Abstract: The present disclosure primarily relates to interceptor unmanned aerial systems and methods for countering Unmanned Aerial Systems (UAS), although the inventions disclosed herein are useful for capture of any aerial object. The system utilizes a rigid effector frame, an effector attached directly to the frame, and at least two propulsion elements connected to the effector frame, and is configured to intercept and disable threat UAS. The disclosed systems can be oriented to any virtually any angle to maximize the chances of intercept.

Abstract: A multiple seat set for use in a transport vehicle such as an aircraft is disclosed. The seat set increases seating room and comfort for passengers without increasing the footprint of the seat set. The seat set includes a staggered seating arrangement where seating surfaces of adjacent seats are disposed in alternating heights (e.g., vertical heights) while the seating surfaces and seat backs of such adjacent seats are disposed in alternating forward and back positions. The staggering of the seat surfaces and seat backs results in misalignment of shoulders and hips of passengers in adjacent seats.

Abstract: A passenger seating arrangement includes at least one seating row, the (or each) row including at least a first seat located beside a second seat or an aisle and a partition assembly located between the first and second seats, or between the first seat and the aisle. The partition assembly includes a partition wall located between the first and second seats, or between the first seat and the aisle. The wall defines an opening and a screen is slidably movable with respect to the wall between an open state in which the opening is exposed by the screen, and a closed state in which the opening is closed by the screen.

Abstract: An aircraft passenger seat configured to facilitate ergonomic alignment of a passenger while in a sleeping position, including a seat bottom; and a seatback including a central opening corresponding to a shoulder region of a passenger, and a sleep support assembly mounted within the central opening, the sleep support assembly including an adjustable support member spanning a central portion of the seatback, where the adjustable support member is configured for at least one of translation and deformation; where, when the seat bottom is aligned with the seatback in a lie-flat seating position, a load provided by the shoulder region of the passenger, at least in a side-sleeping position, causes translation and/or deformation of the adjustable support member toward a floor of an aircraft cabin, thereby facilitating ergonomic alignment of the spine.

Abstract: A ventilation system for ventilating a passenger compartment of an aircraft, an aircraft, and a method of operating the ventilation system are disclosed herein. The ventilation system includes, but is not limited to, a bezel, a fluid vent, an electronic sensor, and a valve. The bezel defines a bezel aperture and the fluid vent defines an axis that passes through the bezel aperture to direct a stream of air through the bezel into the passenger compartment. The electronic sensor is associated with the bezel and is configured to generate a bezel position signal. The valve is configured to vary a flow rate of the stream of air through the fluid vent based on the bezel position signal.

Abstract: For deicing an aircraft, a deicing system includes a base, a plurality of motorized wheel assemblies, a proximal deck and a distal deck, and a plurality of articulated arms. The base may have a length along the longitudinal axis that is substantially equivalent to a specified aircraft. The plurality of motorized wheel assemblies is disposed under the base. A movement direction of each wheel assembly is rotatable about a vertical axis. The plurality of articulated arms is disposed on the proximal deck in the distal deck. A shell is disposed on the end of each articulated arm. The plurality of motorized wheel assemblies moves the deicing system adjacent to the aircraft and the plurality of articulated arms each position a shell adjacent to the aircraft.

Abstract: An electro-pneumatic de-icer for an airfoil includes an electrically-powered compressor for compressing air, an air-storage tank for storing compressed air, a source of negative pressure, an airfoil pneumatic boot, and a control valve located between 1) the air-storage tank, 2) the source of negative pressure, and 3) the pneumatic boot for cycling between compressed air to inflate the pneumatic boot and negative pressure to deflate the pneumatic boot for cracking accumulated ice on the airfoil. An airfoil de-icing method lacking engine bleed air extraction includes compressing air with an electrically-powered compressor, storing high-pressure air from the compressor in an air-storage tank, delivering high-pressure air from the air-storage tank to inflate a pneumatic boot located along an airfoil, providing a negative-pressure source, deflating the pneumatic boot with the negative-pressure source, and alternating between inflating and deflating the pneumatic boot for cracking accumulated ice on the airfoil.

Abstract: The invention relates to an aircraft propulsion assembly comprising a cradle receiving a turbine engine comprising at least one propeller having a longitudinal axis of rotation, a gas turbine engine having a longitudinal axis of rotation offset from the axis, and a reduction gear by means of which said propeller receives drive power from said engine, wherein the propeller and the gas turbine engine are designed such that axes and are offset from one another within said cradle at least by a given value in a transverse direction, the axis of the gas turbine engine being transversely closer to a proximal lateral side of the cradle than to an opposite distal lateral side of the cradle in order to create a lateral space between said engine and said distal lateral side of the cradle, thereby forming at least one region for installing equipments, components or accessories of said turbine engine.

Abstract: A multicopter aircraft with boom-mounted rotors is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage; a port side wing coupled to the fuselage; and a starboard side wing coupled to the fuselage. Each of the wings has mounted thereto one or more booms, each boom having a forward end extending forward of a corresponding wing to which the boom is mounted and an after end extending aft of said corresponding wing to which the boom is mounted. The aircraft further includes a first plurality of lift rotors, each rotor in said first plurality being mounted on a forward end of a corresponding one or said booms; and a second plurality of lift rotors, each rotor in said second plurality being mounted on an after end of a corresponding one or said booms. Each rotor produces vertical thrust independent of the thrust produced by the other rotors.

Abstract: An aircraft controller includes a memory for storing instructions. The instructions are operable to cause the controller to perform a thrust balancing method and ensure a balanced thrust output from the aircraft.

Abstract: An aircraft nacelle including a conduit rigidly connected to an air inlet and a conduit rigidly connected to an engine, a link between the conduit rigidly connected to the air inlet and the conduit rigidly connected to the engine. The link includes a sleeve that receives one end of a first conduit and is rigidly connected to a second conduit, and linking elements that link the sleeve and the first conduit and that are distributed about the entire circumference of the nacelle, each linking element having a threaded stem oriented in a radial direction and being configured to enable tightening from inside the first conduit.

Abstract: A battery housing including a plurality of side walls oriented to define an interior, and at least one partition that subdivides the interior into at least a first battery compartment and a second battery compartment. The at least one partition defines a flame arrestor configured to provide fluid communication between the first battery compartment and the second battery compartment such that combustion gases are ventable therebetween.

Abstract: An auxiliary power unit assembly for an aircraft, including an engine assembly including an internal combustion engine, a first duct in fluid communication with an inlet of the internal combustion engine and configured to be in fluid communication with an environment of the aircraft, and a second duct configured to be in fluid communication with the environment. The second duct may be in fluid communication with an inlet of a compressor drivable by the internal combustion engine or with a compartment receiving the engine assembly. A filter extends across the first duct. The filter is removable from the first duct through an opening in a wall of the first duct, the opening accessible from an exterior of the engine assembly.

Abstract: A vehicle system includes a control unit with a weather module configured to receive weather data and to identify a wind shear zone at a location based on the weather data, the weather module further configured to generate wind shear coordinate data and wind shear characteristic data based on the weather data. The control unit further includes a display module configured to generate display commands based on the wind shear coordinate data and wind shear characteristic data from the weather module. The vehicle system further includes a display device coupled to receive the display commands from the control unit and configured to display a three-dimensional forward perspective view corresponding to a vehicle environment. The display device is further configured to display first wind shear symbology within the view at a position that indicates the location of the wind shear zone.

Abstract: The disclosure describes systems and methods for detecting an aerial vehicle landing. One method includes performing at least two of a plurality of landing tests to detect the landing of the aerial vehicle. The plurality of landing tests include a static test, a thrust test, and a shock test. Upon a detection of the landing by one of the at least two landing tests performed, the method further includes performing a free-fall test to detect a free fall of the aerial vehicle. The free fall of the aerial vehicle is a change in altitude of the aerial vehicle above an altitude change threshold. Upon a lack of a detection of the free fall by the free-fall test, the method includes setting a landed state for the aerial vehicle. Upon a detection of the free fall by the free-fall test, the method includes setting an in-air state for the aerial vehicle.

Abstract: A stereo distance measuring apparatus includes a first optical camera and a second optical camera, a position-posture calculator, an image corrector, and a stereo distance measuring unit. The first and second optical cameras are provided in an elastic structure part of an aircraft and separated from each other. The first and second optical cameras constitute a stereo camera. The position-posture calculator calculates, on the basis of a displacement amount of the elastic structure part, first and second position-posture information regarding positions and postures of the first and second optical cameras, respectively. The image corrector generates first and second corrected images by correcting, on the basis of the first and second position-posture information, positions and orientations of images taken by the first and second optical cameras, respectively. The stereo distance measuring unit calculates a distance to a photographing target, on the basis of the first and second corrected images.

Abstract: An apparatuses and method for securing a landed aerospace vehicle/object onto a landing pad includes a use of the magnetic force to couple the landed aerospace vehicle/object with the landing pad. A magnetized base captures and is anchored onto the landing pad. The use of a rocket booster in a high-gravity environment with the ensuring extreme heat exhaust emission considers the use of an exhaust ventilation system.

Abstract: Disclosed is a glide path indicator (2) comprising a light emitter (20) configured to emit a visible light signal that defines a glide path (14) for use by a pilot of an approaching aircraft (10), and a camera (22) configured to capture images of the approaching aircraft (10), the camera (22) being arranged such that at least part of the glide path (14) defined by the light emitter (20) is located within a field of view of the camera (22). The glide path indicator (2) may be mounted to a vehicle (4), for example, an aircraft carrier. The glide path indicator (2) may further comprise a stabilisation module (26) configured to stabilise the light emitter (20) and the camera (22) so as to reduce or eliminate the effects of the vehicle's motion on the glide path (14) and the field of view of the camera (22).

Abstract: A landing pad receives and stores packages delivered from an aerial vehicle and awaiting pickup from an aerial vehicle. The landing pad can be placed outside of a window and can contain a transmitter for sending out an identification signal via radio frequency to aid aerial vehicles in finding the landing pad. The landing pad contains a landing platform with a trapdoor that leads to a storage compartment. The trapdoor can be configured to only open when it receives a signal from an authorized aerial vehicle. The storage compartment can be accessed via a storage compartment door which can contain a locking mechanism. The storage compartment can be climate controlled. The landing pad can also have a transmitter that emits sounds to discourage animals from nesting on or near the landing pad. The landing pad can also include a solar power generator as a source of electrical energy.

Abstract: A method and apparatus for holding a panel. A rigid frame is secured on an aircraft on a rework area on the aircraft. A carrier is attached to the rigid frame. The panel is held on the carrier and the carrier moves the panel about a plurality of axes. The panel moves with the carrier such that the panel has a desired position relative to a rework opening in the rework area. The panel is attached to the aircraft while the panel is held in the desired position relative to the rework opening.

Abstract: A cleaning assembly for leading edges of airfoils, in particular airfoil profiles of aircraft or spacecraft, has a cleaning device that is provided with at least one cleaning member and is intended for applying mechanical pressure to a planar region of an airfoil, and has a drive having at least one drive element, which drive moves the cleaning device along the surface to be cleaned. It is proposed to adhesively hold the cleaning device on the airfoil by the at least one cleaning member and/or for the at least one cleaning member to have a sticky surface and for the at least one cleaning member to be dimensionally stable and have flexible contours.

Abstract: A spacecraft propulsion method uses cosmic ray triggered nuclear micro-fusion events to provide repeated or continuous thrust for artificial gravity during a space flight. In one embodiment, successive packages of deuterium-containing micro-fusion particle fuel material is projected in a specified direction outward from a spacecraft. In another embodiment, the micro-fusion fuel material is a coating upon a set of angled rings arranged circumferentially around the spacecraft. In a third embodiment, the micro-fusion fuel is dispersed in proximity to “wind” turbines to generate electricity for ion thrusters. In each case, the material interacts with the ambient flux of cosmic rays to generate micro-fusion products having kinetic energy that either produce thrust upon the spacecraft or drive the turbines whose electrical output in turn powers the ion thrusters.

Abstract: A Carbon Dioxide Removal System is disclosed. The system can be directed to space applications. The system incorporates unique features that allow ease of maintenance and parts replacement while in space.

Abstract: A system for filling syringes that includes a syringe filling machine. The syringe filling machine includes a syringe feeder, a syringe loader coupled with the syringe feeder, a starwheel, one or more inspection stations provided around the starwheel, a syringe filling station adjacent the starwheel, a cap feeder, a cap loader in communication with the cap feeder and adjacent the starwheel, and an ejection station adjacent the starwheel. The syringe loader is operable to receive one or more syringes and to feed the one or more syringes into the starwheel. The starwheel is operable to move the one or more syringes between the one or more inspection stations, the syringe filling station, and the cap loader.

Abstract: A method of filling packaging with pouches of product comprises conveying a plurality of spaced apart chutes along a first feed path. Each chute is loaded with pouches of product at a chute loading station. Erect boxes are conveyed along a second feed path to a chute unloading station wherein the second feed path is substantially parallel to the first feed path at the chute unloading station. The pouches of product are transferred from the chutes into interior spaces of the erect boxes at the chute unloading station as the chutes move along the first feed path and the erect boxes move along the second feed path. The chutes are returned to the chute loading station to be filled with pouches of product.

Abstract: A bottom-gusseted package comprises a package body, and a bottom gusset positioned transversely of a longitudinal axis of the package body. Formation of the bottom-gusseted package is effected by positioning individual sleeves transversely of the longitudinal axis of a flexible web which forms the package body. Tape elements are applied in overlapping relationship to opposite ends of each individual sleeve. During package formation, the flexible web is cut to form individual packages, and each individual sleeve can be cut to form a bottom gusset in one package, and a top sleeve portion in an adjacent package. A top sleeve portion of the package body can be configured to include a reclosable fastener. The tape elements facilitate formation such that the packages can be formed and filled on an associated vertical form, fill and seal apparatus have conventionally configured heat-sealing jaws.

Abstract: Improved object wrapping materials exhibiting a number of beneficial properties to overcome prior deficiencies are provided. Such properties include the inclusion of a separation interface overlay that allows for greater rigidity at the leading and trailing edges of such wraps. Also, the inclusion of shear-reducing wrap material portions is described, as well as recoil reduction structures within the leading edge regions. Furthermore, core adhesive additions allow for greater resiliency to the base wrap material as it unwinds therefrom, reducing potential waste wrap products by permitting greater amounts of wrap materials in use. Other considerations include the ability, through proper configuration designs, to position a wrap separation indicator within a certain range of distances from the trailing edge, thereby providing greater reliability of wrap application device disengagement during wrap application.

Abstract: A method for producing a pallet-less packaging unit has multiple packaging objects stacked to a stack of goods. The objects are stacked with a special layer that forms at least two encroachment areas for fork legs of a lift truck in at least one stack level. The special layer is first stacked on a normal layer larger than the special layer. The stack of goods is wrapped with its encroachment areas with a first film, the stack of goods that is wrapped on one side is turned around so the part of the stack of goods that has the special layer comes downwards and the stack of goods is wrapped with a second film that reaches up to the first film. In embodiments, second encroachment areas extend essentially at a right angle to first encroachment areas. The method provides a pallet-less packaging unit that can be handled more easily.

Abstract: An egg sorting and packaging method and assembly, wherein eggs are placed on an endless egg conveyor (2) by means of an egg supply device (3). The eggs are selectively moved from the endless egg conveyor into packaging lines (6a-6c), in which packaging lines the eggs are packed into egg packages. Eggs which are not released into one of the packaging lines remain on the endless egg conveyor and are recycled to pass by the packaging lines again in order to be released into one of the packaging lines.

Abstract: An object of the present invention is to allow a medicine dispensing cassette to be easily disassembled. The medicine dispensing cassette according to the embodiments of the present invention may include a main member, a first sub-member, a second sub-member and a third sub-member. The main member further includes an engagement release member so that when said engagement release member is moved to a first position (F), the engagement between the main member and the first sub-member is released, making it possible to separate the first sub-member from the main member. In the same manner, when the engagement release member is moved to a second position (S), the engagement between the main member and the second sub-member is released, making it possible to separate the second sub-member from the main member. The third sub-member can be removed from the main member independently from an operation of the engagement release member.

Abstract: The present invention is directed to an apparatus for loading stacks of container lids into an associated lid-applying apparatus, as typically found in a container filling facility. The apparatus includes a reciprocably movable carriage which is positioned generally above the lid-applying apparatus. The carriage can be positioned in a first, loading position, which is generally offset from the apparatus for convenient placement of the lid stacks by operators. The carriage can then be moved over the lid-applying apparatus to a second, unloading position. The carriage includes movable lid supports, which then open to release the lid stacks downwardly onto the lid-applying apparatus. In the preferred form, vertically movable lid cradles extend upwardly from the lid-applying apparatus, and receive the lid stacks from beneath carriage. The cradles then move downwardly, carrying the lid stacks downwardly, for transfer of the stacks onto the lid-applying apparatus.

Abstract: A liquid milk transfer system for conveying milk from a milk reservoir device to a milk storage container. A support structure has a first opening that communicates with an interior of the milk storage container. The first opening of the support structure has an irregular circumferential shape partially the same as partial surface dimensions of the milk reservoir.

Abstract: Various apparatus embodiments include first, second, third and fourth shafts, and further include a first movable shaft having a first movable axis that is movable between a first axis position and a second axis position, and a second movable shaft having a second movable axis that is movable between a third axis position and fourth axis position. At least one linkage connects the first movable shaft to the second movable shaft. A motor linkage connects the at least one linkage to at least one motor for providing simultaneous movement of the first and second movable shafts.

Abstract: An embodiment includes a pivot, a first station comprising: (a)(i) first clamps to secure a first bag, and (a)(ii) first panels to move a front side of the first bag away from a back side of the first bag; a second station comprising: (b)(i) second clamps to secure a second bag, and (b)(ii) second panels to move a front side of the second bag away from a back side of the second bag; at least one processor to: (c)(i) rotate the first and second stations around the pivot to simultaneously locate the first station at a first rotation stage and the second station at a second rotation stage, (c)(ii) clamp the first clamps to the first bag at the first station; moving the second panels away from each other to open the second bag at the second station; and (c)(iii) fill the third bag at the third station.

Abstract: Embodiments disclosed herein describe systems and methods for systems and methods to dynamically filling inoculations in proper quantities. Embodiments are directed towards a multi-dose prefilled reconstituted device (MPRD) that is configured to automatically prepare a plurality of vials for inoculations quickly and accurately, wherein the MPRD is a transportable device that may be moved from a laboratory environment to a field environment and/or a clinical environment.

Abstract: A method of packaging a series of differently shaped objects. The method includes receiving a first object to be packaged and identifying a first length of a stock packaging material suitable for enclosing the first object. The method continues by creating, with a bag making machine, a first bag from the stock packaging material having approximately the first length, which leads to substantially enclosing the first object in the first bag. Then the method continues by receiving a second object to be packaged, the second object having a shape or size different from the first object. A second length of the stock packaging material suitable for enclosing the second object is identified. The method continues by creating, with the bag making machine, a second bag from the stock packaging material having approximately the second length, followed by substantially enclosing the second object in the second bag.

Abstract: A wrapping machine for wrapping trayed items includes a wrap station and a conveying system for moving trayed items from an input station to the wrap station. The conveying system includes a conveyor for moving trayed items from the input station to a trayed item detection arrangement, and a prime mover operatively connected for moving the conveyor. A controller connected to the trayed item detection arrangement and the prime mover is configured for selectively carrying out a self-calibration operation in which: the prime mover is operated to cause movement of a portion of the conveyor from a start position to the trayed item detection arrangement; and an amount of prime mover movement required for the portion to travel from the start position to the trayed item detection arrangement is monitored and used to store a calibration value in memory of the controller.

Abstract: A pouring nozzle is made from a packaging laminate film which is excellent in the tear-opening property and improves lowering of a liquid draining property in pouring. A method forms a tear-inducing flaw for opening a packaging laminate film suitable for use in a package bag for housing and keeping a liquid packed material. A pouring nozzle is made from a packaging laminate film having a laminate structure of not less than three layers including a base film layer and non-oriented sealant layers laminated on front and rear surface sides of the base film layer and having a pouring path at its central portion. A tear-inducing flaw is formed by irradiating a laser beam across the pouring path and to a position where a portion of at least one of the non-oriented sealant layers on the front and rear surface sides of the base film layer is displaced by pushing.

Abstract: A wrapping machine for wrapping trayed food products includes a plurality of pneumatic components that are actuatable by delivery of pressurized air to the pneumatic components. A pneumatic arrangement produces pressurized air for actuating the pneumatic components. The pneumatic arrangement is configured to reduce moisture in the pressurized air.

Abstract: A method for penetrating a material with a fastener dispensing needle includes the steps of partially penetrating the material using a first penetration stroke, partially withdrawing the needle from the material using a first withdrawal stroke and, in turn, fully penetrating the material using a second penetration stroke. Once fully penetrated, a plastic fastener is dispensed from the fastener dispensing needle. Thereafter, the fastener dispensing needle is fully withdrawn from the material. Additional partial penetration and withdrawal strokes could be incorporated into the needle penetration cycle in a repeating pattern, as needed, with each penetration stroke preferably having a stroke length which is twice the length of each withdrawal stroke. The use of an oscillating, back-and-forth, linear needle penetration cycle serves to minimize the risk of lateral needle deflection which can result in bending or breakage of the needle as well as damage to the penetrated material.

Abstract: A water bottle includes a lid and a body removably attached to the lid. The body may comprise a weighted and rounded bottom portion. The body may further be configured to wobble without tipping over.

Abstract: A method for making a containment element that has a bottom wall (3), a lateral wall (4) connected at the bottom to the bottom wall (3) and a shaped perimetric flange that extends outwards from an upper part of the lateral wall (4), wherein the method comprises a thermoforming operating step in which a flat sheet is thermoformed and the bottom wall (3), the lateral wall (4) and an annular band (2) that projects outwards from the upper part of the lateral wall (4) are created and, subsequently, a hot bending operating step for bending the annular band (2), dividing the annular band (2) into a first annular portion (6) and a second annular portion (7) which are concentric and are not coplanar, after the hot bending the annular band (2) constituting the shaped perimetric flange. An apparatus and a machine able to implement all or part of that method are also claimed.

Abstract: An attachable panel assembly includes a replacement panel having a mounting panel and a closure panel projecting from the mounting panel. The closure panel has an attachment portion and a removable zipper tear strip disposed between the attachment portion and the mounting panel. The panel assembly also includes a first adhesive layer disposed on the mounting panel and a second adhesive layer disposed on the attachment portion of the replacement closure panel, the first adhesive layer and the second adhesive layer being disposed on opposing sides of the replacement panel. A resealable carton system includes the panel assembly attached or attachable to a carton body of a carton assembly by means of the first adhesive layer. The carton assembly can be sealed by closing an inner closure panel of the carton assembly and folding the replacement closure panel so that the second adhesive binds to the inner closure panel.

Abstract: A package (90) includes an outer sleeve (60) and a drawer (50) that is slidably receivable in the outer sleeve (60). The package further includes a two-part locking mechanism for releasably locking the drawer within the outer sleeve. The first part is provided by the outer sleeve, and the second part by the drawer as a locking flap (52) hingedly connected to a rear end of a top panel (106) of the drawer (50). The locking flap is folded outwardly of the drawer toward a forward end of the top panel to be releasably engaged with the first part of the locking mechanism.

Abstract: The invention relates to a package for tobacco related articles, in particular cigarettes, comprising an inner body (1) and an outer shell (2), wherein the inner body is configured to contain the tobacco related article, in particular the cigarettes, wherein the inner body and the outer shell are configured such that the inner body (1) can be shifted within the outer shell (2) in a longitudinal direction of the tobacco related articles, in particular in a longitudinal direction of the cigarettes, and wherein the inner body (1) and the outer shell (2) comprise a first stopping mechanism for stopping the lower bottom wall of the inner body from moving outside or substantially outside the bottom opening of the outer shell and a second stopping mechanism for preventing the lower bottom wall of the inner body from moving outside the upper end of the outer shell. The invention also relates to blanks for manufacturing the package and a method of manufacturing the package.

Abstract: A corrugated plastic box and a method for manufacturing a corrugated plastic box from a blank are provided. The method includes the steps of forming rounded edge seals on the perimeter edges of the blank, pre-sealing portions of the blank—including providing air vents to allow trapped air to escape during the pre-sealing process—to form a plurality of areas in which major and minor flap slots and a glue tab are desired, ultrasonically scoring the blank to form a plurality of flap score lines, and cutting the blank through the plurality of pre-sealed flap slots and glue tab, leaving a sealed edge.

Abstract: The present disclosure relates to a package box and a liner for the same. The package box includes a hexahedral outer box body; a cover configured to cover an opening of the outer box body; a substantially hexahedral liner placed in the outer box body and having six side walls, at least one of which side walls is configured to be a movable side wall, each movable side wall being slidably coupled with the adjacent four side walls to change the volume of the liner; and at least one resilient member disposed between each movable side wall and the wall of the outer box body facing the movable side wall, or between each movable side wall and the cover respectively, to drive each movable side walls to move towards and to get in close contact with articles placed within the liner.

Abstract: A container for consumer goods includes a rigid outer box, a rigid inner box, and a pull tab arranged over a pre-cut opening in the inner box. The pull tab includes a paper liner larger than the pre-cut opening such as a piece of bundle wrap with a paper layer of the bundle wrap contacting the consumer goods inside the box. The outer box has a hinged lid permanently attached to a connecting tab of the pull tab whereby opening the hinged lid simultaneously opens the opening in the inner box by lifting the pull tab. The pull tab includes a re-stick adhesive arranged in a single zone which adheres the piece of bundle wrap to cover the opening and the re-stick adhesive outward of the piece of bundle wrap allows the pull tab to reseal to the outer surface of the inner box.

Abstract: A can end for a metal beverage can, the can end including a cap top, arranged in connection to a pull tab configured to remove the cap top from the can end along a pre-defined groove, to thereby create a drinking or pouring aperture; and a shut-off valve, configured to seal the drinking or pouring aperture after drinking or pouring. The cap top is configured to remain located, after the removal, on top of the shut-off valve; and the pre-defined groove includes a stop for arresting, in a pre-defined location of the pre-defined groove, propagation of a tear along the pre-defined groove during the removal, where the stop includes an abrupt change of direction or an endpoint of the pre-defined groove. The can may be configured for containing a carbonated drink.

Abstract: The present invention provides a block protector assembly including a protector contoured to conform to a block of pallet where the pallet includes a plurality of blocks, and an attachment mechanism coupled to the protector, where the attachment mechanism is configured to secure the protector to the block of the pallet, where the protector includes a rigid material. The present invention also provides a method including determining a contour of a block of a pallet, fabricating a protector to follow the contour of the block, and securing the protector to the block. In addition, the present invention provides a protector configured to prevent damage to a block of a pallet, where the protector includes a first side contoured to a first side of the block, a second side contoured to a second side of the block, and a third side contoured to a third side of the block.