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Patent # Description
2017/0267376 PORTABLE BALLOON LAUNCH RIG
A portable launch rig (PLR) may include a support structure including two side supports defining an interior space for lifting and filling a balloon envelope...
2017/0267375 AIRCRAFT ANTI-COLLISION LIGHT
A light source includes a circular light element having a light source diameter, and a reflector disposed at least partially within the circular light element,...
2017/0267374 MULTISPECTRAL SENSOR FUSION SYSTEM FOR PLATFORM STATE ESTIMATION
An electronic landing platform state module is configured to generate a state estimation of a platform surface at sea includes a plurality of electronic...
2017/0267373 Portable, Externally Mounted Device for Aircraft to Provide User Selected Readings of Airspeed, Pressure,...
The present invention relates to a portable, externally mounted device for aircraft used to provide user selectable readings of airspeed, pressure,...
2017/0267372 DRONE, IN PARTICULAR OF THE FLYING WING TYPE, PROVIDED WITH A MULTIFUNCTION SUPERSTRUCTURE ELEMENT
Disclosed are embodiments of a drone with a flattened tubular part protrudingly mounted on a module located on the fuselage of the drone, where the free distal...
2017/0267371 METHODS OF THREE DIMENSIONAL (3D) AIRFLOW SENSING AND ANALYSIS
Embodiments of methods and apparatus for close formation flight are provided herein. In some embodiments, a method of sensing three dimensional (3D) airflow by...
2017/0267370 ENGINE ASSEMBLY WITH DIRECT DRIVE OF GENERATOR
An engine assembly for use as an aircraft auxiliary power unit, having internal combustion engine(s) in driving engagement with an engine shaft, a generator...
2017/0267369 MOTOR-GENERATOR FOR HIGH EFFICIENCY AUXILIARY POWER SYSTEM
A system for driving an environmental control system (ECS) of a vehicle with ground-based electrical power may include a turbine engine on board the vehicle,...
2017/0267368 FUEL PIPE OF AIRCRAFT AND AIRCRAFT
To provide a fuel pipe of an aircraft that makes it possible to maintain temperature of fuel in the fuel pipe at appropriate temperature while giving...
2017/0267367 AIRCRAFT
A vertical takeoff and landing aircraft (101) for transporting persons or loads, including a plurality of preferably equivalent and redundant electric motors...
2017/0267366 TAKEOFF POWER MANAGEMENT SYSTEM AND METHOD FOR GAS TURBINE ENGINES
A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a control unit to command the gas turbine engine...
2017/0267365 SYSTEM AND METHOD FOR PROTECTING THE STRUCTURAL INTEGRITY OF AN ENGINE STRUT
A system for protecting the structural integrity of an engine strut may include a first monitor, a second monitor, and a controller communicatively coupled to...
2017/0267364 METHOD OF MONITORING AT LEAST ONE FREEWHEEL OF A ROTARY WING AIRCRAFT, AND AN AIRCRAFT
A method of monitoring a first freewheel interposed between a first drive shaft of a first engine and a rotor. The state of operation of said first freewheel...
2017/0267363 UPPER BIFI FRAME FOR A GAS TURBINE ENGINE AND METHODS THEREFOR
An upper bifi frame for preventing air leakage in a gas turbine engine including an engine casing and a fan case is provided. The upper bifi frame includes a...
2017/0267362 EMERGENCY VISION APPARATUS WITH HAND ACCESS
An emergency vision apparatus comprises an inflatable enclosure to enable a user to see through the enclosure when expanded and observe a source of information...
2017/0267361 ROTOR ICE PROTECTION SYSTEM
A rotor ice protection system (RIPS) apparatus for an aircraft to heat aircraft rotor blades is provided. The RIPS apparatus includes circuitry disposed to...
2017/0267360 THERMAL MANAGEMENT SYSTEM FOR DEICING AIRCRAFT WITH TEMPERATURE BASED FLOW RESTRICTOR
Assemblies are provided for an aircraft with a gas turbine engine. One assembly includes a body such as an inlet nose lip of a nacelle for the gas turbine...
2017/0267359 TANDEM AIR CYCLE MACHINE MODULE FOR ENVIRONMENTAL CONTROL SYSTEMS
Tandem air cycle machine modules include a first air cycle machine having a first compressor and a first turbine, a second air cycle machine having a second...
2017/0267358 DEWATERING DEVICE FOR AN AIR CONDITIONING SYSTEM OF A PLANE
The present invention provides a dewatering device for an air-conditioning system of a plane, comprising: one or more filter plates disposed within a mixing...
2017/0267357 RETRACTABLE AIR GASPER APPARATUS
An air gasper (air) for a vehicle includes an air inlet (26), a first housing (24) disposable through a panel in the vehicle (12), the first housing (24) being...
2017/0267356 Flight attendant seat, arrangement having a flight attendant seat, and aircraft area
A flight attendant seat comprises a carrier device having a first surface, a seat element movably coupled to the carrier device, and a backrest element movably...
2017/0267355 LIMITED SWIVEL APPARATUS FOR A PASSENGER SEAT
The present disclosure provides a swivel stop comprising a rotating member, a first boss coupled to the rotating member and a second boss coupled to the...
2017/0267354 TABLE LEG
Described herein is a table leg comprising a first connector for connecting the table leg in pivotable engagement with a seat such that the table leg is...
2017/0267353 DEPLOYABLE CLEARANCE PANEL SYSTEM, METHOD, AND ASSEMBLY FOR A MONUMENT WITHIN AN INTERNAL CABIN OF AN AIRCRAFT
A monument is configured to be positioned within an internal cabin of a vehicle. The monument includes a deployable portion. The deployable portion is...
2017/0267352 SEAT
Described herein is a seat which comprises a seat base, a seat back and a seat frame. The seat back comprises a first connector, a second connector and a...
2017/0267351 FASTENING SYSTEM FOR FASTENING AN OBJECT IN A VEHICLE
A fastening system for fastening an object in a vehicle, in particular in an aircraft comprises at least one rail which is arranged on the vehicle side, and an...
2017/0267350 PARTITION WALL MODULE FOR A CABIN OF A VEHICLE FOR AN OPTICAL AND MECHANICAL SEPARATION OF DIFFERENT CABIN REGIONS
A wall module for a cabin of a vehicle for separation of different cabin regions comprises a lower wall section having at least one first fastening means for...
2017/0267349 Reconfigurable Payload Systems (RPS) With Operational Load Envelopes For Aircraft And Methods Related Thereto
Reconfigurable payload systems (RPS) and methods of configuring and using the same with operational load envelopes are disclosed that may be employed to enable...
2017/0267348 PACKAGING CONTAINER FOR DRONE DELIVERY
Certain aspects of the technology disclosed involve a container for delivery by drone (e.g., an unmanned aerial vehicle). The container can include a coupling...
2017/0267347 PACKAGE DELIVERY MECHANISM IN AN UNMANNED AERIAL VEHICLE
Disclosed is a package delivery mechanism (PDM) of an unmanned aerial vehicle (UAV). The PDM includes a gravity activated locking mechanism to lock and unlock...
2017/0267346 RELEASE METHOD FOR INSECT DISTRIBUTION
A diffuser for distributing insects such as mosquitoes from an aircraft, comprises a distribution tube connected to an insect source at a first end and open to...
2017/0267345 HOVERING AERIAL VEHICLE AND METHOD OF FLYING SAME
A hovering aerial vehicle is provided, comprising an airborne unit and an auxiliary unit. The airborne unit is configured to carry the auxiliary unit during...
2017/0267344 METHOD FOR ENCAPSULATION AND RELEASE OF FRAGILE INSECTS
A method of distributing fragile insects in a distribution involving a wind shear, comprises, encapsulating the insects into a bubble and then releasing the...
2017/0267343 UNMANNED AERIAL VEHICLE OPERATION SYSTEMS
A method of deploying an unmanned aerial vehicle (UAV) operation system may be provided. A method may include estimating an amount of traffic for one or more...
2017/0267342 CROSS FLOW FAN WITH EXIT GUIDE VANES
A cross flow fan to be incorporated into an aircraft comprises a cross flow fan rotor to be positioned in an aircraft, a drive arrangement for the cross flow...
2017/0267341 DIRECTIONAL CONTROL SYSTEM AND METHOD OF PROVIDING DIRECTIONAL CONTROL
A directional control system for a rotorcraft having a tail boom including a no-tail-rotor apparatus configured to control rotorcraft yaw using forced air...
2017/0267340 DAMAGE TOLERANT AND FAIL-SAFE (DTFS) HIGH STRENGTH PRELOADED PIN ASSEMBLY
A hinge assembly such as a lead-lag hinge can include a hinge pin assembly. The hinge pin assembly can include an outer cylinder, a shear pin that extends...
2017/0267339 DAMAGE TOLERANT AND FAIL-SAFE (DTFS) HIGH STRENGTH PRELOADED PIN ASSEMBLY
A fracture-resistant double shear joint including a clevis having a first end defining a first bore and a second end defining a second bore, and a reaction...
2017/0267338 ACOUSTIC SIGNATURE VARIATION OF AIRCRAFT UTILIZING A CLUTCH
An aircraft is provided including an airframe, an extending tail, and a counter rotating coaxial main rotor assembly including an upper rotor assembly and a...
2017/0267337 ADAPTIVE PRESSURE SKID CONTROL
The present disclosure provides a skid control system that includes a brake control device configured to convert a current command value to create a braking...
2017/0267336 AIRCRAFT LANDING GEAR
Aircraft landing gear comprising an axle (100), a wheel (102) borne by the axle, a stack of discs (104) arranged to impose a braking torque on the wheel in...
2017/0267335 LOCKABLE WHEEL ACTUATOR DISENGAGEMENT SYSTEM ON AN AIRCRAFT LANDING GEAR
A landing gear (0) for an aircraft comprising a wheel (R), a system (1) for rotationally driving the wheel that is mobile between a clutched position and a...
2017/0267334 UNMANNED AERIAL VEHICLE AND LANDING METHOD THEREOF
An unmanned aerial vehicle (UAV) and a landing method thereof are provided. The landing method includes the following steps. Firstly, a depth image of a scene...
2017/0267333 AIRCRAFT WING ASSEMBLY
An airplane wing assembly includes a wing, a winglet and a connection element. The wing has a wing box. The wing box is located at a wing tip of the wing and...
2017/0267332 BOUNDARY-LAYER-INFLUENCING AERODYNAMIC PART AND METHOD FOR PRODUCING THE SAME
A boundary-layer-influencing aerodynamic part comprises a carrier element provided with at least one air passage aperture for guiding an air flow through the...
2017/0267331 METHOD AND APPARATUS FOR AUGMENTED PILOT OPERATIONS OF FLY-BY-WIRE VEHICLES
A system for augmented pilot operations is provided to perform checks and balances between navigable systems and a plurality of controlling parties of a...
2017/0267330 CUSTOMIZING AIRCRAFT PERFORMANCE SYSTEMS AND METHODS
Systems and methods are described for changing the performance of an aircraft by customizing aircraft control system parameters based on a subjective personal...
2017/0267329 HYDRAULIC ACTUATION CONTROL IN PROPELLERS
A propeller hydraulic actuation system, includes a double-acting dual chamber hydraulic pitch change actuator. The pitch change actuator includes a first...
2017/0267328 PROPELLER PITCH CHANGE ACTUATION SYSTEM
A yoke plate arrangement may comprise a yoke plate, a wear plate comprising a wear surface and a contact surface, wherein a post extends from the contact...
2017/0267327 CONNECTING MECHANISM BETWEEN AN AIRCRAFT DOOR AND A STRUCTURE OF THE AIRCRAFT, RELATED AIRCRAFT AND METHOD
A connecting mechanism between an aircraft door and a structure of the aircraft, a related aircraft and method are provided. The connecting mechanism includes...
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