Abstract: An aircraft (10) includes a fuselage (12) delimiting a cockpit (14), a passenger entry area (18) and a passenger cabin (16) configured to accommodate passengers during a flight phase. The entry area (18) is interposed longitudinally between the cockpit (14) and the cabin. The cockpit and the entry area are delimited by a front separating element (24) and the entry area and the cabin are delimited by a rear separating element (26). The fuselage delimits a side boarding door (20). A transverse median plane (66) of the boarding door is placed at a distance from the front separating element, considered along the longitudinal axis, greater than 39% of the length between the front separating element and the rear separating element, considered along the longitudinal axis.

Abstract: A luggage compartment arrangement for an aircraft has a base carrier which can be attached in the aircraft and a luggage compartment which is mounted so as to be pivotable about a pivot axis relative to the base carrier and/or so as to be movable translationally along a displacement path. The luggage compartment arrangement further has a spindle drive for pivoting and/or displacing the luggage compartment about the pivot axis. The spindle drive has a motor block with a rotatable spindle and a motor for driving the spindle. Via a spindle nut, at connection points, which are each radially remote from the pivot axis in the case of pivoting, the motor block is attached to the base carrier, and the spindle nut is at least indirectly attached to the luggage compartment, or vice versa.

Abstract: A trolley lift for connecting a lower aircraft deck to an upper aircraft deck. The trolley lift comprises a platform configured to accommodate at least one trolley, wherein the platform delimits a lift compartment at the bottom, and a cover which delimits the lift compartment at the top. In particular, on a side facing away from the lift compartment, the cover at least partly forms a floor of the upper aircraft deck. Furthermore, an aircraft area having a trolley lift and an aircraft having a trolley lift and/or an aircraft area are described.

Abstract: The present disclosure provides a detachable cabin attendant seat (CAS). In various embodiments, the detachable CAS may comprise a first section, comprising, a first rod and a second rod, and a first post and a second post extending from the first section, wherein the first post and the second post are configured to be coupled to a mount assembly when the detachable CAS is in a stowed position and the first rod and the second rod are configured to be coupled to the mount assembly when the detachable CAS is in a deployed position.

Abstract: To provide an air conditioning piping structure for an aircraft which can promote mixing of temperature adjusted air and recirculated air flowing into a mixing chamber forming an air conditioning system. An air conditioning piping structure causes temperature adjusted air obtained by an air conditioning apparatus of an aircraft and recirculated air discharged from a pressurized compartment to flow into a mixing chamber which mixes the temperature adjusted air and the recirculated air. This air conditioning piping structure includes a first pipe through which the temperature adjusted air flows, a second pipe through which the recirculated air flows, and which is connected to the first pipe, and a flow passage restricting part configured to apply a resistance to at least one of the temperature adjusted air and the recirculated air in a vicinity of a merging position where the temperature adjusted air and the recirculated air are merged.

Abstract: A primary structure of an aircraft pylon, which comprises upper and lower spars, right-hand and left-hand lateral panels, transverse reinforcers that are disposed in transverse planes and, each have a square or rectangular contour and at least one sole to which the upper and lower spars and the right-hand and left-hand lateral panels are fastened. At least one of the transverse reinforcers of the primary structure has first and second link rods that are oriented along diagonals of the transverse reinforcer, and connecting systems that each connect first and second ends of the first and second link rods to the sole or to one of the soles.

Abstract: An assembly of parts assembled with one another by a shaft passing through orifices formed in the parts is disclosed. The shaft has a base diameter (DB) and a thickened diameter (DE) over diametrically opposed arcs at two different sections. The orifices are aligned with one another and each have a periphery having a first diameter (D1) on first diametrically opposed portions, the first diameter (D1) corresponding to the thickened diameter (DE), and a second diameter (D2), greater than the first diameter (D1), on second portions of the periphery. This allows the shaft to be fitted easily even when the orifices are only approximately aligned, and also makes removal easier.

Abstract: The present disclosure provides a method and a system for controlling operation of an engine of an aircraft. The method comprises, at a controller of the engine, obtaining an actual engine output power for the engine, the actual engine output power based on a propeller rotation speed and a propeller blade pitch angle; converting the actual engine output power to a predicted thrust value; determining an actual engine power limit associated with a thrust limit of a propeller coupled to the engine from the predicted thrust value; and setting a maximum engine power limit of the engine using the actual engine power limit associated with the thrust limit of the propeller.

Abstract: A system and method for reducing a psychoacoustic penalty of acoustic noise emitted by an aircraft, including a plurality of propulsion assemblies coupled to the aircraft, wherein each of the plurality of propulsion assemblies includes a motor, and a plurality of blades defined by a propeller, wherein the plurality of blades can define an asymmetric blade spacing; a control subsystem coupled to the aircraft and communicatively coupled to the motor of each of the plurality of propulsion assemblies, wherein the control subsystem is operable to rotate each of the plurality of propulsion assemblies at a different frequency to modulate the acoustic power distribution of the emitted acoustic signature.

Abstract: A fuel system is provided for an aircraft having a fuel source. The fuel system includes a fuel oxygen reduction unit defining a liquid fuel supply path, a stripping gas supply path, a liquid fuel outlet path, and a stripping gas return path, wherein the stripping gas return path is in airflow communication with the fuel source.

Abstract: Disclosed herein is a method that comprises detecting that a rate of decrease in fuel quantity for an aircraft exceeds a previously-determined baseline rate of decrease in fuel quantity for the aircraft by a threshold rate during a corresponding segment of flight of the aircraft. The method also comprises determining that a fuel jettison setting for the aircraft is enabled in response to the detected increase in the rate of decrease in fuel quantity. The method further comprises determining that an angle of one or more flaps of the aircraft satisfies a threshold angle. The method additionally comprises generating an alert indicating possible fuel contamination of the one or more flaps due to jettisoned fuel.

Abstract: Apparatus and method for establishing and maintaining a visual reference on a surface below an aircraft for the purpose of landing the aircraft. The apparatus includes an infrared, green, and/or red laser that produces a laser beam terminating in a spot or pattern on a surface below the aircraft, the beam being no more than 1 mW. The laser can be mounted on a lower portion of the nose of the aircraft, and in a fixed direction that remains fixed during flight. The apparatus can also include a light assembly that houses the laser and maintains it in the fixed direction. The light assembly includes a shroud that extends around a front face of the light assembly, and extends from the front face of the light assembly in the fixed direction of the laser. The light assembly can also house non-laser light sources which produce white, green, and/or infrared light.

Abstract: A system and a manner of handling luggage items, such as in an airport, where the luggage items are stored in a plurality of buffers, where the luggage items of one buffer are provided into one container which is configured for loading into and transport on airplanes. The luggage items may be sorted into the buffers so that e.g. high priority luggage items are stored in containers separate from containers holding lower priority luggage items.

Abstract: Systems and methods for fusing and analyzing multiple sources of data from a plurality of aircraft-related data sources for fault determination and other integrated vehicle health management (IVHM) diagnostics are provided. More particularly, one or more portions of data from a plurality of aircraft-related data sources for one or more aircraft are accessed. One or more alerts indicative of a data anomaly within the one or more portions of aircraft-related data sources can be detected, wherein a type of alert and originating data source associated with each alert as well as optional related confidence scores can be identified. One or more aircraft faults can be determined based at least in part on a correlation of identified types and data sources for detected alerts. An output indicative of the determined one or more aircraft faults can be provided.

Abstract: A mobile machine includes a fuselage having at least one door, inside which is located a unit for processing measurements taken by at least one measurement device installed outside said fuselage. The system for communication between the processing unit and the measurement device includes a flex circuit that is affixed at least partially flat in the door corner between the door and the rim of the opening formed in the fuselage with which the door is associated and one of the ends, the internal end, of which is located inside the fuselage and the other, external, end of which is located outside. Since the flex circuit makes it possible to pass through the wall of the fuselage via the opening for doors, the need to make substantial modifications to the aircraft is avoided.

Abstract: An interplanetary spacecraft makes use of ambient cosmic rays and muons generated therefrom to provide micro-fusion propulsion. The craft has a central reaction chamber surrounded by the craft's main body. Deuterium-containing fuel material is injected at a specified rate into the reaction chamber where it is exposed to the cosmic rays and muons to produce energetic reaction products. Some reaction products exit the chamber through an opening to provide reaction thrust, while other reaction products interact with a dome of the chamber to directly apply a thrusting force. The craft can be a preassembled station having multiple reaction chambers and can form an orbiting space station around a planet or moon or a manufacturing or habitat station on a planetary or lunar surface.

Abstract: The disclosure relates to a method and apparatus of rotating mass propulsion. The method and apparatus entails rotating a mass to generate thrust. Varying the speed and direction of rotation provides some control of the magnitude and direction of the thrust generated. The method and apparatus of the invention pertinent to a propulsion system for spacecrafts or astromotive vehicles under conditions of zero to low gravity and atmosphere.

Abstract: Systems and methods are provided for protecting a temperature sensitive object. A system includes a temperature sensitive object and a thermal control material in thermal communication with the temperature sensitive object. The thermal control material has an emissivity that varies as a function of temperature, and includes a substrate comprising a first surface comprising one of a photonic crystal, a metamaterial, a metasurface, and a multilayer film, a solid state phase change material in contact with the surface, and a reflective thin film material at one of a second surface of the substrate, at a surface of the solid state phase change material, and on an opposite side of an optical cavity from the substrate.

Abstract: Example aspects of an assembly and a method for using a deployed electromagnetic radiation deflector shield are disclosed. The assembly can comprise a deployable deployed electromagnetic radiation deflector shield comprising: a power supply; and an electromagnet configured to generate a magnetic field to deflect radiation; and a spacecraft, wherein the deployed electromagnetic radiation deflector shield is unattached to the spacecraft when deployed from the spacecraft, wherein the deployed electromagnetic radiation deflector shield is deployed at a distance away from the spacecraft, and wherein the distance is configured to prevent the magnetic field generated by the electromagnet from interfering with the spacecraft.

Abstract: Systems and methods for launching a plurality of spacecraft, provided in a stack of spacecraft, from a launch vehicle traveling along an in-track path include releasing, in a first separation event occurring at a first time, a first spacecraft from the stack of spacecraft using a first separation force having a first separation force in-track component along the in-track path. Subsequently, in a second separation event occurring at a second time, a second spacecraft is released from the stack of spacecraft using a second separation force having a second separation force in-track component along the in-track path, wherein the second time occurs a first time delay after the first time. The first and second separation in-track components may be different, such as by varying a magnitude of the separation force or an angle at which the spacecraft is launched.

Abstract: Spacecraft multifunction connecting mechanisms, and associated systems and methods are described herein. A representative spacecraft system includes a connecting device, which in turn includes a housing having a common port opening, a first connecting element carried by the housing and positioned to connect with a corresponding first spacecraft connecting structure having a first configuration, and a second connecting element carried by the housing and positioned to connect with a corresponding second spacecraft connecting structure having a second configuration different than the first configuration. At least one of the first and second connecting elements is moveable relative to the other between an operational position and a non-operational position, and each of the first and second connecting elements, when connected to the corresponding first or second spacecraft connecting structure, is positioned to allow transport through the common port opening.

Abstract: The invention relates to a method and to a device for filling a medical packaging formed as a pouch. Preferably, the packaging is filled with liquid via a port, wherein the port is aerated with a protective gas, such as nitrogen, for example, during filling According to the invention, prior to filling with liquid, the packaging is filled with an inert gas, such as nitrogen, for example, which then provides the headspace of the filled and closed pouch. This results in a particularly low oxygen content in the headspace of the pouch.

Abstract: A self-propelled wrapping machine movable around a load, for wrapping the latter with a film of plastic material, comprises a self-propelled carriage with guide means, a column fixed to the carriage and slidably supporting an unwinding unit of the film, sensor means to detect surfaces and/or external edges of the load in their total extension and along a detection direction and process related signals, a control unit to receive the signals from the sensor means, calculate a peripheral outline of plan maximum overall dimension of the load on the basis of the surfaces and/or external edges detected by the sensor means, and process a wrapping path of the wrapping machine around the load on the basis of the peripheral outline so as to avoid collisions with the load; the control unit controls the guide means to guide the wrapping machine along the wrapping path.

Abstract: A method of packaging easel includes attaching an easel packaging fixture to a rotatable turntable of a stretch wrapping apparatus that includes a tower and a carriage movable along the tower. An easel bundle is positioned on the easel packaging fixture. Each easel bundle includes one or more easels with a lower portion inserted into a bottom cap and an upper portion inserted into a top cap. The turntable is rotated, causing rotation of the easel packaging fixture and the easel bundle with respect to the stretch wrapping apparatus. As the easel packaging fixture rotates, a wrapping material from the carriage of the stretch wrapping apparatus wraps around the easel bundle. The carriage moves along the length of the tower to wrap a length of the easel bundle.

Abstract: Recyclable waste byproducts are efficiently collected for recycling at stores or other locations by compacting the recyclable waste as layers in a composite bale. The composite bales can be formed using existing cardboard balers that retailers or other stores typically already have for baling recyclable cardboard. In one embodiment, the composite bales are formed by binding together a layer of one type of recyclable waste and a layer of recyclable waste that includes one or more types of recyclable waste byproducts. The layered structure can be modified to omit one of the layers or to add additional waste byproduct layers.

Abstract: The present disclosure relates to a strapping head of a strapping device for strapping packaged goods with a strap. The strapping head includes an advancing apparatus and tensioning apparatus having at most three rollers for transferring an advancing motion, a retracting motion, and a tensioning motion to the strap. A least one of the wheels is operatively connected to a driving apparatus to cause the at least one of the wheels to rotate about a rotational axis for the advancing, retracting, and tensioning motions. The rollers can be brought in contact with the strap in pairs on both sides of the strap in different combinations with each other.

Abstract: Herein described is a system and method for packaging packages (C), comprising the steps of: forming a row of packages (C) advancing, one following the other, along a pre-set advancement direction (A), picking up at least two first packages (C) from the row, superimposing each of said first packages (C) on a respective second package (C) of the row, releasing each of the first packages (C) resting on the respective second package (C), obtaining at least two stacks of packages, each of which comprises at least two mutually superimposed packages (C) and stabilising the stacks of packages (C).

Abstract: The present disclosure relates to a method of attaching a shrinkable label on at least one product wherein the shrinkable label comprises a film comprising heat shrinkable material and photothermic material, the method comprising: transporting a plurality of products on a product conveyor through an irradiation volume defined by a plurality of UV light emitters arranged sideways of the product conveyor; arranging at least one reflector between consecutive products on the product conveyor while the at least one product is being transported; controlling the UV light emitters to emit UV-light towards the shrinkable label arranged around the at least one product in the irradiation volume and towards the at least one reflector arranged between consecutive products in order for the photothermic material of the shrinkable label to heat up causing the heat shrinkable material to shrink around the at least one product.

Abstract: A method for packaging solar mounting attachments by forming a package box having a first end and a second end, sealing the first end of the package box, placing attachment brackets into compartments defined by dividers in the package box, placing a container of fasteners onto at least one of the attachment brackets, and placing flashings onto at least one other attachment bracket. The flashings, the container of fasteners, and attachment brackets may be removed from the package box from the second end in the order of flashings, the container of fasteners, and attachment brackets.

Abstract: A box has a total inner volume in a closed configuration. The box includes a first box portion that defines a first inner volume and a second box portion that defines a second inner volume. The second box portion is pivotally coupled to the first box portion along a clamshell hinge. The first and second inner volumes combine to provide the total inner volume with each of the first and second inner volumes providing at least 30 percent of the total inner volume. The first box portion and the second box portion are each formed from a unitary sheet of sheetstock material. The clamshell hinge is a living hinge formed in the sheetstock material.

Abstract: A foldable container blank includes at four side walls, a top panel foldably connected to one of the side walls, a bottom panel foldably connected to one of the side walls, and at least one internal support structure that is connected to one of the side walls. Each internal support structure includes a first portion that is in adjacent relation with the top panel when the container is in a closed condition, and a second portion that is in adjacent relation with the first portion when the container is in a closed condition. In some embodiments, the foldable container blank is integrally formed. A method of forming the foldable container blank and a method of folding a container blank are also provided.

Abstract: A box includes a lid having a handle, wherein the handle comprises at one end thereof a toggle, and wherein a wall of the box comprises an opening through which the toggle of the handle is received for securing the lid in a closed position. Also disclosed is the combination of a box, a handle, and a clip, wherein the clip is secured onto a front wall of the box and a toggle of the handle is latched onto the clip for securing the lid of the box in a closed position.

Abstract: A corrugated box container with a main component including a base section and first and second side sections. The box container additionally includes first and second side support components associated with the first and second side sections for reinforcing the first and second side support sections. The box container further includes a cover component that is capable of engagement with the main component or the first and second side support components, such that the main component and the cover component present a fully enclosed space within the box container. The box container is erected from a knockdown configuration by folding the first and second side sections until the side sections are generally perpendicular with the base section; connecting the first and second side support components with the first and second side sections respectively; and connecting the cover component with the main component or the first and second side support components.

Abstract: The present invention relates to a composite container comprising a bottom film layer and a top film layer at least partially adhered to the bottom film layer. The top film layer is scored to form at least one resealable flap and at least one pull tab which is not adhered to the bottom film layer. The bottom film layer comprises at least one cavity opening. A cardboard layer is adhered on its lower surface to the upper surface of the top film layer, wherein the cardboard layer has at least one cavity opening which is substantially aligned with the scoring of the top film layer resealable flap and the cardboard layer is perforated to define a perimeter of at least one pull tab which is substantially aligned with and adhered, on its underside, to the upper surface of the top film layer pull tab.

Abstract: A pop top lid encloses a cylindrical fluid container. The pop top lid includes an end shell having an off-center scored line defining a tear panel; and a stay-on tab assembly riveted through a central portion to the end shell for rotation. An aperture point is attached to a central portion and rotatably positioned proximate to an inner edge of the scored line. A shearing edge is attached to the central portion and radially extending behind the aperture point. An actuator portion is attached to the central portion opposite to the aperture point, is liftable as a first-degree lever to form an aperture at the scored line with the aperture point, and is rotatable to insert the shearing edge into the aperture shearing the scored line to remove the tear panel from the end shell.

Abstract: A dispenser (10) for dispensing a flowable material M has a container (12) having an outer wall (20) and membrane (14) collectively defining a first chamber (22) configured to contain the flowable material M. The membrane (14) has a thickness and a weld seam (40) wherein the weld seam (40) has a thickness less than the thickness of the membrane (14). A fracturing mechanism (16) is operably connected to the container (12). The fracturing mechanism (16) has an extending member (64) projecting from the outer wall (20) of the container (12). The extending member (64) has a projection (66) positioned proximate the membrane (14), wherein in response to deflection of the extending member (64), the projection (66) deflects the outer wall (20) proximate the membrane (14) wherein the weld seam (40) fractures creating an opening (41) through the membrane (14) configured to allow the flowable material M to pass therethrough and from the dispenser (10).

Abstract: In some embodiments, apparatuses and methods are provided herein useful for reusable containers and item delivery using reusable containers. In several embodiments, the reusable containers described herein include removable divider walls that can be used to selectively divide an interior of the container into multiple smaller portions. By a further approach, the container and divider walls can have cooperating components to mount the divider wall to the container. In some embodiments, the reusable containers described herein can also include bag handle holding features so that bags placed therein are prevented from spilling contents during transport.

Abstract: Disclosed herein is a movable platform (MP) for moving freight during cross-dock operations. The MP comprises a mechanical actuation assembly used to deploy a plurality of roller assemblies used for moving the MP. Also disclosed is an actuating attachment used to deploy the mechanical actuation assembly of the MP. The actuating attachment can be attached to a conveyance vehicle, such as a forklift, or built in to an automated guided vehicle.

Abstract: A container having a center portion and two side portions each situated at an angle to the center portion and extending in opposite directions such that the a left half of the container is substantially identical to a right half of the container. The container includes recesses and protrusions which enable the container to stack in two orientations generally perpendicular to each other.

Abstract: A portable deployable container system has structural elements, including a base, a cover, and a set of panels, which can be manipulated into at least two container configurations. In one configuration, a container is formed by releasably securing the cover to the base to define a first volume. Some or all of the panels may be enclosed within such first volume, defining an undeployed configuration for the system. A second configuration involves removably securing some or all of the set of panels to the base and enclosing the panels with the cover, thereby deploying the system and forming a second, deployed configuration enclosing a volume larger than the first volume. Interconnections between the structural elements benefit from duckbill connections which add strength to the configurations by receiving flanges of first elements into corresponding channels of second elements formed by flared walls on such structural elements.

Abstract: The present disclosure provides a container with an increased movable range of an upper wall with respect to a side wall. According to the present disclosure provided is a container including a side wall, an upper hinge member, and an upper wall, wherein the upper hinge member and the side wall are connected rotatably around a first rotation axis, the upper hinge member and the upper wall are connected rotatably around a second rotation axis, and the first and second rotation axes are parallel.

Abstract: Provided is a handle including an annular part configured to fit in a neck part of a container, a first extension part provided so as to be continuous with the annular part, and a first holding part provided so as to be continuous with the first extension part, in which the annular part includes a second contact part capable of coming into contact with a first contact part provided to the neck part, and the first extension part is configured to be positioned with respect to the container by the contact between the first contact part and the second contact part.

Abstract: A selectively removable wall portable container assembly that includes a portable container body and a detachable lid capable of selectively removably coupling to one another and achieving a retained configuration. The portable container body includes a bottom wall coupled to sidewall enclosing the bottom wall, defining a container cavity. The sidewall defines a front opening spatially coupled to the container cavity and includes a selectively removable sidewall portion that superimposes the front opening and is operably configured to translate along a sidewall translation path. The assembly achieves an encapsulated configuration wherein the container cavity is encapsulated by the lid, bottom wall, and sidewall. Further, the assembly achieves a container cavity access configuration wherein the lid is coupled to the container body and the sidewall portion is at least partially slidably removed from the sidewall, exposing the front opening.

Abstract: A method for providing a passivation layer or pH protective coating on a substrate surface by PECVD is provided, the method comprising generating a plasma from a gaseous reactant comprising polymerizing gases. The lubricity, passivation, pH protective, hydrophobicity, and/or barrier properties of the passivation layer or pH protective coating are set by setting the ratio of the O2 to the organosilicon precursor in the precursor feed, and/or by setting the electric power used for generating the plasma. In particular, a passivation layer or pH protective coating made by the method is provided. Pharmaceutical packages coated by the method and the use of such packages protecting composition contained in the vessel against mechanical and/or chemical effects of the surface of the package without a passivation layer or pH protective coating material are also provided.

Abstract: A pour spout has a spout section with an elongate tubular body defining a liquid flow channel. The body has a fluted or corrugated configuration rendering the body flexible or bendable. A dispensing orifice is disposed at a dispensing end of the pour spout and an attachment end is disposed at an end of the body opposite the dispensing end. The attachment end has a liquid inlet orifice. A vent section of the pour spot is joined to the attachment end of the body. The vent section includes an air vent that defines an air flow path, which directs air from outside of the pour spout along the air flow path toward a container interior while bypassing the liquid flow channel.

Abstract: A packaging structure with patterns formed through continuous multi-color hot foil stamping includes a packaging portion consisting of a receiving unit and a bottom panel, and a pattern portion located on an outer surface of the packaging portion and including continuous multi-color hot foil stamped areas. The receiving unit internally defines at least one holding space and has a first and a second opening respectively formed at a top and a bottom thereof and communicable with the holding space. The bottom panel is an integral one-piece member connected to the bottom of the receiving unit to close the second opening. The one-piece bottom panel allows the bottom of the packaging portion to have a flat and seamless middle area and accordingly, increased overall structural stability. Since the pattern portion includes continuous multi-color hot foil stamped areas, it can be formed in a quick, low-cost and aesthetic manner.

Abstract: A closure for a container neck comprises a shell and a fitment. The fitment comprises a body and engagement means that extend radially outwardly from the body and releasably retain the fitment within the shell. During application of the closure to the container neck, the engagement means is forced from an extended condition into a retracted condition to release the fitment from the shell, and the fitment is inserted into the container neck into an operative position.

Abstract: A container lid assembly outfits a container includes a lower lid construction and a slider element. The slider element is received in the lower lid construction and is linearly displaceable in a back and forth manner relative to the lower lid construction for opening and closing the container lid. The lower lid construction includes concave surfacing and the slider element includes convex surfacing. The slider element seats atop the lower lid construction such that the convex surfacing and concave surfacing form a spherical surface-to-surface seal and enabling slidable open-close functionality. The slider element is resiliently actuable when seated atop the lower lid construction for enhancing seated engagement therebetween. The slider element includes a step-down formation cooperable with resilient actuation thereof for further enhancing seated engagement between the slider element and the lower lid construction. The container lid further locks to the container when in an actuated lower lid configuration.

Abstract: A cap for a variable pour flow device is configured to close an opening of a container holding a liquid when assembled with the container. The cap includes a spout in communication with an interior of the container when the cap is assembled with the container. The cap is further configured to provide a first fluid flow in which fluid flows through a first passage and the spout when the container with the cap assembled thereto is tilted from an upright position toward the spout to an intermediate degree. The cap is also configured to provide a second, greater fluid flow in which fluid flows through the first passage, a larger second passage, which is spaced from the first passage, and the spout when the container with the cap assembled thereto is tilted further toward the spout from the intermediate degree.

Abstract: A portable water filling system for a recreational vehicle is provided. The portable water filling system for a recreational vehicle includes a protective container having a first compartment and a second compartment. The first and second compartments are rotatably connected to each other. Each of the first and second compartments forms interior cavities. A first insulative element is positioned in the first compartment. The first insulative element has a first insulative cavity. A second insulative element is positioned in the second compartment. The second insulative element has a second and third insulative cavity. A pump is positioned in the first and second insulative cavities. A plurality of fluid conductive elements is positioned with the pump in the first and second insulative cavities. A bladder is positioned in the third insulative cavity. The first and second compartments are configured for rotation from a closed orientation to an open orientation.