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Patent # Description
2016/0311555 Suspension of a Tubular Element in an Aircraft Compartment
The invention relates to an assembly comprising a structure (2) and a tubular element (6), which is mounted isostatically in the structure (2), said tubular...
2016/0311554 CONTACT DETECTING SYSTEM AND METHOD FOR AIR REFUELING TANKER EQUIPPED WITH AIR REFUELING BOOM SYSTEM
A contact detecting system for an air refueling tanker equipped with an air refueling boom, the system comprising a boom refueling nozzle comprising a valve to...
2016/0311553 TAIL SITTER VEHICLE WITH AERIAL AND GROUND REFUELING SYSTEM
An aircraft is provided and includes a fuselage, first and second wings extending outwardly from opposite sides of the fuselage, proprotors operably disposed...
2016/0311552 ELECTRICALLY HEATED FILTER SCREENS
A heating body for an electrically heated filter screen includes a heater element having an outer surface and a metallic protective layer having an inner...
2016/0311551 ENGINE PROXIMATE NITROGEN GENERATION SYSTEM FOR AN AIRCRAFT
A nitrogen generation system includes a bleed air source. The system also includes an air separation module having an inlet for receiving bleed air, a hollow...
2016/0311550 AIRCRAFT VEHICLE THERMAL MANAGEMENT SYSTEM AND METHOD
An air vehicle power and thermal management system includes an aircraft controller structured to distribute power provided by a gas turbine engine between a...
2016/0311549 Exhaust Arrangement for Aircraft Having Sensor
An exhaust arrangement is for an aircraft having sensing equipment and a front prop engine. An extension mounts on the underside along an edge of the fuselage...
2016/0311548 METHOD FOR AUTOMATICALLY CONTROLLING THE OPERATING SPEED OF A HELICOPTER TURBOSHAFT ENGINE, CORRESPONDING...
The invention relates to a method for automatically controlling an operating mode of a turboshaft engine of a helicopter, comprising a step (10) of receiving...
2016/0311547 METHOD AND A DEVICE FOR STOPPING A TURBOSHAFT ENGINE IN NOMINAL OPERATION
A method of stopping a turboshaft engine in flight. During a power reduction step, a current power of the engine for stopping is reduced to reach zero power,...
2016/0311546 METHOD, SYSTEM, AND APPARATUS FOR REDUCING A TURBINE CLEARANCE
A method for reducing a turbine clearance gap between a plurality of rotor blades of a turbine engine and a shroud of the turbine engine is provided. The...
2016/0311545 Solar-Powered Aircraft
The present invention is directed to a solar-powered aircraft comprising a fixed wing panel, a motor driven propeller, a plurality of secondary wing panels,...
2016/0311544 Micro Hybrid Generator System Drone
An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator...
2016/0311543 SOFT COVER RELEASE MECHANISM FOR EVACUATION SLIDES
An emergency evacuation assembly may comprise an inflatable slide, a soft cover containing the inflatable slide, a lace holding the soft cover closed, a pin...
2016/0311542 WEEPING FERROFLUID ANTI-ICE SYSTEM
Method, system, and aircraft for providing anti-ice protection comprising a supply of ferrofluid that is flowed out of orifices along a first region of an...
2016/0311541 DUCT STRUCTURE WHICH DISCHARGES AIR THROUGH AIR PRESSURE REGULATING VALVE AND AIRCRAFT
An aircraft duct structure includes a first duct through which exhaust air from a front-side equipment compartment flows, and a second duct through which...
2016/0311540 MODULAR ENVIRONMENTAL AIR CONDITIONING SYSTEM
An Environmental Control System (ECS) is disclosed for providing conditioned air to a conditioned air space. The ECS includes one or more first modules, each...
2016/0311539 ENVIRONMENTAL CONTROL SYSTEM MIXING CABIN DISCHARGE AIR WITH BLEED AIR DURING A CYCLE
A system and method that comprises an air cycle machine, a flow of bleed air, at least one heat exchanger, and an inlet configured to supply the flow of the...
2016/0311538 ENVIRONMENTAL CONTROL SYSTEM UTILIZING CABIN DISCHARGE AIR TO POWER A CYCLE
A system and method that comprises an air cycle machine, a flow of bleed air, at least one heat exchanger, and an inlet configured to supply the flow of the...
2016/0311537 REDUCED PROFILE LEGREST FOR A SEAT
A reduced profile legrest system has a legrest frame having at least two opposing edges, a width, and a centerline being a point that is half of the width....
2016/0311536 POSTURE SEAT
Dynamic support systems (10) include a plurality of support members (12), a base material (14), and a support layer (18). Each support member (12) has an upper...
2016/0311535 METHOD OF DETERMINING A SEATING ARRANGEMENT
A method of determining a seating arrangement for an aircraft cabin includes entering configuration parameters into a processor including a cabin width, a...
2016/0311534 AIRCRAFT GALLEY UNIT
An aircraft galley unit includes a housing defining an outer shell, and a rack area and a double deck area arranged within the housing, wherein the double deck...
2016/0311533 FLIGHT SUITS
There are provided flight suits that can be useful for helicopter pilots, airplane pilots, glider pilots etc. Pilots of such vessels have particular needs in...
2016/0311532 Methods And Systems For Providing Aerial Assistance
Embodiments described herein may relate to systems and methods for navigating to a supply request. An alert device may be controlled to issue alerts to draw...
2016/0311531 High Altitude, Long Endurance, Unmanned Aircraft and Methods of Operation Thereof
Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft capable of persistent station-keeping having one or more electromagnetic...
2016/0311530 Aircraft With A Plurality Of Engines Driving A Common Driveshaft
An aircraft may have a fuselage, a left wing extending from the fuselage, a right wing extending from the fuselage, a tail section extending from a rear...
2016/0311529 Modular Electric VTOL Aircraft
A VTOL aircraft is disclosed comprising a plurality of autonomous lifting modules wherein each autonomous lifting module is composed of a physical structure in...
2016/0311528 Multi-rotor Vehicle with Yaw Control and Autorotation
An improved vehicle with superior performance and reliability. The vehicle, such as an unmanned aerial vehicle, is capable of vertical takeoff and landing,...
2016/0311527 METHOD FOR THE DELIVERY OF LUBRICANT TO A ROTORCRAFT GEARBOX
According to one embodiment, a rotorcraft includes a body, a rotor blade, and a power train coupled to the body and operable to rotate the rotor blade. The...
2016/0311526 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...
2016/0311525 AIRCRAFT LANDING GEAR
An aircraft landing gear comprising: a shock-absorbing main leg having a sprung part for attachment to an aircraft and an un-sprung part including a slider and...
2016/0311524 Flow Disruption Devices for the Reduction of High Lift System Noise
Various embodiments provide systems and methods for noise reduction for lift-augmentation wing-sections (e.g., flaps, slats, elevons, etc.) by the use of flow...
2016/0311523 PUSHING DEVICE, MOVING MECHANISM AND AIRCRAFT
The present application relates to a pushing device, a moving mechanism and an aircraft. According to an aspect of the present application, a pushing device...
2016/0311522 Aerofoil for an aircraft, and an aircraft
An aerofoil for an aircraft includes an engine, a first lift body, and a second lift body which is arranged behind the first lift body in the direction of flow...
2016/0311521 SYSTEMS, METHODS, AND APPARATUSES FOR AIRFOIL CONFIGURATION IN AIRCRAFT
The present set of embodiments relate to systems, methods, and apparatuses for airfoil systems designed for aircraft or other craft. More specifically, the...
2016/0311520 OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGESTION ACTIVE LAMINAR FLOW CONTROL
Aspects of the disclosure are directed to a nacelle of an aircraft, comprising a surface that is profiled such that during cruise flight operation lines of...
2016/0311519 WIND TURBINE DOME AND METHOD OF ASSEMBLY
An aerodynamic dome component that is placed in front of a wind turbine hub includes an outer ring, a central axle disposed relative to the outer ring, a...
2016/0311518 WING STRUCTURE UTILIZING CARBON FIBER SPAR AND SHAPED FOAM
An aircraft wing includes a body including plural composite spars, with plural foam ribs positioned adjacent the spars.
2016/0311517 AIRCRAFT ADAPTED FOR TRANSPORTING CARGO
The fuselage of an aircraft comprises a floor structure, a roof structure, a first lateral side structure, a second lateral side structure, and a middle...
2016/0311516 SPLIT LEVEL FORWARD DOUBLE DECK AIRLINER
An aircraft includes a fuselage, having a crown section and a keel, a first passenger cabin, having a first floor, located in an aft portion the fuselage, and...
2016/0311515 METHOD FOR ASSEMBLING AN AIRCRAFT AFT PORTION
In the case of an aircraft aft portion equipped with an engine mounting structure passing across the fuselage, assembly of the aft portion presents problems...
2016/0311514 LIGHTWEIGHT STRUCTURAL PANEL
What is described is a lightweight structural panel which comprises a planarly extended outer skin of given thickness and stiffening elements which are...
2016/0311513 ACOUSTIC CABIN PANEL
The present invention relates to acoustical panels. As to provide a cabin panel to be made as simple as possible and with optimized acoustical properties, an...
2016/0311512 AIRCRAFT FRAME FOR TAILSTRIKE ANGLE ENHANCEMENT
A wedge frame for an aircraft that provides tailstrike angle enhancement. The wedge frame has converging, non-parallel faceplanes that tilt a rear portion of...
2016/0311511 Autopilot Navigation
Various implementations described herein are directed to a non-transitory computer-readable medium having stored thereon a plurality of computer-executable...
2016/0311510 VESSEL DISPLAY DEVICE AND VESSEL INFORMATION DISPLAY METHOD
A vessel display device displays information on a vessel. The vessel display device includes an information acquirer that acquires the same type of information...
2016/0311509 VESSEL CARGO MONITORING SYSTEM
A system for assessing vessel stability includes a weight sensor, a data storage device, a locator, and a display device. The system provides real-time weight...
2016/0311508 Floatation Support Device
A floatation support device supports a person in a seated or prone position in a body of water. The device includes a pair of frames each having an elbow...
2016/0311507 PERSONAL FLOTATION APPARATUS
A personal flotation apparatus having a main body member, a primary support member, a head support member, and a foot support member, each made of flexible,...
2016/0311506 TEMPORARY POST BRACE FOR WATER ACTIVITIES
A post brace that is used to temporarily support solar lights on a boat made of a water resistant shell and filled with beads is disclosed herein. The post...
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