23rd week of 2018 patent applcation highlights part 20 |
Patent application number | Title | Published |
20180154997 | LARGE OUTBOARD MOTOR FOR MARINE VESSEL APPLICATION AND RELATED METHODS OF MAKING AND OPERATING SAME - An outboard motor for a marine vessel application, and related methods of making and operating same, are disclosed herein. In at least one embodiment, the outboard motor includes a horizontal-crankshaft engine in an upper portion of the outboard motor, positioned substantially positioned above a trimming axis of the outboard motor. In at least another embodiment, first, second and third transmission devices are employed to transmit rotational power from the engine to one or more propellers at a lower portion of the outboard motor. In at least a further embodiment, the outboard motor is made to include a rigid interior assembly formed by the engine, multiple transmission devices, and a further structural component. In further embodiments, the outboard motor includes numerous cooling, exhaust, and/or oil system components, as well as other transmission features. | 2018-06-07 |
20180154998 | ADJUSTABLE JACK PLATE AND TRIM AND TILT SYSTEM FOR A MARINE VESSEL - An apparatus for adjusting positions of an outboard propulsion unit of a marine vessel comprises a jack plate having a jack plate actuator capable of moving the propulsion unit between raised and lowered positions and a swivel bracket having a swivel bracket actuator capable of pivoting the propulsion unit between raised and lowered trim positions. There is a control system operatively connected to the jack plate actuator and the swivel bracket actuator. The control system includes a first manual control which incrementally moves the jack plate an incremental amount each time the first manual control is actuated and a second manual control which incrementally pivots the swivel bracket an incremental amount each time the second manual control is actuated. Movement of the propulsion unit within a tilt range may be detected and the jack plate may be moved to a preset position. | 2018-06-07 |
20180154999 | Outboard Motor and Methods of Use Thereof - An outboard motor and methods of use thereof in general, includes a powerhead removeably affixed to the transom of a boat, and a gear case rotationally connected to a propeller shaft, the outboard motor including a telescopic drive shaft, the telescopic drive shaft having a first drive shaft section rotationally connected to the motor and a second drive shaft section rotationally connected to the gear case, and a telescopic drive shaft housing, the telescopic drive shaft housing configured to support the telescopic drive shaft internally therethrough, whereby the telescopic drive shaft and the telescopic drive shaft housing are configured to provide depth adjustment for the gear case and the propeller shaft, and thus enable the propeller to be raised and lowered during propulsion to improve propulsion efficiency. | 2018-06-07 |
20180155000 | FUEL CELL WATERCRAFT - A fuel cell watercraft ( | 2018-06-07 |
20180155001 | LENTICULAR AIRSHIP AND ASSOCIATED CONTROLS - A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle. | 2018-06-07 |
20180155002 | Elongated Structures and Related Assemblies - An elongated structure comprising a web extending along a length of the elongated structure and a flange comprising a first flange portion, the first flange portion extending away from an area of the web. The first flange portion comprises a variable width along at least a portion of the length of the elongated structure. The first flange portion of the elongated structure may comprise the variable width the length of the elongate structure. The first flange portion may comprise a constant width along at least a portion of the length of the elongated structure. The elongated structure may further comprise a second flange portion. The second flange portion may comprise a variable width along at least a portion of the length of the elongate structure. The first flange portion may comprise a first top flange portion. | 2018-06-07 |
20180155003 | Adjustable Hinge - A hinge has a door interface comprising a serrated surface and an oversized hole, a bolt at least partially extending into the oversized hole, and a washer disposed on the bolt and captured between the door interface and a head of the bolt, the washer comprising a serrated surface facing toward the serrated surface of the door interface. The oversized hole has a diameter selected to allow significant radial movement of the bolt within the oversized hole. | 2018-06-07 |
20180155004 | AEROFOIL STRUCTURE COMPONENTS - A component for an aerofoil structure including a unitary member having a spar; a cover panel; and a substantially flat intermediate section which connects the spar to the cover panel. The spar, the cover panel and the intermediate section are integrally formed such that a first angle between the intermediate section and the cover panel and a second angle between the intermediate section and the spar are both in the range 90° to 180°. | 2018-06-07 |
20180155005 | Active Dihedral Control System for a Torsionally Flexible Wing - A span-loaded, highly flexible flying wing, having horizontal control surfaces mounted aft of the wing on extended beams to form local pitch-control devices. Each of five spanwise wing segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other wing segments, to minimize inter-segment loads. Wing dihedral is controlled by separately controlling the local pitch-control devices consisting of a control surface on a boom, such that inboard and outboard wing segment pitch changes relative to each other, and thus relative inboard and outboard lift is varied. | 2018-06-07 |
20180155006 | AIRCRAFT STABILIZER LEADING EDGE INTEGRATION WITH TORSION BOX AND FUSELAGE - An aircraft stabilizer ( | 2018-06-07 |
20180155007 | FLAP AND AIRCRAFT - A flap of an aircraft includes a flap body that is provided deployably with respect to a main wing, an inclined portion that protrudes from an upper surface of a tip part on at least an outboard side in a span direction of the flap body and is inclined with respect to an aircraft axis direction, and a protruding portion that smoothly protrudes from a lower surface of the tip part on at least the outboard side. A rear end of the inclined portion is located closer to a side end edge of the tip part in the span direction of the flap body than a virtual line that passes through a front end of the inclined portion and is parallel to the aircraft axis direction. | 2018-06-07 |
20180155008 | DEVICE FOR MANAGING THE MECHANICAL ENERGY OF AN AIRCRAFT, HAVING A LIGHT SYSTEM, RELATED AIRCRAFT AND PROCESS - A device for managing the mechanical energy of an aircraft, having a light system, includes a support defining a guide; at least one control lever for varying the mechanical energy of the aircraft, mounted moving through the guide; and at least one position sensor detecting the position of the control lever in the guide, configured to create position information for the position of the control lever in the guide intended to be sent to a flight control unit of the aircraft. The device also includes at least one light strip extending on the support along at least part of the travel of the control lever in the guide; and a control unit of the at least one light strip, configured to display at least one light indication at least at one given point of the lighted position ramp calculated as a function of a movement context of the aircraft. | 2018-06-07 |
20180155009 | CONTROLLED FLIGHT OF A MULTICOPTER EXPERIENCING A FAILURE AFFECTING AN EFFECTOR - According to a first aspect of the invention, there is provided a method for operating a multicopter experiencing a failure during flight, the multicopter comprising a body, and at least four effectors attached to the body, each operable to produce both a torque and a thrust force which can cause the multicopter to fly when not experiencing said failure. The method may comprise the step of identifying a failure wherein the failure affects the torque and/or thrust force produced by an effector, and in response to identifying a failure carrying out the following steps, (1) computing an estimate of the orientation of a primary axis of said body with respect to a predefined reference frame, wherein said primary axis is an axis about which said multicopter rotates when flying, (2) computing an estimate of the angular velocity of said multicopter, (3) controlling one or more of said at least four effectors based on said estimate of the orientation of the primary axis of said body with respect to said predefined reference frame and said estimate of the angular velocity of the multicopter. The step of controlling one or more of said at least four effectors may be performed such that (a) said one or more effectors collectively produce a torque along said primary axis and a torque perpendicular to said primary axis, wherein (i) the torque along said primary axis causes said multicopter to rotate about said primary axis, and (ii) the torque perpendicular to said primary axis causes said multicopter to move such that the orientation of said primary axis converges to a target orientation with respect to said predefined reference frame, and (b) such that said one or more effectors individually produce a thrust force along said primary axis. | 2018-06-07 |
20180155010 | CONTROL SYSTEM FOR AN ACTUATOR - There is provided an actuator comprising an output shaft and a control system configured to move the output shaft for actuating a component. The control system comprises a first drive system comprising a first movable component, and a second drive system comprising a second movable component. The first component and the second component are connected to the output shaft, and each other, by a connecting member that moves with the first component and the second component to move the output shaft for actuating a component. The control system further comprises one or more bearing arrangements configured to permit movement of the connecting member by the first movable component or the second movable component upon failure, disengagement, shutdown or other stoppage of the second drive system or the first drive system, respectively. | 2018-06-07 |
20180155011 | ADAPTIVE THRUST VECTOR UNMANNED AERIAL VEHICLE - A method for unmanned delivery of an item to a desired delivery location includes receiving, at an unmanned vehicle, first data representative of an approximate geographic location of the desired delivery location, receiving, at the unmanned vehicle, second data representative of a fiducial expected to be detectable at the desired delivery location, using the first data to operate the unmanned vehicle to travel to the approximate geographic location of the desired delivery location, upon arriving at the approximate geographic location of the desired delivery location, using the second data to operate the unmanned vehicle to detect the fiducial; and upon detecting the fiducial, using the fiducial to operate the unmanned vehicle to deliver the item. | 2018-06-07 |
20180155012 | METHOD FOR PRODUCING A SMOOTH AERODYNAMIC SURFACE OF AN AIRCRAFT COMPONENT - A method for producing a smooth aerodynamic surface of an aircraft component is depicted and described. The method includes: provision of an aircraft component with an aerodynamic surface, which has an uneven section, introduction of a liquid or viscous, uncured sealing compound into the uneven section, introduction of a solid, precured sealing body into the uneven section in such a way that the sealing body presses into the sealing compound until the sealing compound at least partially surrounds the sealing body, curing of the sealing compound. | 2018-06-07 |
20180155013 | AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT - An aircraft airflow modification device, comprising: at least one resiliently deformable base member; and at least one resiliently deformable flap member that extends from the resiliently deformable base member. Deformation of the resiliently deformable base member from a first state to a second state results in corresponding deformation of the resiliently deformable flap member from a first state to a second state. | 2018-06-07 |
20180155014 | ELECTRICALLY CONTROLLED PARK AND EMERGENCY VALVE ASSEMBLY - An electrically controlled park and emergency brake system is disclosed. The brake system may comprise a brake control module having a shut-off valve in fluid communication with an outboard servo-valve and an inboard servo-valve. An emergency/park power source may supply fluid to the shut-off valve. The brake system may also comprise a vehicle management system in electronic communication with the brake control module. The brake system may also comprise mechanical inputs, including a wheel well brake handle and a cockpit brake handle. The brake system may also comprise redundant emergency/park power sources. | 2018-06-07 |
20180155015 | Automatic, Active Blade Tracking and Balance System - The present invention includes an apparatus and method for automatically adjusting the tracking of one or more blades comprising: a blade tracking adjustment mechanism connected to one or more blades of an aircraft; a blade tracking measurement system that measures the tracking of the one or more blades; and a computer that receives an output from the blade tracking measurement system with tracking information for each of the one or more blades; wherein the computer outputs instructions for the blade tracking adjustment mechanism to change a pitch of one or more of the blades to correct blade tracking. | 2018-06-07 |
20180155016 | AERIAL VEHICLE - Disclosed is an aerial vehicle, comprising: an airframe, a propeller(s), a duct(s) and a driving device, wherein the duct(s) is arranged on the airframe and adapted to increase a lifting force for the aerial vehicle, the propeller is arranged in the respective duct and is connected to the airframe, and the driving device is connected to the propeller(s) and is arranged on the airframe. | 2018-06-07 |
20180155017 | VTOL AIRCRAFT WITH WINGS - A VTOL aircraft is provided with a fuselage, a pair of first thrust units, a pair of second thrust units, and a pair of first wings. The first thrust units and the second thrust units are tiltably mounted on the fuselage. The first wings are securely mounted on the fuselage, and each first wing has a root end and an outer end. The longitudinal length of the outer end is larger than that of the root end. Thus, when the VTOL aircraft is landing or taking off, the airflow can pass around the root ends of the first wings; when the VTOL aircraft is cruising or gliding, the wings can provide lift, so that the first thrust units and the second thrust units can operate in a low mode, which makes the VTOL aircraft save energy and land safely even when the thrust units are broken. | 2018-06-07 |
20180155018 | Aerial Devices Capable of Controlled Flight - An aerial device ( | 2018-06-07 |
20180155019 | TILT-PROP AIRCRAFT - A tilt-prop aircraft is configured to operate in a vertical take-off and landing (VTOL) mode or a forward flight mode by adjusting a tilt angle of a rotor connected to a wing. The tilt-prop aircraft includes: a blade included in the rotor and configured to rotate to produce lift and thrust; and a tilt center shaft configured to connect the rotor and the wing to each other and adjust the tilt angle of the rotor with respect to a flight plane of the tilt-prop aircraft, wherein when the tilt angle of the rotor is adjusted, a pitch angle of the blade is varied by a power transmission unit mechanically interlocked with the tilt center shaft. | 2018-06-07 |
20180155020 | MOTORIZED DEVICE WITH RECIPROCATING MOTION OF A LOCOMOTION MEMBER AND ASSOCIATED CONTROL METHOD - Some embodiments relate to a motorized device capable of moving in a fluid and including one or more locomotor systems, each having at least one drive assembly linked to at least one locomotion member and a motor controlled by a voltage. The frequency of a reciprocating motion of the drive assembly matches the resonant frequency of the locomotion member linked to a non-movable portion by at least one prestrained elastic member. The instantaneous amplitude of the reciprocating motion of the drive assembly is adjusted to control the average position and the maximum amplitude of the reciprocating motion of the locomotion member. The Drive assembly includes at least one speed reducer for reducing the speed of rotation of the motor. When the motor is operating at is maximum mechanical power, the speed of rotation transmitted to the at least one locomotion member is reduced to match the resonance frequency. | 2018-06-07 |
20180155021 | Modular Unmanned Aerial System with Multi-Mode Propulsion - A modular Unmanned Aerial System (UAS) includes an Unmanned Aerial Vehicle (UAV) parent module and UAV child modules. A main wing extends from a respective fuselage of the modules. The UAS includes docking mechanisms coupled to wingtips of the main wings. The child modules dock with the wingtips of the parent or an adjacent child module. Docking forms a linked-flight configuration, with undocking and separation from the parent or adjacent child module achieving an independent-flight configuration. The modules have booms arranged transverse to the main wings and parallel to the longitudinal axis, as well as front and rear rotors/propellers. The front and rear propellers have axes of rotation that are normal to a plane of the longitudinal axis in a vertical takeoff and landing (VTOL) configuration, with the axis of rotation of the rear propellers parallel to the longitudinal axis in a forward-flight configuration. | 2018-06-07 |
20180155022 | System for Converting a Safeguarded Free Flight Onboard Battery-Powered Drone to a Ground-Powered Tethered Drone - A system and method for converting onboard battery-powered, free-flight drones into ground-powered tethered drones that overcome the impediments designed into safeguarded free-flight drones. In combination with a ground-sourced power supply for the drone, power being delivered to the drone through a tether, the system comprises a battery emulating module that provides false signals to the drone's battery circuit board such that the onboard batteries may be removed and the alternative ground-based power source utilized without causing the drone's main circuit board to initiate a systems shutdown. | 2018-06-07 |
20180155023 | FLIGHT CONTROL METHOD AND ELECTRONIC DEVICE FOR SUPPORTING THE SAME - An electronic device includes a communication circuit configured to communicate with an unmanned aerial vehicle (UAV) including a camera, a memory configured to store first flight information including a first flight pattern for a first location and first driving information of the camera, the first driving information corresponding to the first flight pattern, and a processor configured to be operatively connected with the communication circuit and the memory. The processor is configured to determine a flight reference location of the UAV, and control the UAV via the communication circuit such that the UAV flies based on the determined flight reference location and the first flight information. | 2018-06-07 |
20180155024 | UNMANNED AERIAL VEHICLE - Disclosed are a body of an unmanned aerial vehicle and an unmanned aerial vehicle including the same. The body includes a housing arranged in a first direction and including at least four housing sidewalls and an opening defined by the housing sidewalls and configured to receive a battery pack, a propeller support extending a specific distance from each housing sidewall in a second direction away from the center of the housing and perpendicular to the first direction and having, on a distal end, a motor and a propeller connected to the motor, and a PCB disposed on at least one of the housing sidewalls and associated with operating the motor and the propeller. | 2018-06-07 |
20180155025 | UNMANNED AERIAL VEHICLE LAUNCH SYSTEM - Aspects of the present invention relate to unmanned aerial vehicle launch technologies and methods for receiving at a head-worn computer (HWC) a plurality of images captured by an unmanned aerial vehicle (UAV) launched from a grenade launcher, and displaying the plurality of captured images in a see-through display of the HWC. | 2018-06-07 |
20180155026 | AERIAL DRONE AIR TREATING DEVICE AND METHOD OF TREATING AIR THEREWITH - A drone which can be piloted autonomously or by a user. The drone has an air treatment dispenser for spraying, or otherwise treating, a target area with one or more desired air treatments. The drone may operate as deemed desirable by a user, upon a predetermined schedule or in response to a demand signal from one or more target areas. By delivering the air treatments from an elevated position, the target area can be more uniformly and efficiently treated. | 2018-06-07 |
20180155027 | UNMANNED AERIAL VEHICLE AND LANDING SYSTEM - Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information. | 2018-06-07 |
20180155028 | DELIVERY VEHICLE INCLUDING AN UNMANNED AERIAL VEHICLE SUPPORT MECHANISM - Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information. | 2018-06-07 |
20180155029 | DELIVERY VEHICLE INCLUDING AN UNMANNED AERIAL VEHICLE LOADING ROBOT - Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information. | 2018-06-07 |
20180155030 | METHODS FOR LOADING A PARCEL CARRIER TO AN UNMANNED AERIAL VEHICLE - Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information. | 2018-06-07 |
20180155031 | METHODS FOR DELIVERING A PARCEL VIA AN UNMANNED AERIAL VEHICLE - Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information. | 2018-06-07 |
20180155032 | METHODS FOR PICKING UP A PARCEL VIA AN UNMANNED AERIAL VEHICLE - Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information. | 2018-06-07 |
20180155033 | SUSPENSION RECLINE SYSTEM - A suspension recline system for a stowable seat may comprise a suspension member comprising a first end configured to be coupled to a seat back of the stowable seat, and a second end configured to be coupled to a legrest for the stowable seat, wherein the suspension recline system is moveable between a stowed position and a deployed position. The stowable seat may recline in response to the suspension recline system being moved to the deployed position. An end of the suspension member may be configured to be inserted into a slot disposed in the legrest, in the deployed position. | 2018-06-07 |
20180155034 | AIRCRAFT SEAT AND METHOD FOR ADJUSTING AN AIRCRAFT SEAT - Aircraft seat having a first seat element and a second seat element, the second seat element being mounted so as to be adjustable relative to the first seat element, a spring element that moves the second seat element relative to the first seat element being provided, it being possible for the force acting on the second seat element by the spring element to be released by an actuating element such that the spring element is deactivated in a first switching position of the actuating element, and the spring element is activated in a second switching position of the actuating element, where a force limitation element is provided, by which the force acting on the second seat element by the spring element can be limited to a predetermined value such that intermediate states between the first and the second switching positions can also be set. | 2018-06-07 |
20180155035 | Components for Enhancement of a Low Profile Crew Attendant Seat - A crew attendant seat (CAS) positioned within a wall of an aircraft cabin includes a frame defining a periphery of the CAS. A seat portion is positioned within the frame that includes a seat bottom connected to a seatback by a hinge mechanism in which the seat bottom rotates between stowed and deployed positions. A spring member is mounted at one end to the frame and at another end to an aperture on the hinge mechanism, which causes the seat bottom to move to the stowed or deployed position based on relative positioning between the aperture and pivot points for the spring member and hinge mechanism. A harness includes at least one shoulder strap and lap belt coupled together by a buckle. A storage area retains the lap belt and the buckle within the frame when the seat bottom is in the stowed position. | 2018-06-07 |
20180155036 | AIRFLOW DIVERTER FOR AIRCRAFT AND METHOD OF USE - Disclosed is a stowable airflow diverter for removable attachment to a floor vent of a turbine aircraft. The air diverter comprises vertical ducting extending from a base. A flexible gasket and magnets are attached to the base for engagement with the floor vent. A nozzle attached to the vertical ducting redirects the airflow emanating from the floor vent from horizontal to vertical in order to direct air conditioned air into the cock pit of the aircraft. In an alternate embodiment, the nozzle is rotatable with respect to the vertical axis of the duct. In another alternate embodiment, the nozzle and vertical duct comprise telescoping segments such that the device can be collapsed into the floor vent. | 2018-06-07 |
20180155037 | APPARATUS AND METHOD OF MONITORING FOR IN-FLIGHT AIRCRAFT ENGINE ICE CRYSTAL ACCRETION - A method of monitoring for the in-flight accretion of matter involves an electric field sensor applying a time-varying electric field to an engine surface of an aircraft while the aircraft is in flight. The electric field sensor is thermally-coupled and thermally-matched to the engine surface. A sensor monitor receives, in substantially real-time from the electric field sensor, at least one measurement set that includes a measurement of a phase and a magnitude of a current detected by the electric field sensor and resulting from the time-varying electric field. The sensor monitor generates an assessment, in substantially real-time, of an instantaneous accumulation of matter on the engine surface from the at least one measurement set. The sensor monitor activates an alarm upon the assessment indicating an accumulation of matter on the engine surface. | 2018-06-07 |
20180155038 | Aircraft Parachute System - An aircraft parachute system includes an aircraft that has a fuselage, a pair of wings, a tail section and a plurality of engines. A plurality of parachute units is provided and each of the parachute units is coupled to the aircraft. Each of the parachute units is selectively deployed when the aircraft experiences an in-flight emergency such that the plurality of parachute units inhibits the aircraft from crashing. A plurality of balloon units is provided and each of the balloon units is coupled to the aircraft. Each of the balloon units is selectively deployed when the aircraft experiences the in-flight emergency. In this way each of the balloon units floats the aircraft in water when the aircraft lands in water. | 2018-06-07 |
20180155039 | COLLAPSIBLE ASPIRATOR BARREL - An aspirator includes an aspirator body having at least one flapper door designed to allow intake of a gas from an environment of the aspirator. The aspirator also includes an aspirator barrel having an end tip, a compressible spring, and a fabric positioned about the compressible spring, and designed to extend in response to receiving the gas and to transfer the gas from the aspirator body to the inflatable flotation device. The aspirator also includes a gas valve designed to receive a fluid from a compressed fluid source. The aspirator also includes a nozzle positioned within the aspirator body, coupled to the gas valve, and designed to receive the fluid via the gas valve and to direct at least a portion of the fluid towards the aspirator barrel such that the at least one flapper door allows the gas to flow from the environment into the aspirator barrel. | 2018-06-07 |
20180155040 | VARIABLE PITCH FOR COORDINATED CONTROL - A system is described that includes a turbine engine including an engine fan including one or more variable-pitch blades driven by a shaft, which rotates at a rotational speed which depends on a pitch of the one or more variable-pitch blades of the engine fan. The system further includes a generator configured to produce alternating-current (AC) electricity at a particular frequency relative to the rotational speed of the shaft. The system also includes a propulsor, which includes a propulsor motor and a propulsor fan. The propulsor motor is configured to drive, based on the AC electricity produced by the generator, the propulsor fan. The system includes a controller configured to control the particular frequency of the AC electricity by at least controlling the pitch of the one or more variable-pitch blades of the engine fan and thereby the rotational speed of the generator. | 2018-06-07 |
20180155041 | TURBINE ENGINE SUSPENSION DEVICE - A suspension device for suspending, for example, a turbine engine to a pylon, the device comprising a first unit interposed between a first lug and a second lug of a second unit, the first unit having a bore for passing an axle running through first and second bushings mounted respectively in said first and second lugs; and a clamping unit interacting with the axle. The device further comprising a third bushing mounted in the second lug and having radial centering means which interact with the complementary centering means of a head section of the axle; and a fourth axially slidably mounted bushing, biased axially by the clamping unit, and comprising radial centering means which interact with complementary centering means of the first bushing. | 2018-06-07 |
20180155042 | Composite Fan Cowl with a Core Having Tailored Thickness - An engine nacelle comprised of a top portion with hinges and a composite fan cowl pivotally connected to the top portion by the hinges. The composite fan cowl comprises a core with a hinge zone having a first thickness and a body zone having a second thickness. The hinge zone includes the hinges. The body zone is distal from the hinge zone, and the first thickness is less than the second thickness. | 2018-06-07 |
20180155043 | Composite Fan Cowl Having Core with Varying Thickness - An engine nacelle comprised of an inlet, an exhaust end, and a composite fan cowl. The composite fan cowl has a core with a thickness varying in a direction moving from the inlet to the exhaust end. | 2018-06-07 |
20180155044 | METHOD AND APPARATUS FOR OPERATING A POWER SYSTEM ARCHITECTURE - A method and apparatus for operating a power system architecture including an electrical power storage system, a power distribution bus selectively connected with the electrical power storage device, a hydraulic pump selectively connected with the electrical power storage device and a controller module communicatively connected with the electrical power storage system and the hydraulic pump. | 2018-06-07 |
20180155045 | CROSS FLOW FAN FOR WIDE AIRCRAFT FUSELAGE - A cross flow fan to be incorporated into an aircraft fuselage comprises an ingestion fan rotor to be positioned in a tail section of an aircraft fuselage to reduce boundary layer air from a top surface of the fuselage and to drive the air away from the top surface, and a drive arrangement for the ingestion fan rotor. An aircraft is also disclosed. | 2018-06-07 |
20180155046 | METHODS AND APPARATUS TO COOL A VEHICLE HEAT SOURCE - Methods and apparatus to cool a vehicle heat source are disclosed herein. An example apparatus includes a first tank and a second tank. The first tank and the second tank are disposed on a vehicle. The second tank is in fluid communication with the first tank. An engine of the vehicle is to be supplied with fuel from at least one of the first tank or the second tank. The example apparatus also includes a cooling system disposed on the vehicle to cool the fuel flowing from the first tank to the second tank. The example apparatus further includes a heat exchanger operatively coupled to a heat source disposed on the vehicle. The fuel from the second tank is to flow to the first tank via the heat exchanger to cool the heat source. | 2018-06-07 |
20180155047 | CATALYTIC FUEL TANK INERTING APPARATUS FOR AIRCRAFT - Fuel tank inerting systems and methods for aircraft are provided. The systems include a fuel tank, a first reactant source fluidly connected to the fuel tank, the first source arranged to receive fuel from the fuel tank, a second reactant source, a catalytic reactor arranged to receive a first reactant from the first source and a second reactant from the second source to generate an inert gas that is supplied to the fuel tank to fill a ullage space of the fuel tank, and a heating duct connected to the second reactant source, wherein a thermal energy of the second reactant is employed to heat the first reactant source. | 2018-06-07 |
20180155048 | CATALYTIC FUEL TANK INERTING APPARATUS FOR AIRCRAFT - Fuel tank inerting systems and methods for aircraft are provided. The systems include a fuel tank, a first reactant source fluidly connected to the fuel tank and arranged to receive fuel from the fuel tank, a second reactant source, a catalytic reactor arranged to receive a first and second reactants from the first and second sources, respectively, to generate an inert gas that is supplied to the fuel tank to fill a ullage space of the fuel tank, a heat exchanger arranged between the catalytic reactor and the fuel tank and downstream of the catalytic reactor, the heat exchanger arranged to at least one of condense and cool an output from the catalytic reactor to separate out an inert gas and a byproduct, and a cool air source arranged to supply cool air to the heat exchanger and then the catalytic reactor to provide thermal control of the catalytic reactor. | 2018-06-07 |
20180155049 | CATALYTIC FUEL TANK INERTING APPARATUS FOR AIRCRAFT - Fuel tank inerting systems and methods for aircraft are provided. The systems include a fuel tank, a first reactant source fluidly connected to the fuel tank, the first source arranged to receive fuel from the fuel tank, a second reactant source, a catalytic reactor arranged to receive a first reactant from the first source and a second reactant from the second source to generate an inert gas that is supplied to the fuel tank to fill a ullage space of the fuel tank, and an inert gas recycling system located downstream of the catalytic reactor and upstream of the fuel tank, wherein the inert gas recycling system is arranged to direct a portion of the inert gas to the catalytic reactor. | 2018-06-07 |
20180155050 | CATALYTIC FUEL TANK INERTING APPARATUS FOR AIRCRAFT - Fuel tank inerting systems and methods for an aircraft. The systems include a fuel tank, a first reactant source fluidly connected to the fuel tank, the first source arranged to receive fuel from the fuel tank, a second reactant source, a catalytic reactor arranged to receive a first reactant from the first source and a second reactant from the second source to generate an inert gas that is supplied to the fuel tank to fill a ullage space of the fuel tank, and a heating duct thermally connected to the catalytic reactor and arranged in thermal communication with the first source to provide heat to the first source to generate the first reactant. | 2018-06-07 |
20180155051 | AIRCRAFT SYSTEM - An aircraft capable of operating at a variety of speeds includes a power plant and an auxiliary turbine. The auxiliary turbine can be a ram air turbine used to expand and cool an airflow and provide work. The cooled airflow from the auxiliary turbine can be used in a heat exchange device such as, but not limited to, a fuel/air heat exchanger. In one embodiment the cooled airflow can be used to exchange heat with a compressor airflow being routed to cool a turbine. Work developed from the auxiliary turbine can be used to power a heating device and rotate a device to add work to a shaft of the aircraft power plant. In one form the aircraft power plant is a gas turbine engine and the work developed from the auxiliary turbine is used to heat a combustor flow or to drive a shaft that couples a turbine and a compressor. | 2018-06-07 |
20180155052 | METHOD AND SYSTEM FOR MONITORING AIRCRAFT STATUS - A computerised method is provided for monitoring the status of an aircraft. The method comprises sending, from an output module of an aircraft monitoring system, a reporting more report data signal response and monitoring, at an input module of the aircraft monitoring system, for received data signal to the aircraft monitoring system. This sets a contract with the aircraft that may be used to monitor for unexpected behaviour or non-compliance with the contract terms. The method further comprises determining, at a processor of the aircraft monitoring system, if one or more alert criteria have been satisfied by the received data signal responses and generating, at an alerting module of the aircraft monitoring system, an alert based on the determination. | 2018-06-07 |
20180155053 | DIFFERENTIAL FOR CONTROL SURFACE ACTUATORS - An actuation mechanism, a flap mechanism, and an aircraft are provided. The actuation mechanism includes drive links and drive mechanisms connected to opposite ends of the flap that move the flap to various positions. The drive mechanisms are actuated by torque tubes connected to a drive motor via a differential. The differential distributes torque to the torque tubes. In the event of abnormal operation of one of the drive links or drive mechanisms, the differential limits torque to the remaining drive link and drive mechanism such that the flap does not deploy or retract in a skewed manner. | 2018-06-07 |
20180155054 | INDICATING SYSTEMS, DEVICES AND METHODS FOR HIGH-LIFT FLIGHT CONTROL SURFACES OF AIRCRAFT - Systems, devices and methods a for use with one or more high-lift flight control surfaces ( | 2018-06-07 |
20180155055 | Structural Composite Component And Method For Configuring A Structural Composite Component - A structural composite component, in particular for an aircraft or spacecraft, includes: a lightning strike protection layer; and a composite battery including a cathode layer and a separation layer, wherein the lightning strike protection layer is formed integrated with the cathode layer, and wherein the separation layer is configured for providing acoustic damping, and/or fire barrier, and/or impact resistance to the structural composite component. A method for configuring such a structural composite component; and an aircraft or spacecraft including such a structural composite component are also described. | 2018-06-07 |
20180155056 | Flight Landing Sequence of an Unmanned Aerial Vehicle into the Hand of the Operator - A landing sequence for the unmanned aerial vehicle (“UAV”) wherein once the landing sequence is initiated, the UAV detects the operator's hand after hovering at an operative height, then the UAV begins a dissent at an operative rate toward the operators hands reducing the lift generated by the UAV until a time where the operator's hand exerts enough pressure on the bottom of the UAV to trigger the UAV to cut all power to the motors thereby landing the UAV in the operator's hand giving the operator the ability to “catch” the UAV in their hand and not risk landing the UAV in an undesirable location. | 2018-06-07 |
20180155057 | METHOD AND APPARATUS USING A DRONE TO INPUT VEHICLE DATA - An unmanned aerial vehicle is operated to utilize one or more tools included in an attachment assembly to obtain state measurements on an object being analyzed by the unmanned aerial vehicle. The attachment assembly can include one or more of a digital camera for capturing a digital image (or a series of images), a color meter for measuring a paint color, a thermographic camera for measuring infrared radiation, an electronic nose device for measuring odors, or an electronic distance measuring device for measuring a distance between objects. An operation of the unmanned aerial vehicle is then modified based on the obtained state measurements. | 2018-06-07 |
20180155058 | AUTONOMOUS VEHICLE WITH SECONDARY CAMERA SYSTEM FOR USE WITH ENCOUNTERED EVENTS DURING TRAVEL - In some embodiments, apparatuses and methods are provided herein useful to monitoring an event encountered by an autonomous vehicle. In some embodiments, an autonomous vehicle for monitoring an encountered event comprises a vehicle body, a propulsion mechanism, a plurality of sensors configured to detect travel information, a primary camera system affixed to the vehicle body, a secondary camera system including two or more cameras, wherein each of the two or more camera has a different fixed field of view, and wherein each of the two or more cameras are affixed to different portions of the vehicle body, and a control circuit, the control circuit configured to receive, from the plurality of sensors, the travel information, determine, based on the travel information, that a trigger condition has occurred, and in response to a determination that the trigger condition has occurred, cause video captured by the secondary camera system to be stored. | 2018-06-07 |
20180155059 | A SYSTEM FOR HANDLING OF LUGGAGE OR PARCEL ITEMS - A system for handling of luggage or parcel items comprises a principal conveyor for conveying the items to respective unloading positions along the principal conveyor, and a first item buffer section comprising a number of first item accumulation units arranged at the unloading positions of the principal conveyor. Each of the first item accumulation units comprises a plurality of shelves for storing a plurality of items on each shelf. At least one directing apparatus at each unloading position is provided for directing the items onto the shelves of the first item accumulation units. A second item buffer section comprises second item accumulation units comprising a plurality of shelves for storing a plurality of items on each shelf. An item transfer apparatus is arranged to receive items unloaded from the first item accumulation units. A control system controls operation of the item transfer apparatus. | 2018-06-07 |
20180155060 | Maintenance Operation Analytics - One example aspect of the present disclosure is directed to a method for enhancing a maintenance operation routine. The method includes receiving, at one or more processors, engine history data. The method includes comparing, at the one or more processors, the received engine history data to expected engine history data. The method includes determining, at the one or more processors, an expected effectiveness of a plurality of maintenance operation types based on the comparison. The method includes selecting, at the one or more processors, one of the plurality of maintenance operation types based on the determinations. The method includes transmitting, at the one or more processors, a signal indicative of a notification of the selected maintenance operation type. | 2018-06-07 |
20180155061 | CONTROL SYSTEM AND METHOD - A control system having one or more controllers configured to determine a maintenance date of an engine based on monitored parameters of the engine of an aircraft. The one or more controllers also are configured to, determine an amount of coating sprayed on the engine on the determined maintenance date based on the monitored parameters and determined maintenance date. The one or more controllers also are configured to adjust the maintenance date based on needs of an aircraft fleet and regularly scheduled maintenance of the engine. | 2018-06-07 |
20180155062 | WEIGHTS FOR WATER IMMERSION TESTING - A method and apparatus for securing a rotor blade is disclosed. The apparatus includes a base and an offset member configured to maintain the base at a selected distance from a set point. A clamping member is supported by the base and is receptive of the rotor blade at a selected location of the rotor blade, wherein the rotor blade is positioned against the set point. A slidable component supports the clamping member and slides the clamping member within the base to the selected location of the rotor blade. The free end of the clam shell assembly can be secured to a support beam that raises the clam shell assembly and rotor blade from the base for immersion testing. | 2018-06-07 |
20180155063 | SYSTEMS AND METHODS FOR DIAGNOSING TURBOSHAFT ENGINE BLEED VALVES - A method for diagnosing the function of an anti-ice/start bleed valve (AISBV) includes determining an operating mode of an engine and retrieving current engine system data associated with the operating mode. The method includes indicating whether the AISBV is functioning properly based on the current engine system data. An AISBV assessment system includes an AISB V assessment module configured to be operatively connected to a plurality of sensors. The AISBV assessment module includes a processor operatively connected to a memory, wherein the memory includes instructions recorded thereon that, when read by the processor, cause the processor to determine an operating mode of an engine, retrieve current engine system data associated with the operating mode, and indicate whether an AISBV is functioning properly based on the current engine system data. | 2018-06-07 |
20180155064 | Pointing mechanism for use in an electric propulsion system of a spacecraft and electric propulsion system for use in a spacecraft - A pointing mechanism for use in an electric propulsion system of a spacecraft, the pointing mechanism comprises a mobile plate adapted to receive a thruster and defining a thrust vector of the thruster received on the mobile plate. The pointing mechanism further comprises a rotary actuator coupled to the mobile plate by means of a connecting element, the rotary actuator being configured to rotate the connecting element about a rotational axis of the rotary actuator such that the thrust vector defined by the mobile plate rotates about the rotational axis, wherein the thrust vector is inclined relative to the rotational axis. | 2018-06-07 |
20180155065 | SYSTEMS AND METHODS FOR MULTI-SPACECRAFT DISTRIBUTED ASCENT - Example methods and systems of deploying a constellation of spacecraft are described. An example method includes releasing a cluster of spacecraft from a launch vehicle at a first orbit, separating spacecraft in the cluster of spacecraft from each other to minimize overlap of visibility periods from a ground station, and raising each of the spacecraft as separated simultaneously in a synchronized ascent to a respective final orbit. An example system includes a cluster of spacecraft in orbit at a first orbit, and a ground station in communication with spacecraft of the cluster of spacecraft when the spacecraft of the cluster are visible to the ground station. The ground station commands each spacecraft to separate from each other and to raise in altitude as separated simultaneously in a synchronized ascent to a respective final orbit. | 2018-06-07 |
20180155066 | METHOD AND APPARATUS FOR CONTROLLING ORBIT OF COLLOCATED SATELLITE - Provided is a satellite orbit controlling method and apparatus. A satellite orbit adjusting method performed at a current satellite may include measuring a distance between the current satellite and another satellite using a radio frequency; calculating a relative location relationship between the current satellite and the other satellite based on the measured distance, and estimating an orbit element based on the location relationship; calculating speed increment information for controlling a maneuver based on the estimated orbit element; and adjusting a satellite orbit of the current satellite based on the speed increment information. | 2018-06-07 |
20180155067 | Satellite System - A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit. | 2018-06-07 |
20180155068 | Filling Assembly - There is described a pharmaceutical container filler assembly for filling said container with a pharmaceutical powder material, which assembly comprises: means for supporting a pharmaceutical container; a reservoir suitable for holding a bulk pharmaceutical powder, wherein the powder reservoir is connected to a filler nozzle; said filler nozzle being adapted to be located in or adjacent to the pharmaceutical container such that the pharmaceutical container can be filled with the pharmaceutical powder; characterised in that the assembly is provided with means for vibrating, such that at least a portion of the assembly can be vibrated. | 2018-06-07 |
20180155069 | A PRODUCT DISPENSER AND A METHOD OF DISPENSING A FLOWABLE PRODUCT - The present invention relates to a method and a product dispenser comprising a tank for storing a flowable product and a conveyor for conveying storage containers along a longitudinal direction from an entry position to an exit position. The product dispenser further comprises a dosing mechanism extending in the longitudinal direction above the conveyor. The dosing mechanism comprises an inner cylindrical part and an outer cylindrical part enclosing and sealing against the inner cylindrical part. The inner cylindrical part defines a circumferential groove and a helically shaped groove extending between the entry position and the exit position. The outer cylindrical part defines an elongated opening extending in the longitudinal direction and an inlet opening for establishing a fluid path from the tank via the circumferential groove and the helically shaped groove to the elongated opening. The inner cylindrical part is rotatable for dispensing the flowable product into the storage containers. | 2018-06-07 |
20180155070 | FILL AND FINISH SYSTEMS AND METHODS - A variety of fill options is provided for a cell processing system. Certain options relate to a filling system associated with the cell processing system, the filling system comprising one or more filling stations, each with at least one container that may receive product from a container associated with a cell processing system. Other options relate to a syringe assembly that receives a product from a container associated with a cell processing system. | 2018-06-07 |
20180155071 | VOLUMETRIC METERING DEVICE FOR CONTAINER FILLING MACHINE - Some embodiments relate to a metering device, including: a metering chamber; a piston separating the metering chamber into a supply compartment and a metering compartment, the piston including a passage between the two compartments; a valve for closing the passage, allowing the passage of the product when same is in the open position; and movement mechanisms of the valve. The valve includes drive mechanisms of the piston arranged on either side of the piston in such a way that the movement of the valve in a discharge direction drives the movement of the piston in the discharge direction and the movement of the valve along the length of the cylinder body in a transfer direction, and drives the movement of the piston. | 2018-06-07 |
20180155072 | DEVICE FOR VACUUM PACKAGING, PARTICULARLY OF FOOD PRODUCTS - A packaging device, particularly for packaging trays containing food products or technical materials in a controlled atmosphere and by means of a film of plastic material, comprising an upper chamber and a lower chamber, which can be fastened by mutually superimposing them and are each provided internally with a plurality of heat-sealing and/or cutting and/or die-cutting elements arranged concentrically, the lower chamber being provided centrally with a plurality of supporting elements for a tray. | 2018-06-07 |
20180155073 | Vacuum Packaging Machine With Removable Internal And Low-Temperature "Sous Vide" Cooking Chamber - A vacuum packaging machine ( | 2018-06-07 |
20180155074 | TRAY SEALER - A tray sealer including a sealing station comprising a tool upper part, a clamping frame and a tool lower part. The tool upper part may surround a dome-shaped die used for deforming a skinnable top film. First and second channels in the dome-shaped die and in the tool upper part, respectively, are connectable to one another. The tool upper part or the dome-shaped die may comprise at least a third channel communicating with a vacuum generator so as to generate a thermal air convection from the first channel to the third channel along a side of the top film facing the dome-shaped die. | 2018-06-07 |
20180155075 | TAGGING GUN AND METHOD AND SYSTEM TO USE RADIO FREQUENCY IDENTIFICATION TAGGING - Apparatuses and methods are provided for labeling a product and reading one or more labels. The apparatus includes an outer housing, a processing unit, wherein the processing unit includes a processor, a digital reader, coupled to the housing, wherein the digital reader is configured to extract information from one or more labels, one or more labels, and a label hatch configured to eject the one or more labels. | 2018-06-07 |
20180155076 | COLLAPSIBLE INSULATING CONTAINER LINER - Collapsible insulating container liners and methods of manufacturing the same are disclosed herein. The container liner is formed as one unitary, foldable body that includes, in one example, beveled edges that form top panel(s), bottom panel(s), and side panel(s) that facilitate folding of the body to form the resulting liner. | 2018-06-07 |
20180155077 | APPARATUS AND METHOD FOR CLOSING A PACKAGE WITH A MOVABLE POURING SPOUT - For closing packages ( | 2018-06-07 |
20180155078 | DISPLAY CONTAINER - A container for transporting and storing or presenting goods includes a bottom, a first side wall segment articulated to the bottom and which can be folded about a folding axis parallel to the bottom between a first folding position and a second folding position, and at least one second side wall segment, which is articulated to a side edge of the first side wall segment and which can be pivoted about a pivoting axis perpendicular to the bottom between a first pivoting position pivoted laterally away from the first side wall segment and a second pivoting position. The first side wall segment and/or the second side wall segment have at least one angled side border segment on the side edges facing each other and the two side wall segments are articulated to each other. | 2018-06-07 |
20180155079 | EGG CARTON WITH DIAGONAL LID PANEL - A plastic egg carton having features that enable aligning and stacking of multiple cartons for transport, and providing easy-to-view print and labeling areas in multiple directions. In one embodiment, the egg carton has a unique lid including a flat diagonal stacking panel (also referred to as a diagonal lid panel) that extends between two opposing corners of the rectangular shaped carton. The top wall of the diagonal lid panel can receive labeling or printing. The diagonal lid panel also includes a sidewall extending downwardly from the top wall toward a bottom perimeter edge of the lid, the sidewall having at each of the two opposing corners at least one flat side panel that can also receive printing or labeling. In one embodiment, each of the opposing corners includes a rounded corner portion and two flat side panels disposed on either side of the rounded corner, thus providing a total of four side viewing areas (each in a different direction) for labeling or printing, enabling the consumer to view information such as egg size, date, nutritional information, retail information, or UPC labels. | 2018-06-07 |
20180155080 | SYSTEMS AND METHODS FOR DETERMINING SHRINKAGE OF A COMMODITY - Systems and methods for determining shrinkage of a commodity sold by a store are provided which may include: identifying data indicative of a volume of the commodity, associating a label with a container that holds the commodity, collecting the label information with a reader and transmitting collected label information to at least one server, automatically determining data characterizing the material in the container, associating the label information and the data characterizing the material in the container, and determining performance data related to the commodity by comparing the data indicative of the volume of the commodity supplied to the store, the data indicative of the volume of the commodity sold by the store, and the data characterizing the material in the container. | 2018-06-07 |
20180155081 | STRUCTURED BODY HAVING LIQUID FILM FORMED ON SURFACE - A structured body of the present invention has a base material ( | 2018-06-07 |
20180155082 | DRINKING OR EATING VESSEL - There is provided a drinking or eating vessel comprising an inner surface that defines a volume for receiving liquid or solid food and an outer surface that supports a polymeric coating and a decorative layer, wherein the polymeric coat- ing comprises a polymer formed by curing a coating mixture on the outer surface of the drinking or eating vessel, said coating mixture comprising a matting agent, wherein the polymeric coating has an inner surface in contact with the drinking or eating vessel and an outer surface in contact with the decorative layer, and wherein the decorative layer comprises a dry toner image applied to the outer surface of the polymeric coating. Also provided is a corresponding process for producing the drinking or eating vessel. | 2018-06-07 |
20180155083 | TAMPER EVIDENT LOCKING DEVICE - A locking device includes a lock body, a hasp and a seal. The lock body includes a hasp locking latch pivotally disposed therein and a seal locking latch pivotally disposed therein. The hasp is disposed at the lock body and movable between an open state, where a free end of the hasp is external the lock body, and a closed state, where the free end of the hasp is within the lock body. The seal, when inserted into the lock body when the hasp is in its closed state, engages the hasp locking latch to pivot the hasp locking latch to engage and lock the hasp in its closed state, and the seal, when inserted into the lock body, engages the seal locking latch to lock the seal within the lock body. The seal includes a frangible portion that is configured to break the seal into first and second portions. | 2018-06-07 |
20180155084 | Flat Patch Bottom Self Opening Style Bag and Method of Manufacture - A method of manufacturing an SOS bag of indefinite length is disclosed including, as a preliminary step, providing a gusseted tube of indefinite length. In a series of steps, the gusseted tube may be folded inwardly at its base to create front and rear flaps that are then folded about fold lines to create a folded bottom gusseted tube. A rectangular patch may then be applied thereto in a series of steps, including for example hot air welding and/or ultrasonic welding, to complete an embodiment of a bag of the disclosure, one having a unique bottom for an SOS bag. The disclosure additionally includes bags manufactured by the method disclosed herein, as well as SOS bags having the unique construction disclosed herein. | 2018-06-07 |
20180155085 | Flat Folded Bottom Self Opening Style Bag and Method of Manufacture - A method of manufacturing an SOS bag of indefinite length is disclosed including, as a preliminary step, providing a gusseted tube of indefinite length. In a series of steps, the gusseted tube may be cut, trimmed, folded, and sealed to create a unique bottom for an SOS bag. The bottoms of the front panel and the rear panel may be cut so as to permit the inward folding of the bottoms of the gussets of the gusseted tube, such that the bottoms of the gussets overlap. A front panel of the gusseted tube may then undergo a trimming and folding and heat sealing, followed by the rear panel of the gusseted tube undergoing a trimming and folding and heat sealing. The disclosure additionally includes bags manufactured by the method disclosed herein, as well as SOS bags having the unique construction disclosed herein. | 2018-06-07 |
20180155086 | Center Folded Bottom Self Opening Style Bag and Method of Manufacture - A method of manufacturing an SOS bag of indefinite length is disclosed including, as a preliminary step, providing a gusseted tube of indefinite length. In a series of steps, the gusseted tube may be cut, folded, and sealed to create a unique bottom for an SOS bag. The bottom of the tube includes a center flap flanked by two bottom flaps, where the center flap may be heat sealed onto a bottom flap. The disclosure additionally includes bags manufactured by the method disclosed herein, as well as SOS bags having the unique construction disclosed herein. | 2018-06-07 |
20180155087 | CARRYING DEVICE FOR MOBILITY AIDS - A carrying device including substantially flexible walls and a substantially rigid base. The base may be made rigid via insertion of a rigid support between two substantially flexible base pieces coupled with at least one temporary joint, such as a zipper. The walls may include a plurality of pockets and open-bottom supports for items such as drinking glasses. The device may include straps with removable fastening mechanisms to allow the device to be disposed over, around, or between the handles of a mobility device, such as a walker or a wheelchair. The device may be comprised of washable or high-durability fabric. | 2018-06-07 |
20180155088 | GUSSET STYLE POUCH, IN PARTICULAR FOR FOOD PRODUCT, CONTAINING A MEASURING DEVICE - A gusset style pouch is provided with a resealable closure system configured to selectively define a top opening of the pouch, at the opposite from a bottom, at least one strip of this system being adapted for locking an open configuration, by engaging locking elements that pivot and cause interengagement between the strips of the closure system. The locking elements are integrally formed with at least one strip of the system and made of a semi rigid plastic material, less flexible than material of the pouch sidewall. An elongated predetermined measuring utensil of shorter length than height of an interior pouch volume can be stored along the sidewall by use of a holding part formed on the strip as a lower extension. A leveling can also be performed using a free edge below the interlocking area. | 2018-06-07 |
20180155089 | Powder Dispensing Assembly - A powder dispensing assembly includes a bottle that may be inserted into a neck of a water bottle. The bottle is comprised of a deformable material and the bottle may be squeezed. A granular material is provided and the bottle contains the granular material. The granular material is urged outwardly from the bottle when the bottle is squeezed. In this way the granular material is added to a fluid in the water bottle. A seal is coupled to the bottle and the seal retains the granular material in the bottle. The seal is selectively urged into an open position when the bottle is squeezed thereby facilitating the granular material to pass through the seal. | 2018-06-07 |
20180155090 | INTEGRATED SQUEEZABLE DISPENSING CONTAINER - An elongated tubular housing adapted to receive an adjustable external compression device introduced on one end of the tubular housing distal from the opening releasing the contents, and retained in position by a member engaging a grooved strip that is integrated with and/or retained on the housing surface material with a strip surface of like material, providing a reliable, economic and functional outer compression member retention apparatus and method. Further embodiments according to the present invention include a dispenser having regions provided for ease and comfort of gripping, grooved strip end-stop to retain compression device, and grooved strip dimensional and placement details to provide functional, manufacturable and economic material dispenser. | 2018-06-07 |
20180155091 | CONTAINER AND OPENING ARRANGEMENT FOR BEVERAGE PRODUCTION - Systems, methods and containers for forming a beverage. A container includes a closure arranged with a movable element that is movable to pierce a membrane and permit beverage material in the container to exit. The movable element can include a piercing element that pierces the membrane. Gas can be introduced into the container to force beverage material to exit the container. A gas inlet port can be provided with the closure and arranged to mate with a gas source of a beverage machine. | 2018-06-07 |
20180155092 | END FITTING FOR BOTTLE HAVING SPOUTS - The invention provides a mouth-piece ( | 2018-06-07 |
20180155093 | APPARATUS FOR CONTROLLED APPLICATION OF A VISCOUS FLUID - Systems and methods for dispensing a viscous fluid using an apparatus that may include: a housing; an applicator coupling on the housing that can releasably couple an applicator that contains a viscous fluid; a gas supply coupling that receives a pressurized gas from a gas supply; a valve having a first open position in which the valve can be gradually and controllably opened to adjustably control the delivery of pressurized gas to the applicator coupling, and a second closed position where the pressurized gas delivered to the applicator coupling is vented; and a valve actuator configured to permit a user to gradually and controllably open the valve to controllably dispense the viscous fluid from the applicator, where ceasing to depress the valve actuator vents the applicator coupling and immediately discontinues the dispensing of viscous fluid from the applicator. | 2018-06-07 |
20180155094 | TAMPER EVIDENT FLIP-TOP CLOSURE, METHOD AND TOOL FOR MAKING THE SAME - A closure is provided for a container. The closure includes a base having a substantially cylindrical shape with a recessed area along a top perimeter of the base. The closure also includes a lid configured to close over and open off of the base. The closure further includes a tab that extends from a lower surface of the lid and includes a lip portion configured to fold back onto the tab and lock with the base when the lid is closed over the base. The tab detaches from the lid when opening the lid from the base after the lip portion is folded back onto the tab. A portion of the outer surface of the tab is visible through the at least one recessed area after the lid is closed over the base and remains partially visible after the tab has detached from the lid. | 2018-06-07 |
20180155095 | FLUID RECEIVER FITTING FOR ASEPTIC FLUID TRANSFER AND METHODS FOR MAKING THE SAME - A fluid receiver fitting (FRF) for supporting aseptic fluid transfer between enclosures, as well as methods for forming the fluid receiver, is disclosed. The FRF includes a unitized seal section (226) and channel section (228) formed together by 2-shot injection molding, thereby eliminating or minimizing modes of fluid contamination where the seal section and channel section are separate members. The channel section may comprise one or more channels (286) for insertion of a needle (N) therein and a respective penetration zone (266) in a corresponding section of the seal section for the needle to penetrate and thereby extract a fluid sample from a liquid stream against which a portion of the seal section is exposed. An angled interface (288) between each channel and its corresponding penetration zone provides a liquid stream pressure concentration zone which applies pressure to close a core (C) in the seal section formed by removal of the needle. | 2018-06-07 |
20180155096 | LID WITH REMOVABLE BOTTLE OPENER AND BEVERAGE CONTAINER INCLUDING THE LID - A lid which includes a removable bottle opener and a beverage container including the lid are disclosed. The lid includes a lid surface having a receiving slot that receives the bottle opener, a circumferential wall which surrounds the lid surface and engages an open end of a beverage container, and a port that is sized and shaped for passage of a liquid, the port passing through the lid surface and positioned proximal to the circumferential wall of the lid within the receiving slot. The bottle opener includes an opening at a distal end which is sized and shaped to open a cap of a bottle. The bottle opener is slidingly received in the receiving slot of the lid surface so that a proximal end of the bottle opener covers the port and impedes passage of the liquid therethrough. | 2018-06-07 |