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Patent # Description
2016/0280406 VACUUM PACKAGING ARRANGEMENT, KITCHEN CABINET AND KITCHEN FURNITURE
The present application in particular is related to a vacuum packaging arrangement. The vacuum packaging arrangement (2) comprises a drawer (4) configured to...
2016/0280405 PORTABLE CABLE TIE TOOL
A portable tool for tying an object, in particular a cable harness, using a strip, comprising a tool element with a cycle controller arranged in the tool...
2016/0280404 WRAPPING MATERIALS FOR SOLID OBJECTS
Improved object wrapping materials exhibiting a number of beneficial properties to overcome prior deficiencies are provided. Such properties include the...
2016/0280403 3-D Printed Packaging
Items may be packaged for shipping or storage using additive manufacturing techniques, also known as three dimensional (3-D) printing. Packages made by such...
2016/0280402 SYSTEM AND APPARATUS FOR FEEDING, SOLUBILIZING, GROWING AND DISCHARGING A BIOLOGICAL MATERIAL
Apparatus useful for feeding a particulate starter material comprising nutrient and bacteria to a mixing tank, for solubilizing the starter material inside the...
2016/0280401 SYSTEMS, METHODS AND DEVICES FOR SATELLITE NAVIGATION
A three-dimensional map of an environment with buildings is used to computationally predict locations and times of global navigation satellite system (GNSS)...
2016/0280400 Spacecraft Landing and Recovery Inflation System
A landing inflation system may include a compressed gas source, an airbag assembly fluidly coupled to the compressed gas source and configured to receive...
2016/0280399 ROCKET ENGINE RECOVERY SYSTEM
This recovery system is used mainly for the recovery of liquid propellant rocket engines, so that they can be reused once or more times, in first stages...
2016/0280398 Ergonomic Device for Suspending Aircraft Flight Control Apparatuses
In one embodiment, a device includes a spine, a first support coupled to a first end of the spine, a second support coupled to a second end of the spine, and a...
2016/0280397 METHOD AND SYSTEM TO AVOID PLANT SHADOWS FOR VEGETATION AND SOIL IMAGING
A method, a computer program product, and a system is disclosed of obtaining aerial images from an aerial vehicle to avoid shadows produced by the sun, the...
2016/0280396 EXTERIOR AIRCRAFT NAVIGATION LIGHT AND METHOD OF CONTROLLING AN EXTERIOR AIRCRAFT NAVIGATION LIGHT
An exterior aircraft navigation light for an aircraft having a nominal forward flight direction and being able to fly into the nominal forward flight direction...
2016/0280395 AT LEAST PARTIALLY TRANSPARENT EXTERIOR AIRCRAFT LIGHT COVER AND EXTERIOR AIRCRAFT LIGHTING DEVICE COMPRISING...
An at least partially transparent exterior aircraft light cover includes at least one protrusion provided at a lateral end of the exterior aircraft light...
2016/0280394 POWER DISTRIBUTION SYSTEM FOR AN AIRCRAFT
An aircraft power distribution system (22) includes at least one DC power source, a first DC power distribution bus and a second DC power distribution bus...
2016/0280393 METHOD AND A DEVICE FOR MARKING THE GROUND FOR AN AIRCRAFT IN FLIGHT, AND AN AIRCRAFT INCLUDING THE DEVICE
A method of marking a landing zone on ground for an aircraft in flight. The aircraft projects on the ground a light shape referred to as a "projected light...
2016/0280392 WINGTIP CONTROL SYSTEM
A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller....
2016/0280391 AIR DATA PROBES
An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. The probe includes a thermocouple having a sense end...
2016/0280390 ARRANGEMENT FOR PASSING A LINE IN A LOAD-FREE MANNER THROUGH A PRESSURE FRAME OF A FUSELAGE OF AN AIRCRAFT OR...
The present invention provides an arrangement for passing a line in a load-free manner through a pressure frame of a fuselage of an aircraft or spacecraft,...
2016/0280389 HEAT EXCHANGER FOR AIRCRAFTS
This aircraft heat exchanger includes a heat exchanger body, which includes: a temperature raising section configured at least to raise a temperature of the...
2016/0280388 INTAKE STRUCTURE OF AIRCRAFT
In an intake structure of an aircraft that takes in air from a front side of an airframe, a bump is provided on a surface of the airframe of the aircraft at a...
2016/0280387 AIRCRAFT THERMAL MANAGEMENT SYSTEM
An aircraft thermal management system includes a first fluid system containing a first fluid, a fluid loop containing a thermally neutral heat transfer fluid,...
2016/0280386 FLIGHT CONTROLLER WITH GENERATOR CONTROL
A flight controller system includes an electronic speed control throttle input from which an anticipated electrical power demand is determined. The flight...
2016/0280385 CONTROL SCHEME USING VARIABLE AREA TURBINE AND EXHAUST NOZZLE TO REDUCE DRAG
A method to reduce aerodynamic drag of a engine exhaust/engine nozzle includes collecting data that is indicative of an instant flight condition, entering the...
2016/0280384 HIGH VISIBILITY LATCH HANDLE
A latch handle is disclosed. The latch handle may comprise a first portion and a second portion. The first portion may comprise a high aspect ratio. The second...
2016/0280383 FAN COWL BALKING LATCH
A nacelle may include fan cowl panels which may be opened to provide access to the fan case. A latching mechanism may latch a left fan cowl panel to a right...
2016/0280382 FAN COWL LATCH
A nacelle may include fan cowl panels which may be opened to provide access to the fan case. A latching mechanism may latch a left fan cowl panel to a right...
2016/0280381 TURBOPROP ENGINE ATTACHMENT SYSTEMS AND METHODS
An engine attachment system (EAS) includes a forward collar (202), an aft collar (204), at least one truss subassembly (216) disposed between the forward...
2016/0280380 Parachute System Mounted to Payload
A balloon system is provided including a balloon envelope, a payload secured to the balloon envelope, a first parachute positioned within a parachute...
2016/0280379 METHOD AND APPARATUS FOR INHIBITING FORMATION OF AND/OR REMOVING ICE FROM AIRCRAFT COMPONENTS
Methods and systems are generally described that inhibit debris (such as ice) accretions and/or remove debris (such as ice) accretions from the exterior...
2016/0280378 PASSENGER SEAT
Described are seat units having a lower support structure with at least two leg supports, each leg support integrally formed into an arcuate shape, and an...
2016/0280377 STOWABLE RECLINING SEAT WITH LATERAL TRANSLATION LINKAGE
A stowable seat is provided. The stowable seat may comprise a housing, a back rest coupled to the housing at a top of the back rest, and a seat bottom coupled...
2016/0280376 SEAT BACK PERSONAL ELECTRONIC DEVICE HOLDER
A personal electronic device holder for a seat back that includes a support housing positioned on an upper shroud portion of the seat back and an upper support...
2016/0280375 PERSONAL ELECTRONIC DEVICE MOUNTING ASSEMBLIES
Described herein are personal electronics device mounting assemblies including a passenger seat and a case assembly comprising a case configured to receive a...
2016/0280374 MOBILE PASSENGER ENTERTAINMENT AND INFORMATION SYSTEM
A mobile passenger entertainment and information system that includes a control device, a plurality of passenger devices, a satellite communication device, a...
2016/0280373 INTERIOR AIRCRAFT LED LIGHT UNIT AND METHOD OF CALIBRATING AN INTERIOR AIRCRAFT LED LIGHT UNIT
An interior aircraft LED light unit includes at least one LED and a lens cover arranged over the at least one LED, the lens cover having a proximal side facing...
2016/0280372 CRANED AIR TRANSPORTER
A multi-purpose craned air transporter (CAT) that is structurally configured to manage liabilities, and to expedite independent functions for hauling and...
2016/0280371 UNMANNED VEHICLE ROLLBACK
An unmanned vehicle determines how to perform a task based at least in part on a message received from another unmanned vehicle. At a later time, the unmanned...
2016/0280370 INFLUENCING ACCEPTANCE OF MESSAGES IN UNMANNED VEHICLES
An unmanned vehicle receives a message from another unmanned vehicle. The recipient unmanned vehicle uses information included with the message to determine...
2016/0280369 ROTORCRAFT
A rotorcraft having a body and a propulsion system wherein the propulsion system includes a main thrust rotor and multiple control rotors, wherein the main...
2016/0280368 LAYER MATERIAL FOR ARRANGING ON A ROTOR BLADE TIP OF A HELICOPTER, HELICOPTER LIGHT SYSTEM, AND HELICOPTER...
In an embodiment, a layer material configured to be arranged on a rotor blade tip of a helicopter comprises at least one light emitting or reflecting section...
2016/0280367 COMPOSITE YOKE FITTING FOR BEARING ATTACHMENT TO ROTORCRAFT BLADE
A rotor blade assembly includes a rotor blade comprising an inboard end and an outboard end. A composite yoke fitting made from a composite material is...
2016/0280366 FLAPPING ABUTMENT MECHANISM FOR A LIFT ASSEMBLY, A ROTORCRAFT ROTOR INCLUDING THE ABUTMENT MECHANISM, AND A...
An abutment mechanism for a lift assembly of an aircraft. The abutment mechanism comprises a single rigid link having variable travel, the link comprising a...
2016/0280365 CABLE CUTTER ANTENNA FOR AIRCRAFT
A cable cutter (10) for an aircraft (27) comprises an electrically-conducting body (12) configured to be mounted on an aircraft (27) and to cut a cable and an...
2016/0280364 EMERGENCY STOP FOR BLADES OF DRONE
Disclosed is a drone having at least one rotor. The at least one rotor comprises a mast and at least two blades having a proximal end and a distal end. The at...
2016/0280363 ACTIVE VIBRATION ISOLATION WITH DIRECT FLUID ACTUATION
A method of isolating vibrations between vibrating bodies includes determining a pressure differential between a first fluid chamber and a second fluid chamber...
2016/0280362 AIRCRAFT AND LANDING GEAR PROVIDED WITH AT LEAST ONE PAIR OF SHOCK ABSORBERS, AND A METHOD PERFORMED BY SAID...
Landing gear for an aircraft, the landing gear having at least one pair of shock absorbers comprising a first shock absorber and a second shock absorber, each...
2016/0280361 RETRACTABLE LANDING GEAR
The present disclosure describes systems and methods for retractable landing gear. A landing gear arrangement may comprise: a trailing arm; a shock strut; a...
2016/0280360 AIRCRAFT LANDING GEAR
The invention relates to an aircraft landing gear, particularly a front landing gear with at least one EHDC unit, which has at least one electric motor and at...
2016/0280359 PERCHING ATTACHMENT FOR UNMANNED AIRCRAFT
An aerial vehicle system includes a flight system configured to generate propulsive force and lift, a protective framework, and an attachment mechanism secured...
2016/0280358 Hybrid Flow Control Method for Simple Hinged Flap High-Lift System
Systems, methods, and devices are provided that provide hybrid flow control for a simple hinged flap high-lift system using sweeping jet (SWJ) actuators for...
2016/0280357 RHEOLOGIC FLUID COUPLER FOR REDUNDANT LINEAR ELECTROMECHANICAL ACTUATORS
An actuation assembly includes a first shaft comprising a first end disposed opposite a second end. The actuation assembly further includes a second shaft with...
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