Abstract: A method of manufacturing a shell component for an aircraft or spacecraft includes positioning a skin panel, which includes a skin of the aircraft or spacecraft and first and second stringers stiffening the skin, opposite a frame having first and second mouseholes for receiving the first and second stringers, elastically bending the skin panel, inserting the first stringer into the first mousehole, and releasing the elastic bend to insert the second stringer into the second mousehole.

Abstract: An aircraft flooring system for an aircraft fuselage adapted to secure a payload component may include first and second seat tracks extending longitudinally with respect to the aircraft fuselage, the first and second seat tracks being spaced from one another; and an intercostal assembly extending between the first and second seat tracks. The intercostal assembly can include a first intercostal having a center member having a first end and a second end and a top flange including a mounting region between the first and second ends; and at least first and second tab members. The first tab member can be coupled to the top flange toward the first end of the center member and the second tab member can be coupled to the top flange toward the second end of the center member. The first and second tab members can extend beyond the first and second ends of the center member, respectively, and be configured to be coupled to the first and second seat tracks.

Abstract: An aircraft rear structure comprising a substantially flat rear pressure bulkhead, with a first side and a second side, opposite to the first side. The aircraft rear structure also comprises a horizontal stabilizer and a vertical stabilizer which in turn comprises a first spar and a second spar. The first spar is attached to a first attachment zone of the second side of the rear pressure bulkhead via first attaching elements, and the second spar is attached to a second attachment zone of the second side of the rear pressure bulkhead via second attaching elements. The second attachment zone being different from the first attachment zone.

Abstract: The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in a manufacturing process to be reduced, and weight increases to be prevented. The fuel tank includes a structural member in which carbon fiber reinforced plastic (CFRP) is used, the carbon fiber reinforced plastic (CFRP) including a reinforcing material that includes carbon fibers and a matrix that includes plastic. The structural member is formed by laminating a conductive sheet between prepregs of the carbon fiber reinforced plastic (CFRP). In this case, a cut surface of the structural member formed by cutting the structural member may be exposed on the inside in which fuel is stored.

Abstract: An aerial vehicle includes a fuselage, a wing, and a wing shift device. The wing shift device is configured to be coupled to the fuselage. The wing shift device comprises a plurality of apertures for coupling the wing to the aerial vehicle. The plurality of apertures are configured to permit the wing to be shifted in a forward or aft direction along the fuselage based on a center of gravity of the aerial vehicle.

Abstract: A noise abatement system for an aircraft landing gear is provided. The system may have a retention member and a covering member. In this regard, the system may be configured to block the airflow through a structural void to abate noise. Moreover, the system may be shaped to diminish aerodynamic drag.

Abstract: Hub-mounted active vibration control (HAVC) devices, systems, and related methods are provided. An HAVC device (100) includes a housing (206) having a tolerance ring (600) attached to a rotary hub (702). The tolerance ring can accommodate dissimilar coefficients of thermal expansion between dissimilar metals. The HAVC device can also include a plurality of coaxial ring motors (308A, 308B, 310A, 310B) configured to rotate a plurality of imbalance masses for controlling vibration. An HAVC system can further include a de-icing distributor (208) for communicating instructions to one or more heating sources (HS) provided at one or more rotary blades (802) of a vehicle or aircraft. A method of controlling vibratory loads occurring at a moving platform can include providing a moving platform, mounting a vibration control device to a portion of the moving platform, and rotating at least one pair of imbalance masses such that the combined forces of the masses substantially cancel unwanted vibration of the platform.

Abstract: An aircraft includes at least one propulsion engine, coupled to a fuselage, and configured to provide forward thrust to propel the aircraft along a first vector during forward flight. Each of at least two of multiple rotors coupled to the fuselage is coupled to a motor configured to supply power to that rotor and/or to draw power from that rotor. At least two of the rotors are configured to operate during forward flight to provide at least some lift to the aircraft along a second vector. A flight control system is configured to control the rotors that are configured to operate during forward flight in a power managed regime in which a net electrical power, consisting of the sum of the power being supplied to or drawn from each rotor by its motor, is maintained within a range determined by a feedback control system of the flight control system.

Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.

Abstract: An aerial vehicle adapted for vertical takeoff and landing using pivoting thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to takeoff with thrust units providing vertical thrust and then transitioning to a horizontal flight path. An aerial vehicle with pivoting thrust units with propellers, wherein some or all of the propellers are able to be stowed and fully nested during forward flight. An aerial vehicle adapted to withstand impacts upon its propellers. An aerial vehicle able to quickly alter the thrust of its propellers.

Abstract: Disclosed herein is a system and method for controlling the takeoff and landing of a drone. The system for controlling the takeoff and landing of a drone includes: a landing control device configured to vary the transmission range of Low Frequency (LF) landing control signals based on whether a response signal to a transmitted landing control signal in the transmission range is received, and to transmit a landing signal if the varied transmission range is less than a minimum radius; and a drone configured to fly in a control signal-based flight mode based on a landing control signal when receiving the landing control signal transmitted from the landing control device during GPS signal-based flight, and to land at a destination by flying in a landing mode when receiving a landing signal from the landing control device during flight in the control signal-based flight mode.

Abstract: 1. Method for controlling a flying body for cleaning surfaces 2.1. Flying bodies can cover large distances between arrangements of smooth and curved surfaces without requiring manual manipulation. This reduces personnel requirements and enables large surfaces to be maintained, for example solar power stations, in a fully automated manner. 2.2. The method for controlling a flying body for cleaning surfaces consists of detecting the surrounding surfaces of an object to be cleaned, directing the flying body with respect thereto and structuring the flight path. As a result, the surface can be cleaned particularly efficiently and, if needed, worked on further. 2.3. Said method for controlling a flying object for cleaning surfaces is suitable for use on glass facades or on solar power stations, particularly in arid regions.

Abstract: Aspects of the disclosure include a method, system, and computer program for delivering a product. The method includes determining a delivery location and time for a payload using an aircraft. A recipient is notified of the delivery location and time. A first signal is received from the recipient. The time or location of the delivery location and time is changed, dynamically, based on the first signal. The payload is delivered to the recipient.

Abstract: A bleed air pressure regulation system for an aircraft anti-icing system comprises a first, upstream pressure regulating valve and a second, downstream pressure regulating valve arranged in series in a bleed airflow path. The respective pressure regulating valves each have a regulating pressure chamber in fluid communication with a respective pressure setting valve. Each pressure setting valve is in fluid communication with a bleed air inlet upstream of the first, upstream pressure regulating valve. The first, upstream pressure regulating valve is set to regulate the pressure of the bleed air to a first pressure and the second, downstream pressure regulating valve is set to regulate the pressure of the bleed air to a second pressure which is higher than the first pressure.

Abstract: The present invention provides a windshield device including: a windshield; a heater that is provided in the windshield and configured to generate heat by energization; a temperature sensor that is provided in the windshield and configured to detect a temperature; and a control unit that performs power control on the heater. The control unit is configured to supply an input power to the heater, the input power being acquired by applying a detected temperature detected by the temperature sensor to a function that is determined in accordance with a dew-point temperature of an inside of a compartment separated from an outside of the compartment by the windshield.

Abstract: An aircraft system comprising a deflector assembly including, a base having mounting apertures; an inner ring concentrically positioned within an outer ring, the inner ring and the outer ring have an annulus defined therebetween via a base plate, a plurality of rods attached within the annulus and culminating at an apex creating a conical profile; and a forward-mounted cone-shaped deflecting member. The base plate comprises a through hole allowing airflow through the deflector assembly to supply an airplane engine. The aircraft safety device system further comprises at least one locking latch for removably securing the deflector assembly to a housing of the airplane engine. The aircraft safety device is mountable inside a lip of the housing of the airplane engine. Further, the aircraft safety device provides protection for airplane engines from air born animate and inanimate objects.

Abstract: A mounting apparatus includes a cradle, a stand, a cradle attachment member, and a rotation member. The cradle includes an electronic display attachment member which is configured to removably attach an electronic display to the cradle. The cradle attachment member is configured to removably attach the cradle to the stand. The rotation member is configured to allow rotation of the electronic display when it is attached to the electronic display attachment member.

Abstract: A mobile helicopter landing pad comprises a platform with one or more elongate, concave guiding channels for aligning a helicopter on the landing pad by forcing the helicopter's skates into a specific alignment upon landing. The guiding channels may have laterally disposed rollers or else be made of slick material to allow the helicopter to slide towards the base of the guiding channel under the helicopter's own weight. Additional crosswise rollers at the bottom of the guiding channel(s) may be provided to allow the helicopter to be moved forward or backward after landing. A blade locking arm swings upward and secures the top rotor. The pad may include a foldable enclosure that protects the helicopter after landing, and an electronic guidance system that assists the pilot during landing by providing instructions to the pilot or visual indications of the prevailing wind direction and velocity, through illuminated signals on the platform.

Abstract: Systems, devices, and methods for impacting, by a small unmanned aerial vehicle (SUAV), a net having at least three sides; and converting the kinetic energy of the SUAV into at least one of: elastic potential energy of one or more tensioned elastic cords connected to at least one corner of the net, gravitational potential energy of a frame member connected to at least one corner of the net, rotational kinetic energy of the frame member connected to at least one corner of the net, and elastic potential energy of the frame member connected to at least one corner of the net.

Abstract: An apparatus and method for installation of a frame assembly to a body may include a tooling assembly configured to support a frame assembly, the tooling assembly being positioned with respect to a body, wherein the frame assembly is positioned with respect to the body at a plurality of predetermined engineering locations.

Abstract: An apparatus for automatically mounting and dismounting an aircraft fuselage includes stages disposed to be spaced apart from each other, positioners disposed between the stages and on which a plurality of fuselage parts are mounted, the positioners adjusting a position of each of the mounted fuselage parts in X, Y, and Z directions, and a transfer unit allowing the fuselage parts to be automatically respectively mounted on the positioners, the transfer unit automatically dismounting the assembled fuselage from the positioners to transfer the assembled fuselage after the fuselage parts are completely assembled with each other. The apparatus may automatically mount and dismount the fuselage to reduce assembly time, thereby improving productivity of the fuselage, assembly quality and workability.

Abstract: Systems and methods are described herein for mounting a thruster onto a vehicle. A thruster mounting structure may comprise a first, second, and third rotational joint, a boom, and thruster pallet, and a thruster attached to the thruster pallet. The first rotational joint may be attached to the vehicle and configured to rotate in a first axis. The first rotational joint may be connected to the boom and configured to pivot the boom about the first axis. The boom may be connected to the second rotational joint, which is connected to the third rotational joint and configured to rotate the third rotational joint in the first axis. The third rotational joint may be connected to the thruster pallet and configured to pivot the thruster pallet in a second axis that is perpendicular to the first axis.

Abstract: A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.

Abstract: The use of an accelerometer for inertial navigation of a low thrust spacecraft undergoing acceleration wherein the inaccuracy of the accelerometer is less than the uncertainty in the accuracy of a modeled non-gravitational component of the acceleration that the spacecraft is undergoing is disclosed. A method of navigating a spacecraft having a low thrust propulsion system is also disclosed. The method comprises engaging the low thrust propulsion system, measuring the acceleration of the spacecraft using an accelerometer with an inaccuracy less than the uncertainty in the acceleration imparted by the low thrust propulsion system and acquiring a trajectory estimate using the measured acceleration. The trajectory estimate may be updated using an external reference navigation sensor.

Abstract: A flexible bag and a method for filling a flexible bag which is collapsed when empty, wherein at least one fastening means is provided on a surface of the flexible bag such that at least two upper parts of the flexible bag can be held together by this at least one fastening means during a first part of filling of the flexible bag, whereby the fastening means is designed to release when the bag is filled to a certain amount such that the two upper parts being held together by the fastening means will lose contact.

Abstract: An electronic cigarette and fluid dispensing system (E-Cig FDS) that utilizes an electronic cigarette (e-cig) having an inner end, an outer end, and an outer surface with a first aperture and a second aperture, and a keyed fluid dispenser having a body with an inner surface, an outer surface, an open first end, and a second end. Located within the body at the first end is a plunger that can slideably move inside the body. Extending from the body's second end is an injector dimensioned to interface with the first aperture or second aperture. The fluid facilitates the smoking, or vaping, of the e-cig. A user can selectively choose if the fluid is safe, non-nicotine or nicotine-infused. The E-Cig FDS provides visual differentiation of the type of fluid that is being smoked, or vaped.

Abstract: A method for transferring a viscous material from a container into a dispensing syringe having first and second ends, the second end being a discharge port smaller than the inner diameter of the main body portion, includes inserting into the syringe a plug configured to permit gas flow in only one direction to divide a chamber within the syringe into a first sub-chamber in communication with the discharge port and a second sub-chamber in communication with the first open end of the syringe. Then, a rod is inserted into the syringe from the first open end of the syringe to engage the plug, and the viscous material is extruded from the container and through the discharge port into the first sub-chamber of the syringe. While the first sub-chamber is being filled with the viscous material, the plug and the rod are moving away from the discharge port.

Abstract: A device for filling and closing disposable bags for containing banknotes comprises an upper container for temporarily housing banknotes, provided with a bottom with an opening for the exit of the banknotes from the container, a piston for pushing the banknotes towards the opening on the bottom of the container, a bag made of flexible plastic film, intended to be filled with the banknotes temporarily housed in the container, a support for the bag containing the banknotes, vertically movable through controlled lowering means and placed below the container, sealing bars arranged between the upper container and the movable support, and an electromagnetic stop element that can be controlled to lock the movable support with respect to the sealing bars, said electromagnetic stop element consisting of an electromagnet applied to the movable support and of a fixed element made of ferromagnetic material, adapted to face the electromagnet in operative condition.

Abstract: An ultrasonic sealing tool including an anvil with a sealing surface, a horn with a sealing surface facing the sealing surface of the anvil, the sealing surface of the anvil including a plurality of beads including a first bead having a first height and at least one second bead having a second height, the second height being less than the first height, the ultrasonic sealing tool delivering ultrasonic vibrations via at least one of the anvil and the horn to create a closure seal in a work piece positioned between the anvil and the horn, the closure seal including a first seal created by the first bead and at least one second seal created by the at least one second bead, the first seal having a weld depth greater than a weld depth of the at least one second seal.

Abstract: Packing machine and packing method for producing an inner container of a slide-open package of tobacco articles by folding an inner blank about a wrapped group of tobacco articles; the inner blank is folded, by way of first folding means, so as to form a hinged lid; in a feed station, the partly folded inner blank is coupled to the wrapped group of tobacco articles so that a rear wall of the wrapped group of tobacco articles rests on a panel of the inner blank corresponding to a rear wall of the inner container; and the inner blank is folded, by second folding means arranged downstream from the feed station, about the wrapped group of tobacco articles to complete the production of the inner container.

Abstract: In the method for transferring at least one item to be packaged into a container and for transporting the filled container onward the at least one item to be packaged is conveyed in a conveying direction to a transfer position by a linear motor transport device. The at least one item to be packaged is then moved from the transfer position to an intermediate storage area, which is arranged next to the transport device. A container is conveyed in the conveying direction to the transfer position by the linear motor transport device, and the at least one item to be packaged is moved back from the intermediate storage area to the transport device, thus filling the container. Afterwards, the filled container is moved onward in the conveying direction by the linear motor transport device.

Abstract: Electron beam generator comprising an electron emitting device adapted to emit an electron beam when heated to an elevated temperature, wherein the electron emitting device comprises a filament having a spiral portion.

Abstract: A method for the production and filling of packaging includes unwinding flattened tubular film material from a roll along a primary axis of symmetry thereof, providing the tubular film material via a welding and separating process with a first lateral welding seam perpendicular relative to the axis, and separating the tubular film material along a separation line to provide a hose section. The hose section open at one side is filled, and the still open other side of the hose section is provided with a second lateral welding seam. Two subsequent separation lines are inserted in the hose section at a distance that is less than the distance between the two edges of the hose.

Abstract: An apparatus for attaching a label to a moving cable, the apparatus comprising: an attaching device for applying a label onto a moving cable and a roller for pressing the label against the moving cable, wherein the roller comprises a first roller for pressing one label against the moving cable, wherein the first roller comprises a U shape hollow portion and is mounted at an angle with the U shape hollow portion directly facing a side of the moving cable and wherein the label is formed into a U shape a first edge of the U shape longer than a second edge of the U shape; a first roll down roller for folding the second edge of the label against the moving cable and the first edge of the label; and a second roll down roller for folding the first edge of the label against the folded second edge of the label and wherein the first roll down roller is mounted to overlap the second roll down roller to overlap the label edges onto the moving cable.

Abstract: A vessel is configured to hold a product in an interior region formed in the vessel. In illustrative embodiments, the vessel includes a floor and a sidewall coupled to the floor to extend away from the floor. Together the floor and sidewall cooperate to define the interior region.

Abstract: A resin container of the invention is the resin container capable of storing a predetermined amount of fluid having flexibility, the resin container including a first surface part formed with an inlet/outlet part for the fluid, a second surface part connected to the first surface part and forming a peripheral surface, and a third surface part arranged at an opposite side of the first surface part and connected to the second surface part, wherein the first surface part is formed with a first recess recessed from the first surface part toward a third surface part side, and the second surface part is formed with a second recess recessed toward the center of the container from the first surface part to the third surface part.

Abstract: A blank for forming a carton, the blank including a first panel and a second panel adjoining the first panel along a fold line and extending in a longitudinal direction of the blank. A pair of side panels adjoins the second panel at respective fold lines. The side panels extend from the second panel in a transverse direction of the blank. The side panels each having a side panel flap adjoining at a fold line, the side panel flaps extending from the side panels in the longitudinal direction of the blank, toward the first panel. The blank further includes a third panel adjoining the second panel along a fold line and extending in the longitudinal direction of the blank. The blank further includes a fourth panel adjoining the third panel along a fold line and extending in the longitudinal direction of the blank.

Abstract: A toy figure display stand displays a toy figure behind a transparent fluid-retaining wall, thus simulating immersion of the toy figure within the transparent fluid. The simulated immersion provides an additional level of engagement between the toy figure and a child or collector. The wall may include an interior transparent shell portion and an exterior transparent shell portion. The interior transparent shell portion and the exterior transparent shell portion may together define a cavity. A fluid may be received within the cavity.

Abstract: A material-supporting cartridge comprises a frame having an upper surface with an opening, and a pin removably positioned in the opening in a first orientation with a first end of the pin positioned in the frame and a second end of the pin positioned a first height above the upper surface. The pin is dimensioned to be removed and inserted into the opening in a second orientation with the second end of the pin positioned in the frame and the first end of the pin positioned a second height above the upper surface, the first height being greater than the second height. The frame further includes a support tube dimensioned to receive the pin in each of the first and second orientations. The material-supporting cartridge can be used with a rack that defines multiple stacked rows having a vertical spacing between adjacent rows, the vertical spacing being greater than the second height.

Abstract: An insulating container having a base and a lid is provided. The lid may be rotatable about a hinge from a closed configuration to an open configuration and may be secured, via one or more latching devices, in either the closed configuration or the open configuration. In some examples, the rotatable lid may be non-destructively removable from the base. Some example arrangements include a removable lid that, when removed, may be secured to the base via an additional portion of the latching device. Additional features of the insulating container include handles that are integrally formed with the base, a recess formed in the base and housing a spigot, and/or a spigot guard.

Abstract: A lid hanging structure of a container is disclosed in the present invention. The container includes a base, side plates and a lid. the hanging structure includes hanging members and hanging slots, wherein the hanging members are engaged or disengaged with the hanging slots respectively so as to hang the lid on the container or remove the lid from the container, and one of the anging members and the hanging slot is provided on the lid and the other is provided on the side plates. According to the lid hanging structure, it is convenient to remove the lid from the container when necessary. That is to say that, the lid can be removed directly when not in use or in the hanging state, and can be removed by simple operation in the hanging state, so as to reduce the amount of labor, and the structure is simple and the cost is low.

Abstract: In one example, a lid configured for use with a container includes an upper surface that is generally circular in shape, and further includes a side wall with an annular configuration, the side wall intersecting the upper surface to define an edge of the lid. A grip element is defined in the upper surface and sized and configured to be grasped by one or more fingers of a user, and the grip element includes a grip portion that is set back a distance from the edge of the lid. Finally, a tab is provided that is attached to the side wall of the lid by an elastically deformable standoff element.

Abstract: A discharge apparatus for use with a bulk container of the kind having an outlet through which product is to be dispensed. The apparatus has an inlet end, an outlet end and a wall extending between said inlet end and said outlet end. The apparatus is configured for directing a flow of product from an outlet of a bulk container, and is further configured to permit relative movement between said inlet end and said outlet end between a retracted position and an extended position. The outlet end may take the form of a plate for supporting the lower end of the bulk container. The plate may be vibrated for assisting discharge of product from the bulk container.

Abstract: The present disclosure provides a container and a process for producing the container. In an embodiment, the process includes placing a sleeve bag on valve assembly (SBoV) in a blow mold apparatus. The blow mold apparatus has two opposing and movable molds. The SBoV has a valve seat. The process includes extending a parison of flowable polymeric material around the SBoV and between the opposing molds. The process includes moving the opposing molds to a closed position and pressing an upstream portion of the parison against the valve seat. The process includes blow molding a downstream portion of the parison into a container-shape within the closed mold. The process includes forming a container with the valve seat melt bonded to a neck portion of the container.

Abstract: A child resistant closure for use on a container that include an inner closure member having a threaded portion and an inclined surface, and an outer closure member coupled to the inner closure member for axial translation therebetween. A series of engagement features extend between the inner and outer closure to permit selective engagement of the outer closure to the inner closure to effect removal of the child resistant closure. The outer closure includes at least one finger spring member being inwardly directed and contacting the inclined surface of the inner closure member, thereby biasing the outer closure member into an operationally disengaged position. The finger spring member T-shaped in cross-section.

Abstract: Provided are: a lid capable of capturing a foreign substance from a liquid crystal material in advance before the liquid crystal material is used; and a method of capturing a foreign substance. In a lid (20) including a bottom part (22) closing an opening on one end of a circumferential part (21) having a tubular shape is provided and a circumferential part (21) placed over a tubular part having an opening of a container provided at the container, the bottom part (22) covering the tubular part, the lid further includes a partition board (211) provided at an inner surface of the circumferential part in a slanted direction against the bottom part (22) and dividing the inside of the circumferential part (21) into a first space proximal to the bottom part (22) and a second space apart from the bottom part (22), and a connection part (213) which connects the first space with the second space being provided at a portion of the partition board (211) closest to the bottom part (22).

Abstract: A tamper-evident device for valves comprises: an anti-theft buckle (1), provided with an anti-theft buckle body (17), a pulling portion (4), a tearable portion (5), an elastic hook (7), and a position limiting surface (6); an anti-theft cover (2), provided with a position limiting contour (8) and a hook receiving portion (9); and a position limiting slot (10) provided at a passage outlet (13) of a valve body (3). During use, the anti-theft cover (2) is connected to the passage outlet (13), and the elastic hook (7) is hooked to the hook receiving portion (9) and fitted to position limiting slot (10) to limit relative positions of the anti-theft cover (2) and the valve body (3). Also disclosed is a valve having the temper-evident device. The temper-evident device is easy to open and can effectively prevent stored materials from being stolen.

Abstract: A patterned thermoplastic elastomer (TPE) film for fabricating a liquid-filled blister, has a blister-sized cavity in fluid communication with a microfluidic channel via a gating region.

Abstract: A kit for supporting and multi-directionally aiming a heat source. The kit includes a heat air gun, a tripod, and an extension arm. At least one of the tripod and the extension arm support the heat air gun so as to allow the heat air gun to be supported while having multi-directional aiming.

Abstract: A packing and/or transport unit comprising several insulation elements for flat roof insulation, wherein each insulation element has four side faces being arranged rectangular to each other, a lower surface and an upper surface, the lower and upper surfaces being connected to the side faces and being arranged spaced apart and non-parallel to each other. The insulation elements are arranged in layers in at least one stack on at least one support means being arranged under the stack, which support means comprises at least two carrying feet arranged for resting on a support surface. The stack comprises an uneven number of layers of insulation elements, and the packing and/or transport unit comprises at least one leveling means ensuring that a top plane of the packing and/or transport unit is arranged substantially parallel to the support surface.