Abstract: A dropping mechanism with universal mounting points includes a device for securing a payload to a drone, mechanically releasing it and mounting additional accessories that can be used during flight. The dropping mechanism can be attached to either the landing gear or body of the drone, in an orientation that allows contact between the release trigger and the drone's camera. A notch and groove system holds a sliding restraint in place, keeping the payload secure during flight. Once the release trigger is pushed, an energized member pulls the sliding restraint allowing the payload to drop. Since the camera is pointed down to actuate the trigger, the user can watch as the payload falls to the ground. The use of a mechanical dropping system makes this device compatible with drones that only have an electrical connection for the camera. Universal mounting points allow attachment of a wide variety of accessories.

Abstract: Embodiments described herein may help to provide medical support via a fleet of unmanned aerial vehicles (UAVs). An illustrative UAV may include a housing, a payload, a line-deployment mechanism coupled to the housing and a line, and a payload-release mechanism that couples the line to the payload, wherein the payload -release mechanism is configured to release the payload from the line. The UAV may further include a control system configured to determine that the UAV is located at or near a delivery location and responsively: operate the line-deployment mechanism according to a variable deployment-rate profile to lower the payload to or near to the ground, determine that the payload is touching or is within a threshold distance from the ground, and responsively operate the payload-release mechanism to release the payload from the line.

Abstract: A contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having a convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include multiple panel portions that are coupled together and articulate relative to one another. The contoured class divider may include an articulation system to articulate the panel portions with respect to one another from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft.

Abstract: A passenger seat arrangement for a vehicle cabin includes at least one first group of passenger seats with a first passenger seat and a second passenger seat, at least one third passenger seat, and an aisle extending parallel to a longitudinal axis. The first passenger seat or the third passenger seat is arranged directly adjacent to the aisle and with a seating direction extending parallel thereto. A seating direction of the second passenger seat is rotated relative to the seating direction of the first passenger seat by a first angle of at least 2°, and the first group of passenger seats and the third passenger seat are arranged adjacent to one another and have a longitudinal offset along the longitudinal axis.

Abstract: A gas turbine engine includes a fan section delivering air into a compressor section. The compressor section compresses air and delivers air into a combustion section. Products of combustion pass from the combustion section over a turbine section to drive the fan section and main compressor sections. A gearbox is driven by the turbine section to drive the fan section. An environmental control system includes a higher pressure tap at a higher pressure location in the compressor section, and a lower pressure tap at a lower pressure location. The lower pressure location being at a lower pressure than the higher pressure location. The lower pressure tap communicates to a first passage leading to a downstream outlet, and having a second passage leading into a compressor section of a turbocompressor. The higher pressure tap leads into a turbine section of the turbocompressor such that air in the higher pressure tap drives the turbine section to in turn drive the compressor section of the turbocompressor.

Abstract: An emergency escape slide container includes a first portion having a first end wall and a first side wall, the first side wall and the first end wall defining a first storage space that is sized and shaped to receive an emergency escape slide. The first side wall also includes a first rolling mechanism. The emergency escape slide container also includes a second portion having a second end wall and a second side wall, the second side wall and the second end wall defining a second storage space sized and shaped to receive the emergency escape slide. The second side wall also includes a second rolling mechanism. The first portion and the second portion cooperate to define a third storage space therebetween, the third storage space being equal to a combination of the first storage space and the second storage space.

Abstract: A hybrid airship (drone, UAV) capable of significantly extended flight times can use one of two technologies, or both together. The first technology uses a combination of a lifting gas (such as hydrogen or helium) in a central volume or balloon and multirotor technology for lift and maneuvering. The second technology equips the airship with an on board generator to charge the batteries during flight for extended flight operations, with an internal combustion engine (such as a high power to weight ratio gas turbine engine) driving the generator. A quadcopter or other multicopter configuration is desirable.

Abstract: A pedestal assembly receives a pylon assembly of a tiltrotor aircraft having an airframe including a fuselage and a wing. The pedestal assembly includes inboard and outboard tip ribs that extend above the wing and respectively define inboard and outboard slots. The pedestal assembly also includes inboard and outboard bearing cartridges. The inboard bearing cartridge is received within the inboard slot, is coupled to the inboard tip rib and includes an inboard bearing assembly. The outboard bearing cartridge is received within the outboard slot, is coupled to the outboard tip rib and includes an outboard bearing assembly. The inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard tip ribs to selectively operate the tiltrotor aircraft between a helicopter mode and an airplane mode.

Abstract: An aspect includes a system for pre-start motoring synchronization for multiple engines of an aircraft. The system includes a first engine starting system of a first engine and a controller. The controller is operable to synchronize a motoring time of the first engine starting system with one or more other engine starting systems of one or more other engines of the aircraft by extending the motoring time of the first engine starting system to match, within a synchronization tolerance, the motoring time of the one or more other engine starting systems in a pre-start motoring sequence.

Abstract: A system is provided for cross engine coordination during gas turbine engine motoring. The system includes a first gas turbine engine of a first engine system, a first air turbine starter of the first engine system, a first starter air valve of the first engine system, and a controller. The controller is operable to command the first starter air valve to control delivery of compressed air to the first air turbine starter during motoring of the first gas turbine engine, monitor cross engine data of a second gas turbine engine of a second engine system to detect a present condition or a commanded action that modifies an aspect of the compressed air received at the first starter air valve, and command an adjustment to the first engine system to compensate for the modified aspect of the compressed air based on the cross engine data.

Abstract: A system is provided for alternating starter use during multi-engine motoring in an aircraft. The system includes a first engine starting system of a first engine and a controller. The controller is operable to coordinate control of the first engine starting system to alternate use of power from a power source relative to use of the power by one or more other engine starting systems of the aircraft while maintaining a starting spool speed of the first engine below a resonance speed of the starting spool during motoring of the first engine.

Abstract: A cooling system for an aircraft has at least one moveable member configured to cover an opening formed within an aircraft outer skin. An actuator moves the at least one moveable member between a fully open position where external atmosphere air can be directed through the opening to an internal passage enclosed by the aircraft outer skin and a fully closed position where the opening is covered. A controller selectively controls the actuator to move the at least one moveable member between the fully open and fully closed positions. An aircraft engine and a method of cooling an aircraft engine in an aircraft are also disclosed.

Abstract: A vertical take-off and landing (VTOL) aircraft is provided and includes wings, first and second nacelles supported on each of the wings, each of the first and second nacelles including a propeller drivable to generate aircraft thrust, and an asymmetrical power generation unit. The asymmetrical power generation unit includes a single engine unit disposed in only one of the first and second nacelles to generate power to drive the propellers of both the first and second nacelles.

Abstract: A suspension system for an aircraft auxiliary power unit located in a fuselage structure, the system including: struts (10), auxiliary power unit attachment brackets (51, 52) for connecting the strut (10) to the auxiliary power unit (30), vibration isolators (5) for joining the struts (10) and the auxiliary power unit attachment bracket (51, 52), a cone-bolt (1) attached to the auxiliary power unit attachment brackets (51, 52) and having a longitudinal threaded hollow, an inner bolt (2) partially located within the hollow of the cone-bolt (1) and threaded to it (1), an outer bolt (3) having a longitudinal through-hole and partially located within the hollow of the cone-bolt (1) and including an external thread that engages the thread of the cone-bolt (1), the inner bolt (2) extending across the hollow of said outer bolt (3).

Abstract: A system and related methods for providing stall recovery guidance symbology via a head-up display (HUD) or similar avionics display element detects stall or near-stall conditions and provides symbology to guide the pilot through recovering from the stall by prioritizing pitch correction and disengagement of the autopilot system. Pitch correction symbology guides the pilot toward reducing the aircraft angle of attack and establishing level flight, while thrust recovery symbology helps the pilot control the application of thrust to avoid prolonging or reinstituting the stall. The system modifies the stall recovery symbology in response to detected changes in pitch, angle of attack, or airspeed. Once level flight has been established and stall conditions are no longer present, the system may transition out of stall recovery mode to regular inflight symbology.

Abstract: Various embodiments of the present invention provide a system and method for notifying a flight crew of a fire condition in a cargo container of an aircraft. For instance, particular embodiments involve installing at least one notification device on a cargo container that is in communication with at least one of a fire-detection system or a fire-suppression system for the cargo container. In these particular embodiments, the notification device is configured to emit energy when the fire-detection system detects the fire condition in the cargo container or the fire-suppression system activates as a result of the fire condition. Further, particular embodiments of the invention involve installing at least one detector positioned to detect the energy emitted by the notification device. In these particular embodiments, the detector is configured to send a signal to notify the flight crew of the fire condition after detecting the energy emitted by the notification device.

Abstract: A cockpit internal anti-sabotage system (CIASS) without compromising the cockpit security and the present anti-hijacking procedure and protocol, wherein a single cockpit crew alone in the cockpit cannot deny bonafide entry of other cockpit crew or cabin crew in an attempt to commit suicide or sabotage the aircraft, the system comprises a manual door lock system and an automated door lock system wherein both the systems comprising a mechanical system or a non-mechanical system or combination of both.

Abstract: The displacements of the drone are defined by piloting commands to take moving images of a target carrying the ground station. The system comprises means for adjusting the sight angle of the camera during the displacements of the drone and of the target, so that the images are centred to the target, and means for generating flying instructions so that the distance between drone and target fulfils determined rules, these means being based on a determination of the GPS geographical position of the target with respect to the GPS geographical position of the drone, and of the angular position of the target with respect to a main axis of the drone. These means are also based on the analysis of a non-geographical signal produced by the target and received by the drone. The system allows freeing from the uncertainty of the GPS systems equipping this type of device.

Abstract: A device for automatic detection of whether an item is correctly routed is provided, the item including at least one radio frequency tag, wherein the device includes an RF communication mechanism for receiving at least one reading from the RF tag, said device being adapted to be arranged at a read point in proximity of the conveying mechanism, which conveying mechanism is operable to transport the item towards a destination, wherein the device is configured to extract identification and/or destination information from the reading received from the item on the conveying mechanism crossing past the device and to verify whether the item is correctly routed. Also, provided is a method for automatic detection of whether an item is correctly routed.

Abstract: A configuration for a satellite constellation has a plurality of planes, each plane including a plurality of satellites therein, at least some of the planes situated at a different altitude than other of the planes. In some embodiments, all planes contain the same number of satellites; in some other embodiments, at least one plane includes a different number of satellites than the other planes in the constellation. In some embodiments, the satellites in each plane are evenly spaced.

Abstract: A Hall effect thruster arranged inside a wall and including a magnetic circuit and an electric circuit including an anode, a first cathode, and a voltage source. The magnetic circuit and the electric circuit are arranged in such a manner as to generate magnetic and electric fields around the wall. In every meridian section, the magnetic circuit presents an upstream magnetic pole and a downstream magnetic pole arranged at the surface of the wall and spaced apart from each other; and the anode and the first cathode are situated on either side of the upstream magnetic pole.

Abstract: A device to stabilize and deorbit a satellite includes a pair of coplanar masts, each one carrying at least one membrane forming an aerobraking web. The masts are fixed to the satellite along non-parallel axes. Each mast is provided on the opposite end of the satellite with a mass to generate a gravity gradient. The end of each mast is fixed to the satellite. The masts form, with the bisectrix between the masts, a fixed angle to align the bisectrix with the satellite speed vector at any altitude.

Abstract: Disclosed is support equipment for collecting a reusable rocket, the support equipment including a plurality of supports located on a landing platform and spaced apart from one another, a contact support pad having a contacting face to contact a reusable rocket when the reusable rocket is landing, and connected to each of the supports to secure the reusable rocket, and a distance sensor configured to sense a position of the reusable rocket or the contact support pad, wherein each of the supports is configured to move the contact support pad based on information on a distance measured by the distance sensor, and the contact support pad is configured to secure the reusable rocket when the reusable rocket has landed, in order to prevent a damage of the reusable rocket.

Abstract: A moderator block. The moderator block includes one or more layers of a hydrogen-rich material. A plurality of voids disposed in the one or more hydrogen-rich layers. The plurality of voids is configured to generate a final particle field such that a linear energy transfer (LET) spectrum of the final particle field corresponds to a measured LET.

Abstract: The present disclosure generally relates to an apparatus for filling a biowaste tank having an inner body with first and second ends. The first end receives biowaste and the second end directs the biowaste into a tank. The apparatus has an outer body with first and second ends. The first end receives overflow and the second end is flush with the second end of the inner body, and the outer body fully encompasses the inner body. The apparatus has a first pipe with an inlet configured to attach to the tank and an outlet in the inner body, and a second pipe with an inlet in the outer body, and an outlet in the tank, the pipe configured to direct overflow biowaste from the inner body into the tank through a second aperture in the tank.

Abstract: A filling device for inhomogeneous products or products which have solid or semisolid elements of variable size and compactness in suspensions. In particular, the a filling device for filling machines is provided comprising a hollow body in which a delivery member is movably inserted, wherein the hollow body comprises a lower portion comprising a delivery duct which ends with a delivery opening, said lower portion being intercepted by a cone-shaped rotating shutter, comprising a major base, a minor base and a through hole which is aligned with the delivery duct when the filling device delivers a product, characterized in that the minor base of the rotating shutter is associated with a drawing system, which applies a constant and predetermined drawing force on said minor base. The valve described in the invention can be used in net weight filling machines.

Abstract: 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 source, a flow path providing fluid communication between the fluid source and a plurality of containers coupled to the apparatus, a sealing element disposed within each of the plurality of containers, the sealing element configured to couple the container to the apparatus and automatically seal the container when the container is decoupled from the apparatus, a retaining member including a sleeve affixed to each of the plurality of containers, to position the sealing element in a neck of each of the plurality of containers, the sleeve being configured to prevent radial expansion of the containers, and, a mixing mechanism disposed in the flow path and configured to receive an additive and introduce the additive in to the flow path.

Abstract: A system includes a conveyor that transports a carriage carrying a foodstuff along a path. A bag dispenser contains multiple bags and moves a first bag into the path. A paddle includes a hinge at a trailing edge of the paddle. The paddle includes an actuator that moves a leading edge of the paddle relative to the trailing edge between retracted and extended positions. The leading edge of the paddle moves into a mouth of the first bag as the leading edge is moved from the retracted to the extended position. While the paddle is in the extended position, movement of the carriage and the foodstuff underneath the paddle rotates the leading edge of the paddle about the hinge to open the mouth of the first bag such that continued movement of the carriage and the foodstuff moves the foodstuff through the mouth and into the first bag.

Abstract: A bag includes an upper surface and a lower surface. When the bag is in use, a material being collected in the bag is placed on the upper surface, and the lower surface is in contact with a support surface. The bag further includes a channel and a drawstring located in the channel. The channel has an opening through which the drawstring is accessible by a user of the bag. The opening is located in a corner of the bag. The bag is cinched closed by pulling on the drawstring.

Abstract: A zipper closure device for use with a turret type flexible pouch fill machine. The zipper closer device has a pair of rollers supported by an arm which is permitted to oscillate within a support module. The support module is mounted such that the rollers oscillate in a radial direction with respect to the access of rotation of the turret. The support module is supported by an arm in a post which permits positioning of the closer device with respect to the position of the pouches to be closed.

Abstract: This disclosure relates to a machine (1) for sealing containers (91) using a film (95). The machine (1) comprises a first jaw member (21), comprising a plurality of seats (20) for respective containers (91) to be sealed, and a second jaw member (22), facing towards the seats (20) of the first jaw member (21). The first jaw member (21) and the second jaw member (22) are movable one relative to the other between a first condition, in which the two jaw members (21, 22) are separated from each other by an interspace (23) suitable for receiving a film (95), and a second condition, in which the two jaw members (21, 22) are clamped together and, in use, press the film (95) against the containers (91) in the seats (20). The seats (20) are side by side one after another along a longitudinal line (200) extending between a first side (231) and a second side (232) of the interspace (23).

Abstract: A method and apparatus for formation, filling, and sealing unit dose packages for consumer products are described herein. A filling system with a filling control system is also disclosed. Although the filling system is described in conjunction with a method for forming, filling, and sealing unit dose packages, the filling system and filling control system can be used in other dispensing processes.

Abstract: A wrapping unit (1) for a packaging line (2) comprises a conveyor (6) for feeding a succession of products (3) in a first direction (7) and a wrapping station (9) arranged along the conveyor (6) for wrapping a film (5) of wrapping material around said products (3), said wrapping station (9) comprising a wrapping device (13) provided with a plurality of wrapping members (15), each of said wrapping members (15) extending in a second direction (11) perpendicular to said first direction (7), said wrapping unit (1) further comprising a stability control group (12) for preventing said products (3) from tipping along said conveyor (6), said stability control group (12) comprising a plurality of anti-tip devices (33), each of said anti-tip devices (33) being associated, during operation, with a respective product (3) to move together with said respective product (3) through said wrapping station (9).

Abstract: Control of a wrapping apparatus is facilitated by enabling an operator to input a load containment force requirement and/or a minimum number of layers of packaging material to be applied to a load, with a wrap control system automatically determining wrap force and other parameters required to meet user input requirements and/or parameters to minimize the expertise required of an operator and to provide more consistent and reliable wrapping of loads. In addition, a wrapping apparatus may be controlled to apply at least a minimum number of layers of packaging material to a load throughout a contiguous region thereof.

Abstract: In a method for wrapping a band around at least one object of at least one object, in which the at least one object is wrapped with a band, wherein the band in the form of an object-band loop is arranged around the at least one object in such a manner that at least two sections of the band are made to overlap and are connected together, wherein in an area in which the at least two band sections are made to overlap, a counter-pressure plate is introduced between the at least one object and the band, and the at least two overlapping band sections are pressed against the counter-pressure plate to connect them, prior to the introduction of the counter-pressure plate the band is passed through a band guiding device and/or positioned such that a defined free space is created for introducing the counter-pressure plate.

Abstract: A vacuum sealing system includes a vacuum pump, a lower tool to hold one or more trays carrying product, an upper tool to seal a plastic film onto the one or more trays, the upper tool including at least one seal plate with a seal plate cavity and a vacuum clamp, the system also including a controller to control the vacuum pump, the lower tool, and the upper tool.

Abstract: A lumber stacking and strapping system can provide a single-station solution for both lumber stacking and package strapping. In addition, the package strapping system may apply multiple straps simultaneously to the package. For example, a package stacking and strapping system can provide not only a mechanism for formulating a package of lumber one layer at a time, but also a mechanism for lowering a completed package directly into a compression and strapping station, such as using the lumber stacker package accumulation hoist. The stacking and strapping system can then simultaneously apply strapping around the package in multiple positions along the length of the package, with bottom battens and top corner protectors further supplied and strapped into place as desired. A method for stacking and strapping a package in a single location is also provided.

Abstract: A packing apparatus includes a sealing mechanism, a timing sensing section, and a control section. The sealing mechanism affixes tape continuously on portions of a cardboard box transported with major flaps thereof folded. The sealing mechanism includes an affixing roller to press the tape against a first side surface and the major flaps. The timing sensing section senses the timing at which the affixing of the tape on the first side surface is initiated. The control section controls pressing force exerted by the affixing roller, based on a result of the sensing performed by the timing sensing section, in such a way that the pressing force is reduced after the affixing of the tape on the first side surface is initiated.

Abstract: A packaging system for high flexibility and speed box-last packaging comprises one or more dimensional scanning sensors that are configured to scan a group of one or more target products that are to be boxed and gather dimension information describing physical dimensions of the group of one or more target products. The system also comprises one or more packaging-production machines that are configured to generate custom-made packaging templates that conform to a pre-determined set of packaging template types. Additionally, the system comprises a packaging template buffer that comprises physically divided sections that contain multiple packaging templates selected from the pre-determined set of packaging template types that are generated by the one or more packaging-production machines. Each of the packaging templates are organized within the physically divided section based upon packaging template type.

Abstract: A filling and sealing machine configured for a flexible pouch having a turret, a servomotor, and a control unit is provided. The control unit includes a memory component having logic module stored within, a processor, and a user interface. The servomotor is connected to the turret and upon an instruction from the processor, rotates the turret. The set speed of the turret, the acceleration of the turret, and the deceleration of the turret may be modified by manual control parameters. The logic module includes preset recipe programs based upon the product being dispensed. Each preset recipe includes a different parameter for the servomotor to rotate the turret. The control unit may monitor the production system status and automatically adjust the speed, acceleration and/or deceleration of the turret to meet a desired production output.

Abstract: The present disclosure relates to a labeling apparatus for labeling articles. In one implementation, the apparatus may include a transfer drum having at least one label retaining segment adapted to receive and to retain at least one label, a glue application unit adapted to apply glue onto the label, a cleaning unit adapted to clean the transfer drum and a control unit adapted to selectively activate the cleaning unit into at least any one of: a partial cleaning configuration in which the cleaning unit is configured to partially clean the at least one label retaining segment or a full cleaning configuration in which the cleaning unit is configured to fully clean the at least one label retaining segment.

Abstract: A reusable packaging and storage article for an elastic constriction ring is described wherein the article comprises a bottom top member and a member configured to releasably engage with each other, wherein the bottom member comprises: a cavity of substantially circular shape having a perimeter lip with an inner and outer surface to house, in use, a portion of the elastic constriction ring; and an at least partially pillar extending from a substantially central portion of the cavity; and wherein a summit of the pillar has a diameter less than the diameter of a central aperture of the elastic constriction ring, and a lower portion of the pillar has a diameter greater than the diameter of a central aperture of the elastic constriction ring; and wherein the top member comprises: a cavity of substantially circular shape having a perimeter lip with an inner and outer surface to house, in use, a portion of the elastic constriction ring, wherein the diameter of an inner surface of the perimeter is the same or greate

Abstract: A fluid housing of a fluid treatment system of a fluid system has a housing part of plastic material that is provided with a receiving chamber for accommodating a fluid treatment component; an installation opening, closable by a closure housing part, for installing the fluid treatment component in the receiving chamber; and a housing connecting section to connect the housing part to the closure housing part. A housing fastening section is provided with which the fluid housing can be fastened to a holding component of the fluid system. An insert is at least partially introduced into the plastic material of the housing part. The insert is provided with a reinforcement region extending with sections thereof in the housing connecting section and is further provided with fastening region extending with sections thereof in the housing fastening section. A fluid treatment system with such a fluid housing is provided.

Abstract: A child-resistant package is disclosed comprising at least one locking tab, at least one locking slot, the at least one locking slot engaging with the at least one locking tab when the child-resistant package is in a locked position. The at least one locking tab comprising memory properties to allow the at least one locking tab to releasably engage with the at least one locking slot. The at least one locking tab further comprising a corrugated material having flutes oriented in a flute direction and the memory properties including the at least one locking tab returning to the locked position after being in an unlocked position in response to being bent against the flute direction.

Abstract: The present invention provides a carton (100) made of paperboard having flaps (101, 105), the carton (100) comprising, at least one score (102) along a crease line (103) of at least one flap (101, 105), wherein the score (102) is 25% to 85% of thickness of the paperboard and 5% to 70% of length of the crease line (103). The invention also provides a method of securing flaps (101, 105) of the carton (100).

Abstract: A display box is provided for housing and retaining a cylindrical container. The box may include two side walls and a front and rear wall, a top lid extending from an upper end of one of the walls and a bottom lid extending from the lower end of the same or a different wall. At least one elongate flap further extends from the lower end of one of said side walls or rear wall, said flap being provided with crease lines along which said flap may be folded. The flap has an end portion adhered to the inner surface of the wall from which the flap extends, a first lateral portion having a proximal end adjacent the wall and a distal end extending into the box. A vertical portion extends down from the distal end of the first lateral portion and a second lateral portion connects a lower end of the vertical portion and a distal end of a base portion.

Abstract: A carton (90) for packaging one or more articles (A) includes a plurality of panels (12, 14, 16, 18) for forming a tubular structure. The plurality of panels include a top panel (16) and a pair of first and second opposed side panels (14, 18) hingedly connected to first and second opposite sides of the top panel respectively. The first and second side panels include first and second corner edges (C2, C1) respectively which are free of hinged connection to any other part of the carton. The first and second corner edges extend from the first and second sides of the top panel respectively. The carton includes a first severance line (70) extending from the first corner and a second severance line (78) extending from the second corner edge.

Abstract: A repulpable moisture resistant poultry box having a composite structure with a fluted medium, a top backing board secured to one side of the fluted medium and a bottom backing board secured to the other side of the fluted medium. The backing boards and the fluted medium are impregnated with a hydrogenated triglyceride. The backing boards each have an outer surface coated with an emulsion of hydrogenated triglyceride and styrene acrylic to provide moisture resistance repulpable and recyclable box.

Abstract: A carton for holding at least one article includes a dispenser that includes a dispenser feature and at least two first panels extending at least partially around an interior of the dispenser. The carton also includes a sleeve including at least two second panels extending at least partially around an interior of the sleeve. The interior of the sleeve at least partially receives the dispenser, and the dispenser is in slidable engagement with the sleeve and is moveable between a first position in which the dispenser feature is inaccessible and a second position in which the dispenser feature is accessible.

Abstract: A production process of a bamboo bowl includes: cutting out arc-shaped bamboo strips on a bamboo board; splicing the bamboo strips into a bamboo ring; finally gluing several bamboo rings with gradually larger diameters on the bottom of the bamboo bowl successively to form a bamboo bowl billet, and making into a bamboo bowl after subsequent processings. The bamboo bowl made by the above production process includes a bamboo bowl bottom and bamboo rings superimposed on the bamboo bowl bottom; the bamboo ring consists of at least two arc-shaped bamboo strips, the diameters of the bamboo rings are gradually increased from the bottom up; the arc-shaped bamboo strips are fixed through adhesive, and the bamboo rings are also fixed through adhesive.