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Patent # Description
2017/0275033 IDLER ROLLER
An inflatable-cushion inflation and sealing device is provided. The device includes an inflation assembly that inflates with a fluid a cushion cavity disposed...
2017/0275032 DEVICE AND METHOD FOR FILLING OPEN BAGS
Apparatus and method for filling bulk goods into empty open bags (3) comprising at least one weighing unit (7) and at least one filling station (11-18) and a...
2017/0275031 DEVICE AND METHOD FOR FEEDING AND DOSING FILTER BAGS WITH INFUSION OR EXTRACTION PRODUCTS
Described is a device for feeding and dosing infusion or extraction product of a machine (100) for making filter bags (S) containing the infusion or extraction...
2017/0275030 METHOD OF FEEDING ROD-SHAPED CONSUMER GOODS TO A PACKING APPARATUS
A method of feeding rod-shaped consumer goods to a packing apparatus is provided, including providing a plurality of rod-shaped consumer goods to an upstream...
2017/0275029 Method and Device for Automatic Packing of Wood
A method of preparing wood for packing comprises: loading wood lengthwise into a conveyor system; conveying the wood pieces one-by-one onto a loading hatch in...
2017/0275028 System, Apparatus and Methods for a Nosecone and a Propulsive Nozzle of an Airspace Plane
A system, apparatus and method for mitigating the shock front of a rocket or aerospace plane flying at hypersonic speeds while simultaneously distilling liquid...
2017/0275027 PROPELLER BALANCING USING INFLIGHT DATA
There is described herein a propeller balancing system and method that selects at least a portion of received propeller vibration data by comparing received...
2017/0275026 ROBOTS, ROBOTIC SYSTEMS, AND RELATED METHODS
Robots for moving relative to a surface, robotic systems including the same, and associated methods are disclosed. A robot includes a body, at least two legs,...
2017/0275025 LUMINAIRE-MOUNTED LANDING PLATFORM FOR A DRONE
There is provided a landing platform for mounting on a luminaire, where the landing platform provides an interface to a drone. For example, there is provided a...
2017/0275024 SYSTEM AND METHOD FOR DOCKING UNMANNED AERIAL VEHICLES (UAVS)
This document describes a system and method through which unmanned aerial vehicles (UAVs) can be docked, with a device that can secure the UAVs, and...
2017/0275023 COMBINING DEPTH AND THERMAL INFORMATION FOR OBJECT DETECTION AND AVOIDANCE
Described is an imaging component for use by an unmanned aerial vehicle ("UAV") for object detection. As described, the imaging component includes one or more...
2017/0275022 CRASH DEBRIS FIELD LOCATOR USING MINIATURE REDUNDANT TAGS
A system for locating a debris field resulting from a plane crash comprises a plurality of low-power, battery operated electronic transponder tags, and at...
2017/0275021 HYBRID HEADLIGHT FOR AIRCRAFT
This beam shaper for an aircraft headlight comprises a light input surface (3) and a light output surface (6), the output surface comprises prism-shaped areas...
2017/0275020 METHOD AND DEVICE FOR DISPLAYING A SYMBOLOGY FOR ASSISTING THE PILOTING OF AN AIRCRAFT DURING A LANDING PHASE
A method and device for displaying a symbology for assisting the piloting of an aircraft during a landing phase. The display device allows a crew to anticipate...
2017/0275019 FASTENER SYSTEMS THAT PROVIDE EME PROTECTION
Fasteners are inserted into a stack of members and terminated with parts having at least one of a dry dielectric coating and a dry dielectric seal at select...
2017/0275018 METHODS AND APPARATUS FOR PROVIDING CRITICAL ELECTRONIC CHECKLIST DATA DURING FLIGHT
A method for providing electronic checklist data onboard an aircraft is provided. The method detects, by an aircraft onboard system, a current phase of flight...
2017/0275017 ELECTRONIC CHECKLISTS WITH DYNAMIC VISIBILITY OF ANNOTATIONS
Display systems, controllers, and methods are provided. A display system for an aircraft includes a display unit, an input device, and a controller. The...
2017/0275016 APPARATUS TO STORE A DROGUE HOSE ON AN AIRCRAFT
Apparatus to store a drogue hose on an aircraft are disclosed herein. An example apparatus includes a drum to rotate in a first direction to coil a hose and a...
2017/0275015 APPARATUS TO STORE A DROGUE HOSE ON AN AIRCRAFT
Apparatus to store a drogue hose on an aircraft are disclosed herein. An example apparatus includes a pod to be attached to an aircraft to store a drogue hose,...
2017/0275014 ROTORCRAFT ROTOR AND PROPELLER SPEED
An aircraft includes an airframe having an extending tail, a counter rotating, coaxial main rotor assembly disposed at the airframe including an upper rotor...
2017/0275013 WINDMILL SYNCHRONIZATION IN AN ELECTRIC PROPULSION SYSTEM
A propulsion system is described that includes an electrical bus, a generator configured to provide electrical power to the electrical bus, a plurality of...
2017/0275012 THRUST RECOVERY OUTFLOW VALVES FOR USE WITH AIRCRAFT
Thrust recovery outflow valves for aircraft are disclosed. An example thrust recovery outflow valve includes a flow control member having a first aerodynamic...
2017/0275011 POWER MANAGEMENT BETWEEN A PROPULSOR AND A COAXIAL ROTOR OF A HELICOPTER
One aspect is a flight control system for a rotary wing aircraft that includes flight control computer configured to interface with a main rotor system, a...
2017/0275010 AUTOMATIC DEFLECTION LIMITING LATCHES FOR A THRUST REVERSER
A nacelle may include a pylon and a thrust reverser having an inner fixed structure. A locking mechanism may automatically engage and prevent relative movement...
2017/0275009 Hybrid Power System for an Aircraft
Systems and methods for distributing in an aircraft are provided. More particularly, in one embodiment, a system can include one or more gas turbine engines...
2017/0275008 TIME DELAY DEVICE FOR PARACHUTE DEPLOYMENT
Methods, devices, and systems for deploying cargo for high altitude, low opening (HALO) deployments are disclosed. The method comprises the steps of coupling a...
2017/0275007 PARACHUTE HARNESS CONTAINER WITH BIO-CONTOURED LOAD DISTRIBUTING VEST
A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and...
2017/0275006 BLADE HEATER MAT INSULATION
A heater mat assembly for a rotor blade spar is provided including a plurality of electrically conductive heater wires extending in a spaced parallel...
2017/0275005 ANTI-ICING SYSTEM OF AIRCRAFT, AIRCRAFT INCLUDING ANTI-ICING SYSTEM, PROGRAM FOR CONTROLLING ANTI-ICING SYSTEM,...
An anti-icing system at least includes: a precooler that exchanges heat between bleed air and outside air; and an anti-icing unit that receives the bleed air...
2017/0275004 AIRCRAFT AIR CONDITIONING SYSTEM WITH AN ELECTRICALLY DRIVEN AMBIENT AIR COMPRESSOR AND METHOD FOR OPERATING...
An aircraft air conditioning system comprising an ambient air supply line with a first end connected to an ambient air inlet and a second end connected to a...
2017/0275003 AIRCRAFT SEAT
A seat attachable to a floor of a vehicle includes a seat frame movable between a first position and a second position and a mounting assembly attached to the...
2017/0275002 SYSTEM FOR RECEIVING CARGO OR PASSENGERS IN A VEHICLE, AND A VEHICLE WITH SUCH A SYSTEM
An embodiment of the invention relates to a system for receiving cargo or passengers in a vehicle. The system includes a bottom beam and several functional...
2017/0275001 ADJUSTABLE LIE-FLAT SEAT
Described is a passenger seat that includes a seat bottom with a rear edge, the seat bottom including a bottom seating surface and a seat bottom adjustment...
2017/0275000 FOLDABLE SEAT BENCH
A foldable seat bench comprises a seat, a seat area and a backrest, and a carrier arrangement comprising a carrier element carrying the seat and at least one...
2017/0274999 EXPANDABLE SEAT LEG ATTACHMENT FIXTURE
Described is an extendable joint (10,100) for attaching a passenger seat to a cabin floor or support structure. The extendable joint (10,100) exhibits behavior...
2017/0274998 SEAT SUPPORT SYSTEM
Described is a passenger seat that includes a seat bottom assembly (201) with a forward edge and a rear edge and a seat back assembly (101) extending up from...
2017/0274997 ROTORCRAFT-ASSISTED SYSTEM AND METHOD FOR LAUNCHING AND RETRIEVING A FIXED-WING AIRCRAFT INTO AND FROM FREE FLIGHT
The present disclosure provides various embodiments of a rotorcraft-assisted launch and retrieval system including a rotorcraft having a fixed-wing aircraft...
2017/0274996 AIRCRAFT FOR VERTICAL TAKE-OFF AND LANDING
Embodiments of the present invention provide an aircraft for vertical take-off and landing. In various embodiments, an aircraft assembly includes at least one...
2017/0274995 FLYING MACHINE AND FLYING MACHINE USAGE METHOD
A flying machine includes: a flying machine body that includes a rotor blade; a protective member that forms a frame shape inside which the rotor blade is...
2017/0274994 DUAL ROTOR, ROTARY WING AIRCRAFT
An aircraft is provided including an airframe, an extending tail, a counter-rotating, coaxial main rotor assembly having an upper rotor assembly and a lower...
2017/0274993 AERIAL VEHICLE WITH DIFFERENT PROPELLER BLADE CONFIGURATIONS
Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation....
2017/0274992 ELECTROMAGNETIC DISTRIBUTED DIRECT DRIVE FOR AIRCRAFT
A fault tolerant, optically or electrically managed, EMP resilient electromagnetic distributed direct drive powertrain applied to provide lift and/or...
2017/0274991 SELECTIVELY THRUSTING PROPULSION UNITS FOR AERIAL VEHICLES
Aerial vehicles may include propulsion units having motors with drive shafts that may be aligned at a variety of orientations, propellers with variable pitch...
2017/0274990 ROTOR HOVER FIGURE OF MERIT FOR ROTARY WING AIRCRAFT
An aircraft composed of an airframe, an extending tail, a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor...
2017/0274989 AIRCRAFT WHEEL ASSEMBLY
An aircraft wheel assembly that includes first and second hub components having an axis and respective first and second sets of circumferentially spaced apart...
2017/0274987 SINGLE COLLECTIVE STICK FOR A ROTARY WING AIRCRAFT
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...
2017/0274986 METHOD AND APPARATUS FOR LATENT FAULT DETECTION AND MANAGEMENT FOR FLY-BY-WIRE FLIGHT CONTROL SYSTEMS
An aircraft control system includes pilot and co-pilot flight control systems that each include a first shaft mechanically coupled to and displaced apart from...
2017/0274985 PROACTIVE VEHICLE CONTROL SYSTEMS & METHODS
A vehicle may include a sensor and a proactive vehicle controller that is capable of proactively altering one or more vehicle operating parameters in response...
2017/0274984 COAXIALLY ALIGNED PROPELLERS OF AN AERIAL VEHICLE
This disclosure describes aerial vehicles and systems for altering the noise generated by the rotation of a propeller during flight of the aerial vehicle. In...
2017/0274983 AERIAL VEHICLE PROPULSION MECHANISM WITH COAXIALLY ALIGNED AND INDEPENDENTLY ROTATABLE PROPELLERS
Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation....
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