WO2012131987A1 - Plaque de répartition de charge pour avion, et structure de fixation pour conteneurs de transport de fret l'utilisant - Google Patents

Plaque de répartition de charge pour avion, et structure de fixation pour conteneurs de transport de fret l'utilisant Download PDF

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Publication number
WO2012131987A1
WO2012131987A1 PCT/JP2011/058247 JP2011058247W WO2012131987A1 WO 2012131987 A1 WO2012131987 A1 WO 2012131987A1 JP 2011058247 W JP2011058247 W JP 2011058247W WO 2012131987 A1 WO2012131987 A1 WO 2012131987A1
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WO
WIPO (PCT)
Prior art keywords
load distribution
cargo
aircraft
transport container
distribution plate
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Application number
PCT/JP2011/058247
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English (en)
Japanese (ja)
Inventor
高秀 上村
Original Assignee
Ａｎａロジスティクサービス株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
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Priority to PCT/JP2011/058247 priority Critical patent/WO2012131987A1/fr
Publication of WO2012131987A1 publication Critical patent/WO2012131987A1/fr

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like

Definitions

  • the present invention relates to a load distribution plate installed in a cargo compartment of an aircraft, and a transport container fixing structure for fixing the load distribution plate and the cargo transport container to the cargo compartment.
  • General aircraft have a cargo compartment at the bottom of the aircraft, for example.
  • transported cargo is accommodated in a cargo container or the like in an airport and is carried into an aircraft cargo compartment.
  • the cargo container and the like are taken out from the cargo compartment, and then the cargo is taken out from the container and the like.
  • Patent Document 1 an apparatus disclosed in Patent Document 1 below is known as a technique for improving the efficiency of carrying in and carrying out cargo containers and the like.
  • the apparatus of Patent Document 1 facilitates the transportation of cargo containers in the cargo compartment by installing rolls and belt conveyors on the floor of the cargo compartment of the aircraft.
  • the strength of the bottom wall of the cargo compartment is insufficient. Therefore, if a heavy cargo container is installed, the bottom wall may be damaged or deformed.
  • Patent Document 1 is difficult to apply to a small aircraft because the device is large-scale, heavy, and expensive to install.
  • An object of the present invention is to carry an operation of carrying a cargo transport container capable of accommodating heavy cargo into an aircraft cargo compartment, and an operation of carrying out the cargo transport container from the cargo compartment in an aircraft not equipped with a cargo container transport device.
  • a load distribution plate that can be efficiently performed in a short time, is lightweight, inexpensive, and easy to install and remove, and a freight transport container fixing structure using the same.
  • An aircraft load distribution plate includes a main body portion having a bottom surface that is fitted to a floor wall of a cargo compartment provided in an aircraft, the floor wall of the cargo compartment, and the main body portion.
  • the hard plate has a groove for guiding a caster for transporting the cargo transport container.
  • the tip of a roller protrudes from the upper surface of the hard plate, and the cargo transport container is fixed at a predetermined position on the hard plate. It is desirable to further include an elevating roller device that accommodates the roller below the upper surface of the hard plate.
  • the hard plate preferably has a plurality of anti-slip protrusions on the surface.
  • the hard plate includes a foamed polyethylene plate and aluminum plates attached to the upper and lower surfaces of the foamed polyethylene plate.
  • the main body is formed of a urethane material.
  • the adhesion film is preferably a silicone film.
  • a cargo transport container fixing structure using an aircraft load distribution plate according to a second invention of the present application is the aircraft load distribution plate according to the first invention, installed in a cargo compartment of an aircraft, and the aircraft load distribution.
  • a plurality of fixtures provided on the floors or walls on both sides of the cargo compartment along both side surfaces of the plate, a covering material covering the cargo transportation container placed on the upper surface of the aircraft load distribution plate, and A plurality of straps for securing the covering material to the corresponding fitting, one end of which is fixed to the covering material.
  • an aircraft load distribution plate can be installed on the floor wall of the cargo compartment, and the cargo transport container can be transported and fixed on the load distribution plate. Therefore, according to the first invention, the load applied to the floor wall of the cargo compartment by the freight transport container can be dispersed and kept below the floor load amount limit value determined by the aircraft manufacturer. Can be prevented from being damaged or deformed.
  • an adhesion film is provided on the lower surface of the main body of the load distribution plate, it is possible to prevent the load distribution plate from being displaced when the aircraft is tilted during flight or the like.
  • the durability of the load distribution plate can be increased by providing the adhesion film.
  • by providing an adhesive film when the load distribution plate is mechanically fixed to the floor wall of the cargo compartment, simple fixing is sufficient, so that it is easy to remove the load distribution plate when inspecting the aircraft. Become.
  • the hard plate is provided on the main body of the load distribution plate, the surface strength of the load distribution plate can be secured to prevent the load distribution plate from being damaged.
  • the work of transporting and carrying the cargo transport container using the caster can be efficiently performed in a shorter time.
  • the lift roller device by using the lift roller device, it is possible to efficiently carry in and carry the cargo in a short time without providing a caster in the cargo transport container.
  • the first invention by providing a plurality of anti-slip protrusions on the hard plate, it is possible to prevent the operator from sliding the foot and to improve the safety of the work. Furthermore, by providing such protrusions, the cargo transport container can be prevented from slipping and the cargo transport container on the load distribution plate can be stably fixed.
  • strength hard board can be obtained by comprising a hard board using a polyethylene foam board and the aluminum board affixed on the upper surface and lower surface of this foaming polyethylene board.
  • the main body portion by forming the main body portion from a urethane-based material, it is possible to obtain a load distribution plate that is lightweight, inexpensive, and has sufficient strength.
  • sufficiently high adhesion can be obtained by forming the adhesion film with a silicone film.
  • the strap is secured to the fixture provided on the floor or wall of the cargo compartment. Therefore, the load distribution plate and the cargo transport container can be easily and safely fixed.
  • FIG. 1 is an external perspective view conceptually showing the structure of a load distribution plate according to Embodiment 1.
  • FIG. FIG. 3 is a diagram conceptually showing the structure of a load distribution plate according to Embodiment 1, and is a cross-sectional view taken along the line II in FIG. It is a figure which shows notionally the structure of the load distribution board which concerns on Embodiment 1, and is sectional drawing which expanded and showed the area
  • region shown by A in FIG. 1 is a perspective view conceptually showing the structure of a freight transport container used in Embodiment 1.
  • FIG. 3 is a conceptual plan view for explaining a cargo carry-in operation according to the first embodiment.
  • FIG. 3 is a conceptual cross-sectional view for explaining a cargo carry-in operation according to the first embodiment.
  • FIG. 3 is a conceptual cross-sectional view for explaining a cargo carry-in operation according to the first embodiment.
  • 6 is an external perspective view conceptually showing the structure of a load distribution plate according to Embodiment 2.
  • FIG. 5 is an enlarged cross-sectional view conceptually showing a main part structure of a load distribution plate according to Embodiment 2.
  • FIG. 1 is an external perspective view conceptually showing an example of an aircraft to which the present embodiment is applied.
  • the small aircraft 100 has a cargo compartment 110.
  • the cargo compartment 100 is provided, for example, in the lower rear part of the fuselage.
  • a loading / unloading port 111 for loading / unloading the cargo transport container 130 into / from the cargo compartment 110 from the outside of the aircraft is provided.
  • the loading / unloading port 111 is opened and closed by a hatch 112.
  • a mechanism for transferring the cargo transport container 130 between the load / unload port 111 and the ground is used.
  • a mechanism for example, a belt loader 120, a lift loader (not shown), or the like can be employed.
  • the load distribution plate 200 is installed on the floor wall of the cargo compartment 110.
  • FIG. 2 is an external perspective view conceptually showing the structure of the load distribution plate 200 according to the present embodiment.
  • FIG. 3 is a cross-sectional view taken along the line II of FIG. 4 is an enlarged cross-sectional view of the region indicated by A in FIG.
  • a plurality of load distribution plates 200 as shown in FIGS. 2 to 4 are installed in one cargo compartment (see FIG. 7).
  • the load distribution plate 200 of the present embodiment includes a main body 201, an adhesion film 202, and a hard plate 203, and a caster guide groove 204 is provided on the upper surface.
  • the bottom surface of the main body 201 is formed in a shape that fits with the floor wall 113 of the cargo compartment 110. That is, on the bottom surface of the main body 201, the flat surface portion 201a and the inclined portion 201b are formed.
  • the main body 201 is desirably formed of a material that is lightweight and has high resistance to load.
  • a material that satisfies such conditions is a urethane material.
  • the urethane-based material can withstand a load of about 2 tons per square meter, and therefore is difficult to damage the floor wall 113.
  • urethane materials are easy to process and mold and are inexpensive.
  • the dimensions of the main body 201 are, for example, a width (that is, a length in the width direction of the aircraft 100) 1560 mm, a length (that is, a length in the length direction of the aircraft 100) 793 mm, and a height 50 mm.
  • the main body 201 is preferably subjected to waterproofing on the outer surface.
  • the adhesion film 202 is formed on the lower surface of the main body 201.
  • the adhesion film 202 is provided to adhere the floor wall 113 and the bottom surface of the main body 201.
  • the load distribution plate 200 can be prevented from being displaced when the aircraft 100 is inclined during flight or the like, and the durability of the main body 201 can be enhanced.
  • the adhesion film 202 for example, silicone rubber can be used.
  • the hard plate 203 is installed on the upper surface of the main body 201. Then, the cargo transport container 130 is transported and placed on the hard plate 203. By providing the hard plate 203, the strength of the load distribution plate 200 can be secured, and damage to the main body 201 can be prevented.
  • the hard plate 203 a single plate may be used or a plywood may be used. In the present embodiment, a plywood formed by attaching aluminum thin plates 203b and 203c to the front and back surfaces of the foamed polyethylene plate 203a is used as the hard plate 203 (see FIG. 4). This plywood has the characteristics of low weight and sufficiently high strength.
  • the thickness of the hard plate 203 is 3 mm, for example.
  • a large number of protrusions 205 are formed on the surface of the hard plate 203.
  • a protrusion 205 can be formed, for example, by embossing the surface of the aluminum thin plate 201b.
  • the protrusion 205 also functions as a slip stopper for a cargo transport container (described later).
  • other anti-slip means may be provided.
  • the caster guide groove 204 is a groove for guiding a caster (described later) of the cargo transport container 130.
  • a concave stainless steel caster rail 204a is embedded in the main body 201, and a caster guide groove 204 is provided by disposing a reinforcing aluminum plate (thickness, for example, 3 mm) 204b on the bottom surface of the caster rail 204a. (See FIG. 4). Since the direction of the caster differs by 180 degrees between loading and unloading, the width of the caster guide groove 204 is set such that the caster can rotate 180 degrees horizontally.
  • the number of caster guide grooves 204 may be determined according to the maximum weight or the like of the cargo transport container, but in the present embodiment, the number is three. However, the caster guide groove 204 may be two, or four or more. By providing the caster guide groove 204, it is possible to efficiently perform the work of transporting and carrying cargo using the casters in a short time.
  • the hard plate 203 and the caster guide groove 204 are fixed to the main body 201 using, for example, a plurality of dish rivets 206 having a diameter of 4.8 mm.
  • the floor wall 113 is provided with attachments 115 for fixing the cargo transport container to the floor wall 113 at predetermined intervals.
  • the fixture 115 is provided on the inclined portion 113 a of the floor wall 113, but may be provided on the flat portion 113 b of the floor wall 113 or may be provided below the side wall 114. Since such an attachment 115 is also provided in the cargo compartment 110 of the conventional small aircraft 100 (generally referred to as a fitting point), detailed description thereof is omitted.
  • FIG. 5 is a perspective view conceptually showing the configuration of the cargo transport container 130 used in the present embodiment.
  • the freight transport container 130 of this embodiment includes a base pallet 510 and a container body 520.
  • the base pallet 510 includes, for example, a resin base plate 511, an aluminum base frame 512, and a caster elevating mechanism (not shown).
  • the caster lifting mechanism lifts and lowers a caster (not shown in FIG. 5) for transporting the cargo transport container 130.
  • a caster not shown in FIG. 5
  • the lever 513 When the lever 513 is in the position shown in FIG. 5, the casters 514 are accommodated in the freight transport container 130 (see FIG. 8 described later).
  • the lever 513 When the lever 513 is pushed down in the direction indicated by B in FIG. 5, the casters 514 are lowered and exposed from the lower surface of the cargo transport container 130 (see FIG. 9 described later).
  • the dimensions of the casters 514 such as the width and interval are determined so that when the casters 514 are lowered, they can be arranged and moved in the corresponding caster guide grooves 204.
  • two notches 514 for exposing the fixture 115 are formed on both side portions of the base plate 511.
  • FIG. 5 only the notch portion 514 provided on one side surface portion is shown.
  • the container body 520 includes a front surface portion 521, a back surface portion 522, left and right side surface portions 523 and 524, and a ceiling portion 525, and is configured to be openable from the front surface portion 521 to the ceiling portion 525.
  • Each of these portions 521 to 525 can be manufactured using a synthetic resin plate or the like.
  • the front part 521 and the ceiling part 525 can be fixed in a closed state using, for example, hook-and-loop fasteners 526a and 526b.
  • FIG. 6 is a conceptual diagram showing a freight transport container fixing structure according to the present embodiment.
  • the freight transport container 130 placed on the load distribution plate 200 is covered with a net 610 as a covering material.
  • Two kinds of straps 621 and 622 are fixed to the net 610 at two positions respectively corresponding to both side surfaces of the cargo transport container 130.
  • Each strap 621, 622 is provided with length adjusters 621a, 622a for adjusting the strap length.
  • the net 610 is secured to the base pallet 510 of the cargo transport container 130 using the strap 621. Further, the net 610 is secured to a fixture 115 provided on the floor wall 113 of the cargo compartment using a strap 622. By the strap 622, the cargo transport container 130 is pressed against the load distribution plate 200 and the floor wall 113 and fixed.
  • the net 610 may replace with the net
  • the net 610 is required to have a strength that can withstand a predetermined tensile load (for example, about 1 ton). The strength of the net 610 may be determined according to the limit load determined by the aircraft manufacturer for each aircraft.
  • the cargo transport container 130 placed on the load distribution plate 200 is fixed to the fixture 115 provided on the floor wall 113 or the side wall 114 of the cargo chamber 110 via the net 610. Tie up. Therefore, the freight transport container 130 can be fixed more firmly than when the rope is tied to the left and right.
  • FIGS. 8 and 9 are sectional views.
  • a plurality of load distribution plates 200 are laid on the floor wall 113 of the cargo compartment 110.
  • the load distribution plates 200 are arranged in the longitudinal direction of the small aircraft 100 so that the caster guide grooves 204 are connected to each other (see FIG. 7).
  • the adhesion film 202 is provided on the bottom surface of the load distribution plate 200, the load distribution plate 200 can be stably fixed to the floor wall 113.
  • the hatch 112 of the cargo compartment 110 is opened, and a belt loader 120 or the like is installed between the ground and the loading / unloading port 111. Then, using this belt loader 120 or the like, the cargo transport container 130 is raised from the ground to the height of the loading / unloading port 111 and then loaded into the cargo chamber 110. Note that the caster 514 of the freight transport container 130 is in a raised state, that is, accommodated in the freight transport container 130 (see FIG. 8) during transport by the belt loader 120 or the like.
  • an operator places the cargo transport container 130 at a predetermined position on the load distribution plate 200.
  • the worker pushes down the lever 513 of the cargo transport container 130 in the direction indicated by B in FIG.
  • the caster 514 is lowered, and the lower portion thereof is exposed downward from the cargo transport container 130.
  • the caster 514 is accommodated in the caster guide groove 204 and exposed from the lower surface of the cargo transport container 130.
  • the casters 514 push up the main body of the cargo transport container 130 from the surface of the load distribution plate 200 (see FIG. 9). As a result, the freight transport container 130 can be transported by the casters 514.
  • the freight transport container 130 When the worker pushes the freight transport container 130, the freight transport container 130 is guided in the caster guide groove 204 and is transported in the cargo chamber 110. As described above, since a large number of protrusions 205 are provided on the surface of the load distribution plate 200, it is difficult for the operator's feet to slip when pushing the freight transport container 130, thus ensuring the safety of the operator. Work efficiency is improved.
  • the worker pushes up the lever 513 of the cargo transport container 130 to the position shown in FIG. Thereby, the caster 514 is accommodated in the freight transport container 130 (see FIG. 8). As a result, the cargo transport container 130 is lowered and the base plate 511 is in contact with the load distribution plate 200.
  • the worker covers the cargo transport container 130 with the net 610, and further fixes the net 610 to the load distribution plate 200 and the fixture 115 using the straps 621 and 622. Thereby, the carrying-in work of the cargo transport container 130 is completed.
  • the load distribution plate 200 is installed on the floor wall 113 of the cargo chamber 110, and the cargo transport container 130 can be transported and fixed on the load distribution plate 200. it can. Therefore, compared with the case where an operator pushes the cargo transport container 130 placed directly on the floor wall 113 of the cargo chamber 110 and loads / unloads the cargo, the loading / unloading operation is facilitated. According to the study of the present inventor, by using the load distribution plate 200 of the present embodiment, for example, one worker can carry a cargo transport container 130 of about 1 ton.
  • the adhesion film 202 is provided on the lower surface of the main body 201 of the load distribution plate 200, it is possible to prevent the load distribution plate 200 from being displaced when the small aircraft 100 is inclined during flight or the like. Thereby, since it is not necessary to mechanically fix the load distribution plate 200 to the floor wall 113, it is easy to remove at the time of inspection or the like. In addition, by providing the adhesion film 202, the load distribution plate 200 can be prevented from being damaged.
  • the hard plate 203 is provided on the main body 201 of the load distribution plate 200, the load applied to the main body 201 can be dispersed, thereby preventing the main body 201 from being damaged.
  • the main body 201 is formed of a urethane-based material, and a plywood made of the foamed polyethylene plate 203a and the aluminum thin plates 203b and 203c is used as the hard plate, so that a very lightweight load distribution plate 200 is obtained. be able to.
  • the load distribution plate 200 having the above-mentioned dimensions is about 10 kilograms, and can be transported and installed by an operator alone, and can be removed at the time of airframe inspection. Is possible.
  • the net 610 to which the straps 621 and 622 are fixed is used, so that the cargo transport container 130 is firmly fixed. be able to.
  • the cargo transport container 130 shown in FIG. 5 is merely an example of the cargo that can be applied to the present embodiment.
  • the load distribution plate 200 and the freight transport container fixing structure according to this embodiment can be applied to a freight transport container having another structure.
  • the effects of the present embodiment as described above can be obtained.
  • Embodiment 2 of the present invention a load distribution plate and a freight transport container fixing structure according to Embodiment 2 of the present invention will be described with reference to FIGS.
  • This embodiment is different from the above-described first embodiment in that a caster that can be moved up and down is provided on the load distribution plate.
  • FIG. 10 is an external perspective view conceptually showing the structure of the load distribution plate 1000 according to the present embodiment.
  • FIG. 11 is an enlarged cross-sectional view conceptually showing the main structure of the load distribution plate 1000 according to this embodiment. 10 and 11, the same reference numerals as those in FIGS. 2 and 4 denote the same components as those in FIGS. 2 and 4.
  • the load distribution plate 1000 includes an elevating roller device 1010 instead of the caster guide groove 204 of the load distribution plate 200 according to the first embodiment. Yes.
  • the elevating roller device 1010 includes a plurality of rollers 1011 configured to be rotatable and a roller elevating mechanism 1012.
  • the roller lifting mechanism 1012 moves the roller 1011 up and down.
  • the technology disclosed in British Patent 2376869 can be used.
  • the roller 1011 When transporting the cargo transport container, the roller 1011 rises to lift the cargo transport container. When the worker pushes the cargo transport container, the roller 1011 rotates and the cargo transport container moves. Thereby, it will be in the state which can be easily conveyed only by a worker pushing with a weak force.
  • the roller lifting mechanism 1012 lowers the roller 1011 to a position lower than the hard plate 203 of the load distribution plate 200. As a result, the cargo transport container is lowered, and the base plate 511 of the cargo transport container comes into contact with the hard plate 203.
  • load distribution plate 1000 is the same as those of the load distribution plate 200 of the first embodiment (see FIGS. 2 to 4), and thus the description thereof is omitted.
  • the lifting roller device 1012 is provided on the load distribution plate 1000, it is not necessary to provide a caster lifting mechanism on the cargo transport container side. Therefore, even when an inexpensive item that has been conventionally used as a freight transport container is used as it is, the carrying-in / out operation can be performed efficiently in a short time.
  • the present invention is applied to the cargo compartment 110 of the small aircraft 100 as an example.
  • the present invention can be applied regardless of the scale and model of the aircraft. is there.
  • the present invention is particularly useful for an aircraft provided with a small cargo compartment.

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  • Aviation & Aerospace Engineering (AREA)
  • Pallets (AREA)
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Abstract

La présente invention concerne une plaque de répartition de charge pour avion, la plaque de répartition de charge étant prévue pour être installée sur la surface de plancher de la soute à fret. La présente plaque de répartition de charge comporte : une section de corps dotée d'une surface inférieure présentant une forme qui coopère avec la paroi de plancher d'une soute à fret ; un film de contact rapproché formé sur la surface inférieure de la section de corps afin d'amener la paroi de plancher de la soute à fret et la surface inférieure de la section de corps en contact rapproché entre elles ; et une plaque dure disposée sur la surface supérieure de la section de corps et permettant de placer une cargaison sur celle-ci. L'utilisation de la présente plaque de répartition de charge permet d'étaler une charge agissant sur la surface de paroi inférieure de la soute à fret de l'avion, afin de prévenir toute rupture, déformation, etc. de la paroi inférieure.
PCT/JP2011/058247 2011-03-31 2011-03-31 Plaque de répartition de charge pour avion, et structure de fixation pour conteneurs de transport de fret l'utilisant WO2012131987A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/JP2011/058247 WO2012131987A1 (fr) 2011-03-31 2011-03-31 Plaque de répartition de charge pour avion, et structure de fixation pour conteneurs de transport de fret l'utilisant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2011/058247 WO2012131987A1 (fr) 2011-03-31 2011-03-31 Plaque de répartition de charge pour avion, et structure de fixation pour conteneurs de transport de fret l'utilisant

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WO2012131987A1 true WO2012131987A1 (fr) 2012-10-04

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Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0369629U (fr) * 1989-11-14 1991-07-11
JPH1142653A (ja) * 1997-07-25 1999-02-16 Dainippon Ink & Chem Inc パネル材及びその製造方法
JP2002514554A (ja) * 1998-05-11 2002-05-21 バーナム サーヴィス カンパニー インコーポレイテッド 整列されたもしくはオフセット車輪を有する物品を保管するためのパレット
US20030017037A1 (en) * 2001-07-20 2003-01-23 Steven Turner Mechanical handling apparatus
JP2007176533A (ja) * 2005-12-27 2007-07-12 Sekisui Plastics Co Ltd 樹脂製パレットおよびその製造方法
US20080302913A1 (en) * 2007-06-11 2008-12-11 The Boeing Company Cargo floor, system, and method
JP2009166748A (ja) * 2008-01-18 2009-07-30 Yoshiki Kitami 航空貨物輸送用固定具
JP3154138U (ja) * 2009-07-17 2009-10-08 合資会社エス．ピー．オー パレット
JP2010529925A (ja) * 2007-06-15 2010-09-02 エアバス オペラシオン 航空機の貨物室内の特に荷物のための移送装置
JP2010265005A (ja) * 2009-05-14 2010-11-25 Nippon Zeon Co Ltd 航空機用コンテナ

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0369629U (fr) * 1989-11-14 1991-07-11
JPH1142653A (ja) * 1997-07-25 1999-02-16 Dainippon Ink & Chem Inc パネル材及びその製造方法
JP2002514554A (ja) * 1998-05-11 2002-05-21 バーナム サーヴィス カンパニー インコーポレイテッド 整列されたもしくはオフセット車輪を有する物品を保管するためのパレット
US20030017037A1 (en) * 2001-07-20 2003-01-23 Steven Turner Mechanical handling apparatus
JP2007176533A (ja) * 2005-12-27 2007-07-12 Sekisui Plastics Co Ltd 樹脂製パレットおよびその製造方法
US20080302913A1 (en) * 2007-06-11 2008-12-11 The Boeing Company Cargo floor, system, and method
JP2010529925A (ja) * 2007-06-15 2010-09-02 エアバス オペラシオン 航空機の貨物室内の特に荷物のための移送装置
JP2009166748A (ja) * 2008-01-18 2009-07-30 Yoshiki Kitami 航空貨物輸送用固定具
JP2010265005A (ja) * 2009-05-14 2010-11-25 Nippon Zeon Co Ltd 航空機用コンテナ
JP3154138U (ja) * 2009-07-17 2009-10-08 合資会社エス．ピー．オー パレット

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