position. The...
2016/0185429 ASSEMBLY OF FLOATABLE MODULES
An assembly (3) comprising at least a first module (1) and a second module (2) with respective longitudinal axes (5) is described. Each one of the modules (1,...
2016/0185428 DISCONNECTABLE SUBMERGED BUOY MOORING DEVICE COMPRISING CLAMPING DOGS
A mooring assembly includes: a mooring buoy having a central axis, an upper ring portion providing an upper abutment surface; a mooring structure including a...
2016/0185427 ANCHOR LINE TENSIONING METHOD
Method for mooring an offshore structure includes: providing a mooring line having one end connected to the sea bed and a connector at a free end; lifting the free...
2016/0185426 TOWING DEVICE WITH A TWO-PIECE FAIRLEAD
A towing device intended to equip the deck of a ship (10) and comprising a winch (16), a cable (14) and a fairlead (20), the cable (14) circulating in the...
2016/0185425 METHODS AND APPARATUS TO COUPLE COMPONENTS TO A FUEL TANK
Apparatus and methods to couple fuel components to a fuel tank are described. An example method includes coupling a carrier to a guide suspended in a cavity of...
2016/0185424 INFLATABLE CRAFT HAVING V-SHAPED HULL AND FLAPS
The invention relates to a vessel which includes two watertight flaps (13) attached in a tensioned state on the two sides of the longitudinal keel (7), each...
2016/0185423 DEVICE FOR REDUCING FRICTIONAL RESISTANCE, SHIP COMPRISING THE DEVICE, AND METHOD OF REDUCING FRICTIONAL...
A device for reducing frictional resistance includes: a chamber which is provided to a draft part of a hull and in which blowing holes blowing out air into the...
2016/0185422 Surf Tab
A wake-modifying a surf tab that can be attached to a watercraft is disclosed. That surf tab includes a control plate assembly, a mounting hinge for attaching...
2016/0185421 BICYCLE OPERATING SYSTEM
A bicycle operating system comprises an operating device. The operating device is configured to be mounted to a bicycle body. The operating device includes an...
2016/0185420 Multiple Sprocket Assembly for a Bicycle
A roller chain based drive train for a bicycle includes a sprocket assembly configured for mounting to a hub of a rear wheel of the bicycle. The sprocket...
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