• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:

    公开号:DK200800051U1
    申请号:DK200800051U
    申请日:2008-03-18
    公开日:2008-04-11
    发明作者:Lars Thoegersen
    申请人:Rasn As；
    IPC主号:
    专利说明:

    DK 2008 00051 U3
    Aircraft loading and unloading apparatus
    Description
    Technical area
    The invention relates to an apparatus as claimed in the preamble of claim 1.
    When loading and unloading smaller aircraft, such as DC 9s, MD 80s and Boeing 737 and so on (the so-called narrow body aircrafts), it is well known that the work on this is very burdensome for the personnel concerned, This is because that is often very short time available and that the cargo compartment is of such a small size that the person in question must lie on his knees or sit down inside the cargo compartment while handling the luggage. The risk of physical injury is therefore relatively high.
    Several proposals have been made to facilitate this work. A condition for the use of any kind of auxiliary equipment is usually that it must be removable from the aircraft when the loading and unloading work is completed, as it cannot be left in the aircraft due to its weight. At the same time, the auxiliary equipment must be able to move in and out of the aircraft relatively quickly due to the relatively short time available.
    From WO 98/54 073 an apparatus for use in manual loading and unloading of aircraft is known.
    This known apparatus comprises a telescopically constructed conveyor which is introduced into the cargo compartment and which has at the end a height adjustable table which is placed inside the cargo compartment and from which the unit goods are stacked. Outside the aircraft there is a conveyor belt which carries the piece goods up to the telescopically constructed conveyor part.
    2 DK 2008 00051 U3
    DK Patent No. 170,863 and US Patent No. 3,268,099 disclose a conveyor having a number of articulated units, each having a plurality of supporting rollers on the upper side. These support rollers are carried by transverse shafts and on the underside with wheels on which the units can roll on a support. A number of these articulated units are pulled into the aircraft cargo compartment from a storage compartment beneath a belt conveyor located outside the aircraft.
    US Patents Nos. 6,006,893 and 2,990,938 disclose apparatus comprising a conveyor which, however, is unsuitable for being introduced into a cargo hold in an aircraft from a position under a tiltable conveyor.
    Brief description of the production
    The object of the present invention is to provide an apparatus which is relatively simple in structure and which allows for relatively easy insertion and removal of cargo from an aircraft's cargo compartment and at the same time ensures easy and continuous movement of the luggage.
    This is achieved by the measures specified in the characterizing part of claim 1.
    Hereby it is achieved that it is relatively easy to handle the extendable second conveyor, while at the same time allowing easy and continuous movement of the cargo, because the individual conveyor units roll on top of the cargo floor in the direction towards and away from the relevant loading point within the cargo space, and because the conveyor units are adapted to assist with their own propellants in the movement of the piece goods.
    According to the invention, the conveyor paths of the first and second conveyor portions, respectively, can extend in succession and the interconnected conveyor units can be at least partially included in the conveyor paths of both conveyor units because they proceed directly over each other. from the first to the second conveyor part during the extension or retraction of the second conveyor part. The resulting total conveyor path of the apparatus runs relatively unbroken and flat.
    According to an expedient embodiment of the invention, the first conveyor portion may comprise an endless conveyor belt whose conveyor path is longitudinally adjustable according to the extension or retraction of the conveyor units.
    In addition, the apparatus according to the invention may have a bridge through which the conveyor units of the second conveyor part are transferred between the apparatus and the aircraft. The bridge also ensures a smooth transition between the device and the aircraft.
    According to the invention, the endless conveyor belt's endless conveyor belt will particularly preferably extend between a front facing aircraft positionable reversing device and a rearward reversing device, the first conveyor portion having an intermediate forward and backwardly displaceable diverting device through which the conveyor belt is routed from a straight line, extending between the rear reversing device and the diverting device, to an intermediate path extending parallel to the upper path, but at a level below it, between the diverting device and the front reversing device, whereby the conveyor belt between the front reversing device and the rear reversing device is extending the upper and intermediate lanes, whereby the upper lane forms at least a portion of the first lane of the first conveyor portion, thereby connecting the rear end of the plurality of conveyor units with the first conveyor part redirection device and thus arranged to be moved back and forth with it, the transport units moving over the intermediate path of the first conveyor part when outside the aircraft, thereby being obtained in a simple manner, that the conveying paths of the first and second conveyor parts can be substantially unbroken at the same time while simply providing space for the number of conveyor units or the rear part thereof when all or the rear part thereof is not within the plane.
    According to the invention, the apparatus may conveniently have a support device for supporting the endless conveyor belt of the first conveyor part during its movement within the upper web.
    Particularly conveniently, according to the invention, the conveying paths of both transport members can be formed by means of the conveyor units over their entire length. In addition, the apparatus according to the invention may have a magazine for accommodating the rear end of the number of conveyor units, these being arranged in order to be able to be carried out or into the magazine, depending on how far the front end is to be inserted into the aircraft. This allows the number of conveyor units to be easily adapted to the length of the aircraft type cargo space.
    In addition, the first conveyor portion may comprise an endless conveyor belt and may be arranged above the path of the conveyor units to an area adjacent to the bridge, with the result that it is possible to limit the number of conveyor units and, consequently, the cargo space capacity of the apparatus.
    According to the invention, the front of the conveyor units may comprise a rearwardly rotatably mounted conveyor flap, which can be applied by means of propellants at a desired inclination to the plane in which the other conveyor units operate. This opens the possibility for the operator to place the front end of the conveyor flap at a desired level next to the stack of goods with which work is being done inside the aircraft at that time.
    In this connection, according to the invention, the conveyor flap at the front end furthest away from the hinge site may also have a hinge-mounted conveyor front which can be adjusted with a desired inclination with a desired inclination in relation to the conveyor flap's delivery plane.
    This opens the possibility for the operator to place the front part in a plane that best fits the appropriate trajectory of the luggage piece into or out of a stack.
    According to the invention, each conveyor unit may comprise an endless conveyor belt driven by a drive roller and a plurality of other rollers, all supported by a frame which is in turn supported by a wheel supporting support device. This makes the individual conveyor unit particularly simple.
    According to the invention, the conveyor flap of the front conveyor unit can be formed by the frame and the associated conveyor belt and can be pivotally mounted on the wheel supporting support device and its propellants may be a plurality of electric driven actuators. This is achieved in a simple way that the front conveyor unit can be moved back and forth within a cargo hold, even though the conveyor flap is disposed with a slope relative to the floor of the cargo compartment.
    Furthermore, according to the invention, the conveyor flap can project farther than the associated support device, seen in the conveying direction of the second conveyor part during loading, and at the same time according to the production, the conveyor front of the conveyor flap may have wheels for supporting the conveyor flap and the conveyor front part when in the folded-down state. This ensures that an operator can easily fit his legs under the conveyor flap when placed in an inclined position.
    6 DK 2008 00051 U3 When the conveyor front part is folded down in turn, the front part wheels ensure that the flap is supported and easily maneuverable together with the other conveyor units.
    Particularly conveniently, according to the production at the front end of the second conveyor part, a control device may be provided which is connected to all the propellants of the apparatus, so that an operator present within the aircraft can control these by actuation of the control device. This ensures that the operator has effective control over both conveyor parts.
    According to the invention, the conveyor units can be connected to each other by means of releasable coupling devices, whereby the conveyor units can be easily replaced and their number adapted to the conditions in question if desired.
    Furthermore, according to the invention, the bridge may comprise guiding means for guiding the second conveyor part during the entry into and execution from the cargo hold. In this way, this guide can be made relatively easy.
    Furthermore, according to the invention, at least some of the conveyor units' coupling devices may be arranged so that adjacent conveyor units can be displaced relative to each other across the conveying direction so that they can more easily adapt to conditions within the cargo space.
    Particularly conveniently, the conveyor front portion of the front conveyor unit, in accordance with the manufacture, may comprise an endless conveyor belt with its own propellants.
    Finally, according to the invention, the apparatus may conveniently be located on a vehicle.
    7 DK 2008 00051 U3
    Brief description of the drawing
    The invention is explained in more detail below with reference to the drawing, in which fig. 1 is a schematic side view of a first embodiment of an apparatus according to the invention, with parts removed for clarity, and FIG. 1 is a side elevation of the first and second conveyor members, with the second conveyor member disposed in a fully extended position; FIG. 3 the same as FIG. 1, but with the second conveyor part disposed in a partially extended state; FIG. 4 the same as FIG. 2, but with the second conveyor part fully retracted relative to the first conveyor part; FIG. 5 is the one shown in FIG. 4 is a top plan view of FIG. 6 shows the same embodiment as in FIG. 5, viewed from above and in larger scale with parts removed for clarity; FIG. 7 is a side view of the embodiment of FIG. 6; FIG. Figs. 8-11 are schematic views of different stages of the apparatus during insertion of the second conveyor part into the cargo hold of an aircraft, seen from above; 12 schematically shows the apparatus with a bridge inserted through the opening to the cargo hold of an aircraft, but with the conveyor parts removed for clarity, 8 DK 2008 00051 U3 fig. Figures 13 and 14 show the front end of the second conveyor part, viewed from above and from the side respectively, in different operating states; 15 is a schematic perspective view of a conveyor unit which forms part of the second conveyor part with individual parts removed for clarity; FIG. 16 and 17 show the front end of the second conveyor part, shown schematically in use during loading and unloading, respectively; 18 and 19 are schematically a second embodiment of the invention, in which both the first and the second transport parts are formed by a continuous series of conveyor units, seen in the extended and retracted condition, respectively. 20 shows an apparatus according to the invention with a tiltable bridge; FIG. Fig. 21 is a perspective view of another embodiment of a conveyor unit included in the second conveyor part, the individual parts being separated for reasons of clarity; 22 is a perspective view of another embodiment of the front conveyor unit of the second conveyor part; FIG. 23 is a perspective view of another embodiment of a bridge; and FIG. 24 illustrates a third embodiment of the apparatus according to the invention, wherein the first conveyor part is constituted by an endless conveyor belt placed over the row of conveyor units in the first conveyor part within the path of the conveyor units from a storage space to the bridge.
    9 DK 2008 00051 U3
    Best embodiment of the invention
    The apparatus shown in Figure 1 comprises a car, shown by the general reference numeral 1, and which has a cab 2 and a carriage 3. The cab 2 bears a width corresponding to approx. half the width of the drawer 3. Beside the cab 2, the car 1 carries a ramp 4 which is not shown in a rotationally unspecified manner. By means of an actuator 5, the ramp 4 can be arranged with a suitable slope in relation to that of the car 3. The ramp 4 extends substantially over the whole the length of the car 1, the front end 6 of the ramp being in the area around the front of the cab 2.
    The ramp 4 carries a first conveyor portion shown by the general reference numeral 7, and a second conveyor portion shown by the general reference numeral 7. display number 8. The first conveyor portion 7 comprises, as can be seen in particular from Figures 1-4, where parts of the four sides of the ramp are removed for clarity, an endless conveyor belt 9. This endless conveyor belt 9 passes at the rear end of the ramp 4 from a bottom lane 10 to an upper lane 11 or vice versa via a rear reversing device 12 comprising a plurality of rollers 13, 14 and 15. The upper lane 11 terminates at its forward end by a redirector shown by the general reference numeral 16 (see also Figures 6 and 7). This diverting device 16 comprises two interconnected rollers 17 and 18, through which the conveyor belt 9 is redirected to an intermediate web 19 which proceeds forwardly toward the front end 6 of the ramp parallel to the top web 11, but at a level below it. This intermediate web 19 terminates at a front reversing device shown by the general reference numeral 20, which comprises a single roller 21. Via the roller 21, the belt 9 passes back to the lower web 10 extending parallel to the top web 11 and the intermediate path 19.
    As can be seen in particular in Figures 6 and 7, the redirector 16 is connected to the rear end of the second conveyor 8, seen in the longitudinal direction of the car by means of a U-shaped bracket 22. By simultaneously loading the bracket 22 be engaged with appropriate guides not shown further along the sides 23 and 24 of the ramp 4 (see Figure 6), movement of the second conveyor part 8 forward or rearward relative to the longitudinal direction of the car 1 implies that the diverting device 16 follows this movement so that it the top conveyor 11 of the first conveyor portion 7 increases or decreases in length according to the position of the rear end of the second conveyor portion 8. Within the intermediate web 19, the conveyor belt 9 is supported by a carrier plate 25 (see Figure 7) by appropriately not shown means. to reduce friction.
    Within the upper web 11, the conveyor belt 9 is supported by a support device 26, which consists of a plurality of interconnected members 27, which are hingedly connected along their longest away from the conveyor belt 9.
    This support device 26 is connected at one end to the redirector 16 so that it follows the movement of the redirector 16. At the same time, the support device is arranged to pass around from a location in the immediate vicinity of the lower web 10 to a location below the top web 11 via the rear nearest turning device 12 located by the said support plate 25, so that the number of slats located in the support state below the upper web 11 corresponds to substantially the entire length of the top web 11. If necessary, movement from one side to the other side of the support plate can be facilitated by guides not shown. In addition, the farthest end of the redirector 16 of the support device 26 may also be connected to the redirector by commonly known means, so that the said end is subjected to traction when the redirector 16 moves downwardly of the rear reverser 12.
    11 DK 2008 00051 U3
    The second conveyor portion 8 comprises a plurality of conveyor units 30, all except the front 31, being the same. All conveyor units 30 comprise an endless belt 32 (see Figure 15) which is driven around suitable rollers 33, 34 and 35. These rollers are mounted in a frame 36 which is mounted on a support device 37.
    The support device 37 is arranged on rollers 44. The conveyor units 30, 31 are interconnected by means of resilient coupling devices which allow them to be rotated relative to one another in the horizontal and vertical directions and displaced to a smaller extent relative to each other. same directions. These coupling devices are surrounded by bellows tubes with rectangular cross sections and circumferential waves. The frames 36 and the supporting devices 37 are made of a suitable plastic material. Furthermore, the coupling devices are thus arranged in a non-shown manner for releasably coupling the conveyor units 30, 31, so that they can be easily replaced. At the same time, the enclosing bellows-shaped tubes of the couplers easily allow passage of wiring harnesses and associated couplings so that the individual conveyor units 30, 31 are easily supplied with the desired energy, e.g. electric current. As mentioned above, the rear conveyor unit 30 is connected to the first conveyor portion redirector 16. In addition, the conveyor units are formed at such a height that their conveying plane, i.e. the upper side of the conveyor belts 32 is level with the upper web 11 of the endless conveyor belt 9 (see Fig. 7).
    The front conveyor unit 31, as shown particularly in Figures 13 and 14, comprises a rear-mounted conveyor flap 39.1. Figure 13 is shown in two possible positions and In Figure 14 three possible positions of the conveyor flap are shown. This conveyor flap 39 comprises an endless conveyor belt 40 which is not shown in a unspecified manner in a frame 41. The frame 41 is pivotally mounted in the rear in a unspecified manner in a support device 42 which is also mounted on wheel 44 (see Fig. 1). Between the frame 41 and the support device 42 are provided 43 which enable adjustment of the conveyor flap 39 in a position with a desired inclination.
    Furthermore, the conveyor flap 39 carries a pivotally mounted conveyor front portion 45. Seen from the side, the conveyor front portion 45 has a triangular cross-section and is also connected to an endless conveyor belt 46. By means not shown, this conveyor front portion 45 can be adjusted with a desired inclination relative to the conveyor flap 39. Preferably, the upper side of the conveyor front portion 45 of the conveyor belt 46 will be positioned in a horizontal plane when the conveyor flap 39 is disposed at a certain inclination relative to the conveying direction of the other conveyor units.
    The conveyor front portion 45 also has wheels 44 which enable the conveyor front portion 45 to facilitate the support of the relatively long projecting conveyor flap 39 together with the support device 42.
    On the side 41 of the frame 41 of the conveyor flap 39 is provided a handle 47 and 48 respectively. These handles 47 and 48 allow an operator to actuate the second conveyor part 8. At the same time, the handle 47 and 48 are arranged as control devices, so that the operator by appropriate rotation thereof, the different propellants not shown can be activated or influenced by the first and second conveyor parts 7, 8.
    Adjacent the front end of the ramp 4 is a slidable bridge 50 (see Figures 8-12 and 20). This bridge 50 is tiltable (see Fig. 20) and arranged to be placed in a substantially horizontal position by means of an actuator 28 and inserted through an opening 51 to a cargo space 52 in an aircraft 53. In Fig. 8 -12, the hatch that normally covers the opening of a cargo compartment 52 is removed. The bridge then forms a bridge between the ramp 4 and the floor 54 of the cargo space 52 directly within the opening 51.
    As can be seen from Figure 8, the bridge 50 is directly below the front conveyor unit 31 when it is retracted on the ramp. As can be seen in Figure 9, the bridge is advanced forward and inward through the opening 51 together with the front conveyor unit 31. This insertion occurs simultaneously with the inclination of the ramp 4 to fit the floor 54 of the cargo space 52. After the bridge is placed resting on the the floor 54 within cargo space 52 lifts the front conveyor unit toward one side or the other relative to the bridge 50 so that it can be pulled therefrom backwards or forwards into the cargo space together with subsequent conveyor units 30. This control or guide of the front conveyor unit 31 and the subsequent conveyor units 30 are in part promoted by an elevation 55 with suitably shaped guide sides 56 and 57 against which the conveyor units 30 and 31 slip during their movement.
    By appropriate means not shown, the bridge is coupled to and from the front conveyor unit 31 so that the bridge together with the conveyor unit 31 20 can be inserted through and out of the opening 51 of the cargo space 52.
    As shown in FIG. 8, the bridge 50 is located directly below the front conveyor unit 31 when the conveyor unit is in its retracted state on the ramp. As shown in FIG. 9, the bridge is moved forward and through the opening 51 25 together with the front conveyor unit 31. This inward movement is carried out while adjusting the inclination of the ramp 4 to fit the floor 54 in the cargo space 52, the front conveyor unit being lifted outwards to one side or to the other side of the bridge in such a way that it can be pulled backwards or pushed forward within the cargo space 30 together with the subsequent conveyor units 30. Such control or control of the front conveyor unit 31 and the subsequent conveyor units 14 DK 2008 00051 U3 units 30 are enhanced by a raised platform 55 with suitably formed guide sides 56 and 57, the conveyor units 30 and 31 sliding along the guide sides during their movement.
    Convenient means, not shown, connect and disconnect the bridge to and from the front conveyor unit so that the bridge together with the conveyor unit 31 can be moved into and out of the opening 51 of the cargo space 52.
    During use of the apparatus according to the invention, the second conveyor part, as shown in Figures 10 and 11, is pushed and moved into the relevant cargo space, where, as shown in Figures 16 and 17, an operator can use it for loading and unloading, respectively. As can be seen in Figure 16, the operator may allow the luggage 59 to be pulled up over his legs via the conveyor flap 39 and from here via the conveyor front portion 45 directly into a stack 60 of goods. During the unloading, the unit load is pulled out of the stack 60 and placed on top of the front conveyor unit 31, from which it is carried further out of the cargo space. Of course, when using the apparatus, the operator can place and use the conveyor flap 39 as desired. All movements and stops as well as adjusting the length of the second conveyor part 8 within the cargo space according to the given conditions can be controlled by the operator within the cargo space via the handles 47.
    In FIG. 18 and 19, another embodiment of the apparatus according to the invention is shown. Here, both the first and second transport parts 7 and 8 conveying paths are formed by a continuous row of conveyor units 30 and 31. The rear end of this row is accommodated in a magazine 65 under the car 3 of the car 1 and is led from here to the ramp via the rear end of the car. as the front end of the row is inserted into the cargo space 52 of the aircraft 53. This embodiment is particularly suitable for use in particularly long cargo spaces 52 for which a relatively large number of conveyor units are required.
    15 DK 2008 00051 U3
    The individual parts and in particular the conveyor units of the second conveyor part 8 are made mainly of plastic materials having regard to the desired strength. Further, at the rear end of the apparatus, additional conveyors 61 and 62 may be mounted to facilitate the transition between luggage conveying and removal equipment and the rear end of the first conveyor portion 7. All propellants are connected to energy sources in no further detail. the car 1.
    In FIG. 21, another embodiment of a conveyor unit with a continuous belt 71 carried by rollers 72 and 73 is shown, the first roller 72 being a drive roller which is powered by electricity as indicated through a guide 116. The rollers 72 and 73 are mounted in a frame 75 by means of brackets 74 and 75. The frame 75 is provided on both sides with a pair of wheels 76 which are protected by screens 77 and 78 respectively, so that they are covered both at the top and bottom, whereby the conveyor units are able to roll on suitable guides, both when in a position where the conveyor belt 71 faces upwards, and in a position where the conveyor belt faces downwards, cf. 24. Screens 79 and 80 are mounted on frame 75 along the sides of the conveyor belt 71.
    The conveyor units are assembled by means of coupling devices 81 and 82 which are preferably made of die-cast aluminum. Such coupling devices 81 and 82 are pivotally mounted about axes 83 and 84 in two adjacent conveyor units and are mutually pivotally mounted about axis 85, a rubber unit 86 being disposed between the coupling devices. This rubber unit 86 ensures both alignment of the conveyor units when the conveyor units are not subjected to a mutually rotating load, and provides a protected passage for electrical guides between the conveyor units through convenient channels 87 and 88. The conveyor units carry elements 115 which cooperate with the coupling devices 81 and 82 in such a way that they can only rotate in one direction about axes 83 and 16, away from a common plane through the conveyor units parallel to their conveyor paths.
    In FIG. 22, another embodiment of the conveyor front unit is shown. This conveyor unit is designated by the general reference numeral 90 and comprises a conveyor or flap 91 ·. At the front, the conveyor flap 91 forms a bend such that the front conveyor unit comprises a front member 92 permanently connected to the other portion of the flap 91. The front conveyor unit 90 comprises an endless conveyor belt 93 extending above the front member through convenient rollers. . In front of the continuous belt 93 are provided a pair of loosely mounted rollers 94 and 95. The conveyor flap 91 comprises a frame 96 which is pivotally mounted in a support member 97. The support member 97 carries support means 98 and support members 99 and 100 hingedly connected to the support member. 97 and slidably mounted on frame 96. Carrier 97 comprises wheels 101 rotatably disposed about shafts extending perpendicularly to the plane of carrier 97. In addition, one or more wheels 102 are provided, cf. 24, below the front member 92 of the flap 91, which wheels are of the same type as the wheels 101.
    In FIG. 23, a telescopic bridge is shown comprising guiding means 106 and 107. Such guiding means 106 and 107 allow control of the row of conveyor units in the desired direction into the cargo hold of an aircraft. The front guide members 107 of the two guide members are disposed on a rotatable disk 108 which allows adjustment of the guide members 107 in the desired direction. The guide members 106 and 107 are arranged to cooperate with the appropriate control elements not shown on the underside of the conveyor units.
    In FIG. 24 shows a third embodiment of the invention. Here, the conveyor path of the first conveyor portion 7 is constituted by a first endless conveyor belt 110 mounted above the paths of conveyor units 70 between a magazine 111 and the bridge 105. The first conveyor portion 7 further comprises a conveyor front member with a second continuous belt 112. , and which decreases at the front in such a way that the cargo being handled passes relatively easily to and from the first endless conveyor belt of the first conveyor portion 7. As indicated in FIG. 24, rails 113 are provided in the magazine 111, and the conveyor units 70 can travel on these rails by the wheels 76 while the endless conveyor belts face down.
    The movement of the conveyor units 70 to and from the space is carried out by means of a running endless conveyor belt 114 which cooperates with the underside of the conveyor units 70 in an appropriate manner, such as by friction.
    The invention has been described with reference to preferred embodiments. Many changes can be made without departing from the idea of creation. Eg. For example, the first and second conveyor portions 7 and 8, with the associated ramp 4, may be mounted on equipment other than a car. In this connection, the most important thing is that it must be possible to adapt the location of the opening into the cargo space in question.
    The generation is described for use in aircraft, but can of course also be used in other situations where similar conditions apply.
    Instead of slats 27, the support device 26 may also include rollers, and the conveyor units 30, 31 may be adapted to slide on appropriate guides on the sides of the ramp 4 rather than resting on their own wheels as long as they are on the ramp 4 .
    权利要求:
    Claims (43)
    [1]
    An grounding device for loading and unloading aircraft (53) with a cargo compartment (52), via an opening (51) in the aircraft side, comprising: a tiltable, height adjustable first conveyor (7) adapted to transporting goods between an underlying area outside the cargo compartment (52) and a second conveyor (8), said second conveyor (8) having a first end and a second end and being substantially partially extendable relative to the apparatus from a position below it; first conveyor (7) and into the cargo compartment (52), said second conveyor (8) comprising a plurality of conveyor units (30, 31, 70, 90), a front conveyor unit (31, 90) disposed at said first end and being arranged to allow conveying of the conveyed goods to a desired height, and wherein each conveyor unit (30, 31, 70, 90) has a set of wheels (44, 76,101,102), which apparatus is new in that each conveyor unit (30, 31, 70, 90) are connected to each other by means of coupling elements (38, 81, 82) which permit sideways reciprocal rotation of the conveyor units (30, 31, 70, 90) and a reciprocal rotation of the conveyor units (30, 31, 70, 90) about a substantially horizontal axis (83, 84), wherein each conveyor unit (30, 31, 70, 90) defines a respective activatable conveyor path, and the front conveyor unit (31, 90) comprises means for varying the inclination of the conveyor path, and handles (47, 48) by which a operator, 19 DK 2008 00051 U3 located inside the aircraft can maneuver the second conveyor (8) and activate the first conveyor (7) and the second conveyor (8) propellants.
    [2]
    Apparatus according to the preceding claim, characterized in that the front conveyor unit (31,90) comprises a support element (97) with said set of wheels (101), which wheels (101) are rotatably arranged around axles extending perpendicular to the plane of the carrier (97), and that the carrier (97) is pivotally connected to the rear of the frame (96) by a flap (91) comprising the conveyor path of the front conveyor unit (31, 90). 10
    [3]
    Apparatus according to claim 1 or 2, characterized in that the first conveyor (7) comprises a single endless conveyor belt (9) with an upper web (11) defining a goods receiving surface.
    [4]
    Apparatus according to the preceding claim, wherein the length of the upper web (11) of the conveyor belt (9) is adjustable according to the extension or retraction of the second conveyor (8).
    [5]
    Apparatus according to the preceding claim, characterized in that the endless conveyor belt (9) extends between a front facing device (20) located adjacent to the aircraft (53) and a rear facing device (12), the front conveyor (7) further having an intermediate diverting device (16) displaceable in the direction of transport, through which the belt (9) is directed from a direction of the top path (11) of the conveying path extending between the rear reversing device (12) and the diverting device (16) to an intermediate path (19) extending parallel to the upper path (11), but at a level below the upper path between the redirector (16) and the forward facing device (20), the band (9) between the forward reversing device (20) and the rear reversing device (12) extend below the upper (11) and intermediate path (19), whereby the upper path (11) forms at least a portion of the DK 2008 00051 U3 conveyor path of the first conveyor (7), and that the rear end of the plurality of conveyor unit (30, 31, 70, 90) is connected to the diverting device (16) of the first conveyor part (7) and thus arranged to be moved back and forth along with this, moving the conveyor units (30, 31, 70, 90) above the intermediate path (19) of the first conveyor part (7) when outside the aircraft (53).
    [6]
    Apparatus according to claim 5, characterized in that it has a support device (26) for supporting the endless conveyor belt (9) of the first conveyor (7) during its movement within the upper web (11).
    [7]
    Apparatus according to any one of the preceding claims, characterized in that the apparatus comprises a bridge (50, 105) arranged to be supported by the aircraft and to support the conveyor units (30, 31, 70, 90) of the second conveyor ( 8) during its ejection from the apparatus and into the cargo compartment (52).
    [8]
    Apparatus according to any one of the preceding claims 1 or 2, characterized in that the first conveyor (7) comprises a plurality of interconnected conveyor units (30, 31, 70, 90), each having a set of wheels (44). , 76, 101,102) and are pivotally connected to each other by respective coupling devices.
    [9]
    Apparatus according to any one of the preceding claims, characterized in that the apparatus comprises a magazine (65, 111) for accommodating the second conveyor.
    [10]
    Apparatus according to the preceding claim, characterized in that the first conveyor (7) is located above the magazine (52). 21 DK 2008 00051 U3
    [11]
    Apparatus according to any of claims 2-9, characterized in that apparatus has storage means (65,111) for storing the second conveyor (8) in a state in which at least two consecutive conveyor units are rotated relative to each other. about the substantially horizontal axis (83, 84).
    [12]
    Apparatus according to any one of the preceding claims, characterized by a conveyor front element which is hingedly connected to the conveyor unit at the first end and which can be adjusted with a desired inclination relative to the conveyor path of the conveyor unit (39) at the first end.
    [13]
    Apparatus according to any one of the preceding claims, characterized in that each conveyor unit (30, 31, 70, 90) comprises an endless conveyor belt (40,46, 71.93).
    [14]
    Apparatus according to the preceding claim, characterized in that each endless conveyor belt is driven by a drive roller (72) and a number of other rollers (33, 34, 35, 73), all supported by a frame (36, 41, 75). , which in turn is supported by a wheel bearing support device (37, 42, 77, 78, 97).
    [15]
    Apparatus according to claim 13 or 14, characterized in that the width of the conveyor belt (40, 46, 71, 93) is greater than the distance between the rollers.
    [16]
    Apparatus according to any of the preceding claims 7-15, characterized in that the bridge (50, 105) comprises guiding means (55, 56, 57, 106, 107) for guiding the second conveyor (8).
    [17]
    Apparatus according to any one of the preceding claims, characterized in that the front conveyor unit (31, 90) comprises an endless conveyor belt (46). 22 DK 2008 00051 U3
    [18]
    Apparatus according to any one of the preceding claims, characterized in that the apparatus comprises drive means which cooperate with the second conveyor for ejecting the second conveyor (8) from the apparatus, e.g. by friction. 5
    18 DK 2008 00051 U3
    [19]
    Apparatus according to any one of the preceding claims, characterized in that it is located on a vehicle (1).
    [20]
    Apparatus according to any one of the preceding claims, characterized in that a reciprocal lateral rotational movement of at least two consecutive conveyor units (30, 31, 70, 90) allows lateral movement of the front conveyor unit.
    [21]
    Apparatus according to any one of the preceding claims, characterized by an additional conveyor (61, 62) pivotally mounted at the end of the apparatus opposite the projecting region of the second conveyor (8), which further conveyor (61, 62) facilitates the passage of goods between the first conveyor (7) and equipment for conveying and controlling said goods. 20
    [22]
    An grounding apparatus for loading and unloading aircraft (53) with a cargo compartment (52), via an opening (51) in the aircraft side, comprising: a tiltable, height adjustable first conveyor (7) adapted to transporting goods between an underlying area outside the cargo compartment (52) and a second conveyor (8), said second conveyor (8) having a first end and a second end and being substantially partly extendable relative to the apparatus of a position below 30 the first conveyor (7) and into the cargo compartment (52), which second conveyor (8) comprises a plurality of conveyor units (30, 31, 70, 90), of which a front conveyor unit (31.90 ) is disposed at the first end and arranged to permit the conveyance of the conveyed goods to a desired height, and each conveyor unit (30, 31, 70, 90) having a set of wheels (44, 76,101,102), which apparatus is new knowing that each conveyor unit (30, 31, 70, 90) is connected to each other by means of coupling elements (38, 81, 82) which allow sideways reciprocal rotation of the conveyor units (30, 31, 70, 90) and a reciprocal rotational movement of the conveyor units (30, 31, 70, 90) about a substantially horizontal axis (83, 84), wherein each conveyor unit (30, 31, 70, 90) defines a respective activatable conveyor path and wherein the front conveyor unit (31, 90) comprises means for varying the inclination of the conveyor path, and a carrier (97) said carrier element (97) being pivotally connected to the rear end of a flap (91) comprising the conveyor path of the front conveyor unit (31, 90), said flap (91) having such an extension that - in a direction away from the other conveyor (8) other conveyor units (30, 31, 70, 90) - protrude from the carrier (97) when the flap (91) is turned down towards the carrier (97).
    [23]
    Apparatus according to claim 22, characterized in that the first conveyor (7) comprises a single endless conveyor belt (9) with an upper web (11) defining a goods receiving surface.
    [24]
    Apparatus according to the preceding claim, wherein the length of the upper web (11) of the conveyor belt (9) is adjustable according to the extension or retraction of the second conveyor (8). 24 DK 2008 00051 U3
    [25]
    Apparatus according to the preceding claim, characterized in that the endless conveyor belt (9) extends between a front facing device (20) located adjacent to the aircraft (53) and a rear facing device (12), the front conveyor (7) further having a intermediate, in the transport direction, reciprocally displaceable device (16), through which the belt (9) is directed from a direction of the top path (11) of the conveyor path extending between the rear reversing device (12) and the diversion device (16) to an intermediate web (19) extending parallel to the top web (11), but at a level below the top web between the redirector (16) and the front facing device (20), the band (9) between the front facing device (20) and the rear facing device (12) extends below the upper (11) and intermediate web (19), whereby the upper web (11) forms at least a portion of the first transp. conveyor path (7), and the rear end of the plurality of conveyor unit (30, 31, 70, 90) is connected to the diverting device (16) of the first conveyor part (7) and thus arranged to be reciprocated therewith, the conveyor units (30, 31, 70, 90) are moved above the intermediate path (19) of the first conveyor part (7) as they are outside the aircraft (53).
    [26]
    Apparatus according to claim 25, characterized in that it has a support device (26) for supporting the endless conveyor belt (9) of the first conveyor (7) during its movement within the upper web (11).
    [27]
    Apparatus according to any one of the preceding claims 22-26, characterized in that the apparatus comprises a bridge (50,105) which is adapted to be supported by the aircraft and supports the conveyor units (30, 31, 70, 90) thereof. second conveyor (8) during its ejection from the apparatus and into the cargo compartment (52). 25 DK 2008 00051 U3
    [28]
    Apparatus according to claim 22, characterized in that the first conveyor (7) comprises a plurality of interconnected conveyor units (30, 31, 70, 90), each having a set of wheels (44, 76, 101, 102) and pivotally connected to each other. at respective coupling devices.
    [29]
    Apparatus according to any one of the preceding claims 22-28, characterized in that the apparatus comprises a magazine (65, 111) for accommodating the second conveyor.
    [30]
    Apparatus according to the preceding claim, characterized in that the first conveyor (7) is located above the magazine (52).
    [31]
    Apparatus according to any one of claims 23-30, characterized in that the apparatus has storage means (65, 111) for storing the second conveyor (8) in a state in which at least two consecutive conveyor units are rotated. relative to each other about the substantially horizontal axis (83, 84).
    [32]
    Apparatus according to any one of the preceding claims 22-31, characterized by a conveyor front element which is hingedly connected to the conveyor unit at the first end and which can be adjusted with a desired inclination relative to the conveyor path of the conveyor unit (39) at the first end.
    [33]
    Apparatus according to any of the preceding claims 22-32, characterized in that each conveyor unit (30, 31, 70, 90) comprises an endless conveyor belt (40, 46, 71.93).
    [34]
    Apparatus according to the preceding claim, characterized in that each endless conveyor belt is driven by a drive roller (72) and a number of other rollers (33, 34, 35, 26 DK 2008 00051 U3 73), all supported by a frame (36 , 41, 75), which in turn is supported by a wheel supporting support device (37, 42, 77, 78, 97).
    [35]
    Apparatus according to claim 33 or 34, characterized in that the width of the conveyor belt (40, 46, 71.93) is greater than the distance between the rollers.
    [36]
    Apparatus according to any one of the preceding claims 22-35, characterized in that the flap (91), on the part projecting from the support element (97), has control means (47, 48) with which an operator who located inside the aircraft can activate the propellants of the first carrier (7) and the second carrier (8).
    [37]
    Apparatus according to any one of the preceding claims 27-36, characterized in that the bridge (50, 105) comprises guide means (55, 56, 57, 106, 107) for guiding the second conveyor (8).
    [38]
    Apparatus according to any of the preceding claims 22-37, characterized in that the front conveyor unit (31, 90) comprises an endless conveyor belt (46).
    [39]
    Apparatus according to any one of the preceding claims 22-38, characterized in that the apparatus comprises drive means which cooperate with the second conveyor for ejecting the second conveyor (8) from the apparatus, e.g. by friction.
    [40]
    Apparatus according to any one of the preceding claims 22-39, characterized in that it is located on a vehicle (1).
    [41]
    Apparatus according to any of the preceding claims 22-40, characterized in that a reciprocal lateral rotational movement of at least two consecutive conveyor units (30, 31, 70, 90) allows lateral movement of the front conveyor unit.
    [42]
    Apparatus according to any one of the preceding claims 22-41, characterized by an additional conveyor (61, 62) pivotally mounted at the end of the apparatus opposite the projecting area of the second conveyor ( 8) which further conveyor (61, 62) facilitates the passage of goods between the first conveyor (7) and equipment for conveying and ironing said goods. 10
    [43]
    Apparatus according to any one of the preceding claims 22-42, characterized in that the set of wheels (101) of the front conveyor unit (31, 90) on the support element (97) is rotatably arranged about shafts extending perpendicularly to the support element. (97) plan.
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    同族专利:
    公开号 | 公开日
    CA2640645A1|2001-07-19|
    DE60118043T2|2006-10-12|
    MXPA02006757A|2004-09-10|
    CA2640645C|2010-12-21|
    DK200500245U1|2005-11-25|
    US20030161707A1|2003-08-28|
    EP1248726A1|2002-10-16|
    EA003548B1|2003-06-26|
    EP1273517B1|2006-03-15|
    EP1666357A1|2006-06-07|
    JP2003519594A|2003-06-24|
    BR0107552B1|2010-09-08|
    EA200200744A1|2002-12-26|
    EP1248726B1|2004-07-14|
    US7156604B2|2007-01-02|
    DK200000031A|2001-07-12|
    WO2001051356A1|2001-07-19|
    EP1273517A3|2003-12-10|
    US6893200B2|2005-05-17|
    AT320375T|2006-04-15|
    US20030049107A1|2003-03-13|
    NZ520399A|2003-04-29|
    AU774012B2|2004-06-10|
    AU2353401A|2001-07-24|
    ES2259064T3|2006-09-16|
    ES2308644T3|2008-12-01|
    BR0107552A|2002-10-08|
    DE60133327D1|2008-04-30|
    EP1273517A2|2003-01-08|
    DE60104280T2|2005-07-28|
    US7033125B2|2006-04-25|
    DK200800051U3|2008-05-23|
    DK200500245U4|2006-03-10|
    DE60104280D1|2004-08-19|
    PL355969A1|2004-05-31|
    AT389583T|2008-04-15|
    US20030091415A1|2003-05-15|
    CN1162303C|2004-08-18|
    ES2222330T3|2005-02-01|
    EP1666357B1|2008-03-19|
    PL205783B1|2010-05-31|
    DE60133327T2|2009-03-05|
    CN1396877A|2003-02-12|
    US20040105740A1|2004-06-03|
    DK1666357T3|2008-07-14|
    CA2396198C|2008-12-23|
    CA2396198A1|2001-07-19|
    JP4937476B2|2012-05-23|
    DE60118043D1|2006-05-11|
    DK173750B1|2001-09-10|
    ZA200205298B|2003-10-02|
    AT271002T|2004-07-15|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    DE170863C|
    US2242206A|1939-03-02|1941-05-20|Mathews Conveyer Company Ltd|Loading and unloading conveyer apparatus|
    US2242406A|1939-08-11|1941-05-20|Alexander P Stewart|Templet|
    US2346659A|1941-01-28|1944-04-18|John K Bruce|Merchandise conveyer|
    US2494302A|1945-11-05|1950-01-10|James J Mason|Articulated conveyer|
    US2990938A|1956-12-03|1961-07-04|Robert T Sheehan|Self-propelled articulated stacking conveyor|
    US3051295A|1959-03-23|1962-08-28|Moy Peter Charles Duffield|Mobile elevators|
    US2988190A|1960-06-29|1961-06-13|Pearl L Tucker|Retracting stretch-o-veyor|
    US3184045A|1963-03-22|1965-05-18|Fry And Company|Portable conveyor system|
    US3268099A|1964-11-04|1966-08-23|Koehring Co|Universal power conveyor|
    US3356236A|1965-08-05|1967-12-05|Domino Sugar Company|Bi-directional cargo transfer unit|
    US3524558A|1967-03-30|1970-08-18|American Mach & Foundry|Cargo loading means and method|
    US3885682A|1972-11-13|1975-05-27|Joseph E Mcwilliams|Mail bag handling apparatus|
    GB1490874A|1974-12-23|1977-11-02|Automotive Prod Co Ltd|Pivot joints|
    US4164338A|1978-02-23|1979-08-14|Brooks & Perkins, Incorporated|Flexible rail roller system|
    US4266650A|1979-11-26|1981-05-12|Bliss & Laughlin Industries Incorporated|Coupling hinge for two conveyors|
    ES8602504A1|1984-03-05|1985-12-01|Fmc Corp|Aircraft belt-loader vehicle|
    US4618057A|1984-10-24|1986-10-21|Production Systems, Inc.|Chain-link belt conveyor with adjustable parallel offset and variable radius guide|
    US4620629A|1985-03-04|1986-11-04|Fmc Corporation|Side guide for aircraft belt loader|
    US4610559A|1985-04-12|1986-09-09|Weasler Engineering, Inc.|Shield for universal joint|
    DE3703969A1|1986-09-26|1988-04-07|Phb Weserhuette Ag|STACKING AND / OR UNLOADING DEVICE FOR STUECKGUETER|
    NL8603210A|1986-12-17|1988-07-18|Product Suppliers Ag|DEVICE AND METHOD FOR TEMPORARILY REMOVING A PRODUCT FROM A SERIES OF TRANSPORTED PRODUCTS.|
    IT1211805B|1987-09-25|1989-11-03|Sefind Srl|AUTOMATIC OPERATION LOAD FACING DEVICE FOR AIRCRAFT STORES|
    US4957405A|1988-09-26|1990-09-18|Consolidation Coal Company|Apparatus for mining|
    US5009560A|1988-12-06|1991-04-23|Yellow Freight System, Inc.|Mixed freight handling system|
    IT8921799D0|1989-09-22|1989-09-22|Pirelli|VARIABLE LENGTH ROLLER TABLE.|
    JP2778601B2|1990-03-28|1998-07-23|株式会社東京自働機械製作所|Connecting robot|
    IT1244384B|1990-11-05|1994-07-11|Mopa|LUNG FOR THE ACCUMULATION AND LIBERATION IN EQUIDISTANT ROWS OR WITH A PROGRAMMED CADENCE OF PRODUCTS COMING FROM A CONTINUOUS ADVANCE LINE ARRANGED IN NON-EQUIDISTANT RANGES.|
    US5224584A|1991-01-16|1993-07-06|Northstar Industries, Inc.|Expandable powered conveyors|
    DK170863B1|1993-03-16|1996-02-19|Pv System Aps|Article conveyor|
    JPH07277461A|1994-04-11|1995-10-24|Bridgestone Corp|Coupling device for revolving conveyor|
    AU1092797A|1995-12-12|1997-07-03|Caljan A/S|A loading/unloading conveyor|
    NL1002469C2|1996-02-28|1997-08-29|Universal Corrugated Bv|Variable conveyor.|
    US6006893A|1996-04-24|1999-12-28|Mannesmann Dematic Rapistan Corp.|Extendable trailer loader/unloader with user interface section|
    NL1006134C2|1997-05-26|1998-12-01|Nia Tno B V|Auxiliary device for manual loading and / or unloading general cargo.|
    US5836388A|1997-07-16|1998-11-17|Computalog Limited|Flexible joint for downhole tools|
    DE19961349A1|1999-12-17|2001-06-21|Schopf Maschb Gmbh|Mobile device for loading and unloading aircraft|ES2283551T3|2001-04-26|2007-11-01|Bsh Bosch Und Siemens Hausgerate Gmbh|DEVICE FOR LOADING AND / OR DOWNLOADING A TRANSPORTATION LOAD COMPARTMENT.|
    DE20212383U1|2002-03-11|2003-02-20|Telair Internat Ab Lund|System for loading and unloading piece goods in cargo hold of aircraft has intermediate conveyor unit provided between aircraft side end of outside conveyor device and forward end of transporting device in cargo hold|
    DE10210575A1|2002-03-11|2003-12-04|Telair International Lund|System for loading and unloading piece goods in cargo hold of aircraft has intermediate conveyor unit provided between aircraft side end of outside conveyor device and forward end of transporting device in cargo hold|
    WO2003076267A1|2002-03-11|2003-09-18|Telair International Ab|System for loading and unloading unit loads into a cargo hold, in particular of an aircraft, and intermediate transport device or corresponding transport unit|
    ES2258587T3|2002-11-08|2006-09-01|Trepel Airport Equipment Gmbh|PROCEDURE FOR LOADING AND UNLOADING AN AIRPLANE AS WELL AS MOBILE DEVICE FOR LOADING AN AIRPLANE|
    US7053617B2|2003-10-01|2006-05-30|General Electric Co.|Integrated electronic RF shielding apparatus for an MRI magnet|
    DE10345998B4|2003-10-02|2013-07-25|Telair International Ab|System for loading and unloading a cargo space of an aircraft with general cargo|
    DK1713704T3|2004-01-30|2008-11-10|Martin Vestergaard|Transporter|
    US7268676B2|2004-09-13|2007-09-11|Spencer Irvine|Actuated braking and distance sensing system for operational regulation of belt loader equipment|
    AT437820T|2005-01-11|2009-08-15|Martin Vestergaard|CONVEYOR PROTECTION|
    NL1028534C1|2005-03-14|2006-09-18|Vanderlande Ind Nederland|Luggage pieces moving vehicle for aeroplane, has bridging conveyor system with bridging conveyor and guide system for extending conveyor from vehicle into aeroplane by guide system|
    CA2601500A1|2005-03-14|2006-09-21|Vanderlande Industries Nederland B.V.|Vehicle for moving separate pieces of luggage between a luggage depot and an aeroplane|
    DK1879822T3|2005-05-02|2013-05-27|Univeyor As|System for unloading or loading of general cargo|
    DE102005021078B4|2005-05-06|2010-07-15|Rheinmetall Defence Electronics Gmbh|Cargo loading system|
    US7469782B2|2005-07-22|2008-12-30|Dew Engineering And Development Limited|Conveyor system for loading and unloading aircraft baggage|
    NO325120B1|2005-08-19|2008-02-04|Niels Bugge|Bracket and bracket arrangement for connecting modules in a conveyor system|
    US7654378B1|2006-06-08|2010-02-02|Nmc-Wollard, Inc.|Conveying device|
    US7261202B1|2006-06-08|2007-08-28|Nmc-Wollard, Inc.|Conveying device with hollow universal joint|
    US7451866B2|2006-06-08|2008-11-18|Nmc-Wollard, Inc.|Conveying device|
    US7513354B1|2006-08-04|2009-04-07|Nmc-Wollard, Inc.|Portable lift conveyor|
    US7416075B2|2006-08-08|2008-08-26|Northstar Industries, Inc.|Telescoping conveyor with powered and steerable discharge section|
    ITVI20070025A1|2007-01-30|2008-07-31|Virginio Nastri S R L|LOADER IN CONTINUOUS OBJECTS, LIFTABLE AND INCLINABLE|
    FR2917373B1|2007-06-15|2009-12-18|Airbus France|DEVICE FOR MOVING OBJECTS, IN PARTICULAR FOR LUGGAGE IN A AIRCRAFT BODY|
    DE102007034947B4|2007-07-26|2009-06-18|Siemens Ag|Device for unloading a stack of flat objects standing on their narrow sides|
    DE102007048876A1|2007-10-11|2009-04-23|Mulag Fahrzeugwerk Heinz Wössner GmbH u. Co KG|luggage conveyor|
    US8596947B1|2008-01-22|2013-12-03|Kent J. Stenzel|Airport baggage accumulation rack having rotatable shelves, and method for handling baggage|
    GB201010997D0|2010-06-30|2010-08-18|Mallaghan Engineering Ltd|Conveyor apparatus for loading and unloading an aircraft|
    US9650215B2|2013-05-17|2017-05-16|Intelligrated Headquarters Llc|Robotic carton unloader|
    WO2014186781A1|2013-05-17|2014-11-20|Intelligrated Headquarters, Llc|Robotic carton unloader|
    US9623569B2|2014-03-31|2017-04-18|Intelligrated Headquarters, Llc|Autonomous truck loader and unloader|
    US10807805B2|2013-05-17|2020-10-20|Intelligrated Headquarters, Llc|Robotic carton unloader|
    US20160185531A1|2013-08-27|2016-06-30|Crisplant A/S|An item transfer device and a method of operating the item transfer device|
    CN105531207B|2013-08-28|2018-06-08|因特利格兰特总部有限责任公司|Carton unloads robot|
    US9604787B1|2015-12-09|2017-03-28|Caljan Rite-Hite Aps|Adjustable conveyor systems|
    US10597235B2|2016-10-20|2020-03-24|Intelligrated Headquarters, Llc|Carton unloader tool for jam recovery|
    CN106740361B|2017-01-19|2018-09-28|江苏天一机场专用设备有限公司|A kind of compartment of aircraft food car|
    EP3441331A1|2017-08-09|2019-02-13|Siemens Aktiengesellschaft|Method for handling sorting pieces with monitored telescopic conveyor belts|
    CN108106308B|2017-12-29|2020-03-20|郑州航空工业管理学院|Automatic three-dimensional freezer based on thing networking|
    CN108860617A|2018-07-03|2018-11-23|中国民航大学|A kind of aviation luggage draw off gear|
    CN109335701B|2018-09-20|2021-02-09|湖北昌丰粮机有限公司|Be fit for not in bags rice transport piling car of co-altitude|
    WO2021090268A1|2019-11-08|2021-05-14|Leonardo S.P.A.|Closure system of the interconnection of transport units connected to each other in a convoy|
    CN111422120B|2020-04-30|2021-07-13|王于照|Unloading equipment for express delivery transport vehicle|
    CN113321009B|2021-07-09|2021-12-17|湖北和诺生物工程股份有限公司|Automatic treatment system and method for nicotine production waste residues|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    DK200000031A|DK173750B1|2000-01-11|2000-01-11|Aircraft loading and unloading apparatus|
    DK200800051U|DK200800051U3|2000-01-11|2008-03-18|Aircraft loading and unloading apparatus|DK200800051U| DK200800051U3|2000-01-11|2008-03-18|Aircraft loading and unloading apparatus|
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