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Patent # Description
2018/0079542 FILM ROLL SUPPORTING DEVICE
A film roll supporting device comprises a shaft body part, a shaft tip part, and a projection part. The shaft body part extends through a central hole of a...
2018/0079541 PICK-UP DEVICE FOR PACKAGES
A pick-up device for picking up packages that may include a frame to which a first and a second retaining element are mounted. Each retaining element may...
2018/0079540 STORAGE CONTAINER FOR AUTOMATED DISPENSING OF INDIVIDUAL MEDICAMENT PORTIONS
Described herein are methods and systems for automated dispensing of individual medicament portions. The systems can include a housing that encloses a...
2018/0079539 METHOD FOR GAS FILLING OF A COMPARTMENT OF A FLEXIBLE CONTAINER
A method for handling containers (I) of collapsible type in a filling machine (20) comprising consecutively arranged stations (S1, S2, S3, S4, S5, S6)...
2018/0079538 EXTERNAL VACUUM SEALER
The present invention discloses an external vacuum sealer comprising a case, a heating adhesive strip, a heating band assembly and a lifting mechanism that all...
2018/0079537 Stretch Wrapping machine Supporting Top Layer Containment Operations
A method, apparatus and program product implement top layer containment operations to optimize containment of various types of loads such as loads with...
2018/0079536 FILLING APPARATUS
The invention relates to a filling apparatus for filling containers (12a-d) with liquid and/or pasty materials, in particular for a packing machine (14a; 14d),...
2018/0079535 CONTAINER SEALING DEVICE
An apparatus for filling a plurality of containers with a fluid. The apparatus including a connector configured to removably couple the apparatus to a fluid...
2018/0079534 ARTIFICIAL SATELLITE
Disclosed is an artificial satellite including a battery pack capable of dissipating heat, at least one radiator capable of conveying the heat dissipated by...
2018/0079533 AIRCRAFT ENGINE ILLUMINATION AND DIAGNOSTIC SYSTEM
An aircraft engine incorporates one or more externally-visible illuminators that are illuminated responsive to an activation signal. At least one of a...
2018/0079532 AUTOMATED STRUCTURAL INTERROGATION OF AIRCRAFT COMPONENTS
A structural health monitoring system and method includes a plurality of sensors configured to collect sensed data, a first structural component, and a...
2018/0079531 SYSTEM AND METHOD FOR DOCKING UNMANNED VEHICLES
This document describes a system and method through which unmanned aerial vehicles (UAVs) and other vehicles (e.g., unmanned underwater vehicles (UUVs), also...
2018/0079530 Automated Recovery System for Unmanned Aircraft
An unmanned aircraft system includes an automated recovery system that can recover aircraft in a reliable, economical manner, using a dual-pole and line...
2018/0079529 VIBRATION DAMPING GIMBAL SLEEVE FOR AN AERIAL VEHICLE
A gimbal sleeve for connecting to a camera gimbal may float between a floor surface and a ceiling surface of an aerial vehicle chassis such that the gimbal...
2018/0079528 Apparatuses and Methods for Reducing Ozone Creation from Ultraviolet (UV) Light
Apparatuses and methods are described for use of an ultraviolet (UV) light source, such as in a cleaning device, in which ozone creation due to reaction of the...
2018/0079527 STRUCTURE MANUFACTURING DEVICE AND STRUCTURE MANUFACTURING METHOD
Provided is a structure manufacturing device (100) including a constant-current power supply (10) that is configured to apply a current having a predetermined...
2018/0079526 METHOD FOR PLACING ELECTRICAL CONDUCTORS INTERIOR TO A COMPOSITE STRUCTURE PRIOR TO CURING
A method for placing electrical conductors interior to a composite structure prior to curing. A laminate stack is formed by assembling one or more composite...
2018/0079525 ELECTRICAL ISOLATION OF ANGLE OF ATTACK VANE BEARINGS
The bearings of aircraft angle of attack (AOA) vanes are susceptible to lightning strike damage, which causes fluting on the inner and outer races of the...
2018/0079524 DOWNED AIRCRAFT LOCATION SYSTEM AND METHOD
An EM emitter includes at least three orthogonal coils driven by an oscillating voltage source, with the coils being electrically in parallel or series. When...
2018/0079523 PROPELLER HEALTH MONITORING
A method for monitoring the health of propellers in an aircraft is provided. The method includes receiving pressure waves generated by at least one rotating...
2018/0079522 PROPELLER HEALTH MONITORING
A method for monitoring the health of propellers in an aircraft is provided. The method includes receiving a first propeller pitch angle of a first propeller...
2018/0079521 LIGHT DETECTION AND RANGING (LIDAR) ICE DETECTION
Method and system to detect ice accumulation on ice prone surfaces of an aircraft. The method and system sweeps a Light Detection and Ranging (LIDAR) beam...
2018/0079520 INCLEMENT WEATHER DETECTION FOR AIRCRAFT ENGINES
Methods and systems for detecting inclement weather in the vicinity of an aircraft engine are described. Vibration levels of the engine are monitored. Upon...
2018/0079519 Precision Operator for an Aircraft Autothrottle or Autopilot System
An autothrottle system for an aircraft includes a motor, actuator assembly, and position sensor operatively connected between the motor and a moving portion of...
2018/0079518 METHOD AND SYSTEM FOR RECYCLING MOTOR POWER OF A MOVABLE OBJECT
A method for recycling motor power includes controlling a first motor of an unmanned aerial vehicle (UAV) in a decelerating state to work in concert with a...
2018/0079517 LOCKING DEVICE FOR PIVOTING COWLS OF A THRUST REVERSER
The present disclosure provides a device for locking a first cowling and a second cowling of a thrust reverser of an aircraft propulsion assembly. The cowlings...
2018/0079516 POWER GENERATION AND DISTRIBUTION FOR VEHICLE PROPULSION
An aerial vehicle includes a hybrid power generation system comprising an engine; a generator mechanically coupled to the engine; and a propulsion system...
2018/0079515 AIRCRAFT PROPULSION SYSTEM
An aircraft propulsion system (10) comprises at least first and second electrical generators (15a, 15b), each being configured to provide electrical power to a...
2018/0079514 AIRCRAFT HAVING AN AFT ENGINE
An aircraft is provided including a fuselage that extends along a longitudinal direction between a forward end and an aft end. A boundary layer ingestion fan...
2018/0079513 INFLATABLE EVACUATION SYSTEM WITH CANOPY SUPPORT
An inflatable evacuation device for an aircraft may include at least one chamber and at least one canopy support in fluid communication with the at least one...
2018/0079512 FLUID ICE PROTECTION SYSTEM FLOW CONDUCTIVITY SENSOR
Method and system to sense ice protection fluid and verify a Fluid Ice Protection System (FIPS) is distributing the ice protection fluid correctly.
2018/0079511 TURBOFAN ENGINE FLUID ICE PROTECTION DELIVERY SYSTEM
Method and system to deliver anti-ice fluid to an ice prone surface using a pressurized tank pressurized with engine bleed air. The method and system further...
2018/0079510 CONTROL SYSTEM FOR A CABIN BLOWER SYSTEM
A control system for use in controlling a cabin blower system. The cabin blower system includes a gas turbine engine spool, a cabin blower compressor powered...
2018/0079509 AIRCRAFT SEATING ASSEMBLY
Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more...
2018/0079508 UNIVERSAL REST SEATS
A passenger seat assembly (150) includes a seat support (486) and an immobile seat shell (384) mounted on the seat support (486). The seat shell (384) can...
2018/0079507 PASSENGER SUPPLY UNIT FOR AN AIRCRAFT CABIN
A passenger supply unit for an aircraft cabin, including an input device for detecting a control command from a passenger, and for outputting a control signal...
2018/0079506 STORAGE COMPARTMENT AND LATCH THEREFOR
A latch assembly (1) is presented which comprises a safety latch (2) and a trigger latch (4). The safety latch (2) is releasable to raise from a lowered end...
2018/0079505 Oval Lifting-Body Airplane
An oval lifting-body airplane may generate lift without wings. It may be propelled by a pivoting propulsion engine attached to an upper surface, allowing it to...
2018/0079504 AIR VEHICLE FLIGHT MECHANISM AND CONTROL METHOD
Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of...
2018/0079503 ROTATING PROPROTOR ARRANGEMENT FOR A TILTROTOR AIRCRAFT
A propulsion system includes an engine disposed within a fuselage, a first gearbox coupled to the engine, a wing member having an upper wing skin and torque...
2018/0079502 Storage Modes for Tiltrotor Aircraft
A tiltrotor aircraft having a VTOL flight mode, a forward flight mode and a storage mode includes a fuselage having a wing rotatably mounted thereto. The wing...
2018/0079501 Storage Modes for Tiltrotor Aircraft
A tiltrotor aircraft having a VTOL flight mode, a forward flight mode and a storage mode includes a fuselage having a wing rotatably mounted thereto. The wing...
2018/0079500 Storage Modes for Tiltrotor Aircraft
A tiltrotor aircraft having a VTOL flight mode, a forward flight mode and a storage mode includes a fuselage having a wing rotatably mounted thereto. The wing...
2018/0079499 Storage Modes for Tiltrotor Aircraft
A tiltrotor aircraft having a VTOL flight mode, a forward flight mode and a storage mode includes a fuselage having a wing rotatably mounted thereto. The wing...
2018/0079498 CONNECTOR ASSEMBLY FOR ROTOR HEAD SWASHPLATE
A connector assembly to connect a swashplate and a rotor shaft or hub is provided. The connector assembly includes a mount configured to fixedly connect to the...
2018/0079496 LANDING GEAR ARRANGEMENT WITH PASSIVE SHOCK STRUT SHRINK ACTUATOR
A landing gear arrangement may comprise a shock strut, a retraction actuator, and a shrink actuator. The retraction actuator may move the shock strut between a...
2018/0079495 SYSTEMS AND METHODS FOR FORECASTING AND REDUCING THE OCCURRENCE OF TIRE OVERSPEED EVENTS DURING AIRCRAFT...
Avionic systems and methods are provided for forecasting and reducing the likelihood of tire overspeed events during aircraft (A/C) runway procedures, such as...
2018/0079494 AIRCRAFT LANDING GEAR, AIRCRAFT, AND RELATED METHODS
An aircraft landing gear structure includes a strut assembly configured to transition between a compressed configuration, an extended configuration, and a...
2018/0079493 Wing Extension Winglets for Tiltrotor Aircraft
A pylon assembly for a tiltrotor aircraft includes a rotor assembly operable to rotate between a generally vertical orientation, in a VTOL flight mode, and a...
2018/0079492 Flow control device, flow profile body and flow influencing method with acoustic wave generation
For adaptively influencing a flow with little intrusion into the surface, a flow control device is provided to influence the flow of a fluid medium on a...
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