WO2001034501A1 - Conteneur pour cargaisons sensibles - Google Patents

Conteneur pour cargaisons sensibles Download PDF

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Publication number
WO2001034501A1
WO2001034501A1 PCT/SE2000/002202 SE0002202W WO0134501A1 WO 2001034501 A1 WO2001034501 A1 WO 2001034501A1 SE 0002202 W SE0002202 W SE 0002202W WO 0134501 A1 WO0134501 A1 WO 0134501A1
Authority
WO
WIPO (PCT)
Prior art keywords
container
load device
unit load
profiles
air
Prior art date
Application number
PCT/SE2000/002202
Other languages
English (en)
Inventor
Stefan Norelius
Original Assignee
Envirotainer Engineering Ab
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
Publication date
Application filed by Envirotainer Engineering Ab filed Critical Envirotainer Engineering Ab
Priority to DE60013908T priority Critical patent/DE60013908T2/de
Priority to AU13225/01A priority patent/AU1322501A/en
Priority to JP2001536457A priority patent/JP2003513865A/ja
Priority to EP00975132A priority patent/EP1248738B1/fr
Priority to AT00975132T priority patent/ATE276170T1/de
Publication of WO2001034501A1 publication Critical patent/WO2001034501A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/02—Wall construction
    • B65D90/06—Coverings, e.g. for insulating purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00—Large containers
    • B65D88/02—Large containers rigid
    • B65D88/12—Large containers rigid specially adapted for transport
    • B65D88/14—Large containers rigid specially adapted for transport by air
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D88/00—Large containers
    • B65D88/74—Large containers having means for heating, cooling, aerating or other conditioning of contents
    • B65D88/745—Large containers having means for heating, cooling, aerating or other conditioning of contents blowing or injecting heating, cooling or other conditioning fluid inside the container
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00—Component parts, details or accessories for large containers
    • B65D90/02—Wall construction
    • B65D90/08—Interconnections of wall parts; Sealing means therefor

Definitions

  • the present invention relates in general to freight containers and in particular to air-cargo containers or other ULD:s (Unit Load Devices) equipped for transporting sensitive cargo.
  • ULD Unit Load Devices
  • Some goods to be transported by air-freight may require extremely clean conditions, usually called clean room conditions.
  • clean room conditions The number of particles in the air, the atmosphere composition etc. has to be carefully controlled.
  • a container for transporting of such goods thus has to be carefully sealed, in order to maintain the clean conditions inside.
  • No exchange of air between the inside and the outside of the container is admitted. This puts a number of constraints on the container construction.
  • the container When transporting a container in an air plane, the container must be possible to open extremely fast, if a sudden drop of pressure occurs during the flight, in order to prevent the container from exploding. Regulations state that the container has to be possible to evacuate within 0.2 seconds. In containers having an admitted air flow in and out from the container a double directed valve may be provided for this purpose. In containers having clean room conditions inside, such a solution is totally out of the question.
  • a general object of the present invention is thus to provide a container suitable for air-freight with improved possibilities to handle sensitive goods.
  • An object of the present invention is to provide an air-freight container which provides clean room conditions for the cargo compartment.
  • a further object of the present invention is to provide an air-freight container with improved properties concerning thermal isolation.
  • Another object of the present invention is to provide an air- freight container designed for high point loads.
  • Yet another object of the present invention is to provide an air-freight container with an increased admitted cargo volume.
  • the container is sealed for obtaining clean room conditions during transportation.
  • a control compartment is provided at one end of the container, handling temperature and humidity control.
  • a blow out panel is provided at the wall separating the cargo compartment from the control compartment.
  • a container with a height exceeding the normal container heights for air-cargo containers is provided.
  • the increased ceiling height is provided in a central part of the container, sloping towards the longitudinal edges, extending along the entire longitudinal edge.
  • At least one of the short sides presents a cut-away portion extending along the entire length of the short side, in order to facilitate loading in an air plane.
  • the container is built from a framework of profiles connected by thermally insulated panels.
  • the profiles are preferably produced in two major metallic parts, interconnected by polymer connection profiles, in order to break heating bridges.
  • the base of the container is preferable built by an inner base of a panel, formed by two parallel sheets interconnected by vertical plates, attached to an outer base built of a framework of profiles. Attachment means, secured at the bottom side of the inner base, are provided for allowing point loads to be secured safely.
  • FIG. 1 is a schematic drawing of an embodiment of a container according to the present invention.
  • FIG. 2a-c are transversal cross-sections of a container according to the present invention.
  • FIG. 3a, 3b are longitudinal cross-sections of a container according to the present invention
  • FIG. 4a is cross-sections of a construction profile, which can be used as a door frame of a container according to the present invention
  • FIG. 4b is cross-sections of a construction profile, which can be used in a corner of a container according to the present invention.
  • FIG. 5 is a schematic drawing of a base element of a container according to an embodiment of the present invention.
  • FIG. 6a, 6b are details of the drawing in fig. 5.
  • Unit Load Device is a common term including different types of containers for air-freight.
  • ULD Unit Load Device
  • the use of the term ULD implies the intended use of the device for air-freight, and the requirements and problems connected therewith.
  • FIG. 1 illustrates an embodiment of the present invention.
  • An air-freight container generally referred to as 1 , comprises a base 10, side walls 12, 14, end walls, 16, 18 and a ceiling 20.
  • the walls 12- 18 and the ceiling 20 are typically built by thermally insulating panels, connected by profiles.
  • the profiles are normally provided in each corner of the container 1 , but may also be used elsewhere, where there is need for a structural enhancement.
  • the container of the present embodiment is primarily intended to be used as an air-freight container.
  • the construction as such can be used as a land or sea freight container as well.
  • the central invention features solve problems connected with air- freight, and hence, the enclosed claims are only directed to containers for use in air-freight.
  • the container is provided with lifting and attachment means according to appropriate standards.
  • the lifting means are e.g. provided at a certain position, and the width and length of the container is also according to relevant standards.
  • For air-cargo containers there are other standards that have to be met, which normally gives a maximum height of the container. The standards puts some limitations on the shape and size of the container. So does also the measures of the air planes.
  • An air-cargo container is e.g. typically not higher than about 9 feet (2.8 meters), in order to fit into either of two positions in an upper deck cargo room of a Boeing 747 freighter.
  • An air-cargo container is e.g. typically not higher than about 9 feet (2.8 meters), in order to fit into either of two positions in an upper deck cargo room of a Boeing 747 freighter.
  • large cargo units are requested to be transported by air. If the height of the cargo unit exceeds the available inside measures of a container according to the air-cargo container standards, the unit has to be dissembled before transport.
  • the useful height of an air-cargo container 1 may be increased, at least for a part of the loading area.
  • the height limitations are set by the rounded-off shape of the cargo room. Since there are normally two positions in the cargo room, the limitations are really only present at one side of the container, since the ceiling of the cargo room increase towards the middle.
  • the container 1 may still be possible to load in e.g. a Boeing 747 freighter.
  • the portion of the ceiling 20 with reduced height 24, 26 may be present only at the side positioned against the wall of the air plane cargo room, but in order to be able to position the container 1 in any position in the cargo room, the portion of reduced height 24, 26 is preferably present at both sides of the container. However, the portion of reduced height 24, 26 always extends along the entire length of the container.
  • the central part 22 of the container thus has ceiling height which may be considerably higher than with conventional containers.
  • this height reduction 28 towards the end door is only provided at one side.
  • the height reduction 28 may be present at both sides, but will then either give a door height which is lower than the maximum height within the container, or give a complex design of the doors.
  • the portions with reduced height 24, 26, 28 may be designed in different ways.
  • the portion is divided into three parts, two side parts 24, 26, comprising sloping flat panels between the horizontal maximum height portion 22 and the side walls 12, 14, and one end part, which provides a recess 28 in the ceiling 20.
  • Fig. 2a-c illustrates the transversal cross section profile (taken along a line as illustrated by the line 2-2 in fig. 1) of a number of embodiments according to the present invention.
  • one side is provided by a sloping plane 30, while the other side has the full height 22.
  • Such a container may normally only be loaded into one particular side of the air plane.
  • both sides are provided with recesses 32, 34, leaving a rectangular central volume 22.
  • the sides of the ceiling are rounded off, providing a generally arc- shaped ceiling 36.
  • the end part 28 of the portion with reduced height may be designed with different shapes.
  • a few embodiment are illustrated as longitudinal cross sections of a container (taken along a line as illustrated by the line 3-3 in fig. 1) in fig. 3a and 3b.
  • both ends of the container are provided with a ceiling recess 38, 40.
  • fig. 3b only one of the ends has a decreased height portion, comprising a flat sloping portion 42.
  • the goods transported by a container 1 require a certain temperature.
  • the container may be equipped with heating and /or cooling arrangements.
  • the heat content of the transported goods is normally quite large, and the temperature may often be maintained within a admitted temperature interval just by providing a very good heat insulation of the container 1.
  • the container 1 of fig. 1 is built by thermally insulated panels interconnected by profiles. The heat conductance through the panels is very low and the major heat transportation through the container walls usually takes place through the profiles, which typically are made of aluminium.
  • the profile arrangement comprises an outer metallic profile portion 62 and an inner metallic profile portion 60. These metallic profile portions 60, 62 are preferably of aluminium.
  • the outer profile portion 62 and the inner profile portion 60 are interconnected by a number of distance profiles 70 made of a heat insulating material, preferably polymer material.
  • the distance profiles 70 maintains the outer and inner profile portions 60, 62 separated in order to break any heat conducting bridges through the wall.
  • the inner profile portion 60 comprises an inner retaining projection 76 and the outer profile portion 62 comprises an outer retaining projection 78.
  • the insulating panels are positioned between these retaining projections and fastened thereto.
  • the insulating panels are typically made of an outer polymer surface 66, and an inner polymer surface 68, between which an insulating material 64 is arranged.
  • the profiles 60, 62, 70 are serving as structural members of the container 1 , providing rigidity and load bearing means.
  • aluminium profiles may be too weak, in particular in the vicinity of e.g. doors.
  • the profiles are then preferably designed forming cavities 72, closed or open, into which structural strength enhancing elements, such as steel beams may be introduced.
  • the profile may also preferably be formed to provide the stationary part of a hinge for the container doors. The entire hinge may then easily be folded into the container wall, not requiring any space outside the surface of the wall. This reduces the risk for damages of such details.
  • the outer profile portion may preferably also be provided with a sealing surface 73, against which the doors sealing is arranged when the door is closed.
  • the sealing surface 73 is preferably inclined, having a thicker measure at the inner side than at the outer side.
  • a closed container 1 in which a pressure lower than the surroundings have is present, is difficult to open unless the pressure difference is removed.
  • the inclined surface 73 facilitates the opening of a door, since it almost immediately admits an air passage upon opening the door.
  • the profiles may also be used in ordinary corners without door arrangements. Such a profile arrangement is schematically illustrated in fig. 4b.
  • both metal profile portions 60, 62 have retaining projections 76, 78 in two directions, being capable of connecting two wall or ceiling panels 64- 68.
  • the actual design of the profiles are adjusted according to the requirements, and many modifications and variations are thus possible.
  • the container 1 in fig. 1 is intended to be used for clean room conditions.
  • a separate control compartment 44 is provided.
  • equipment for regulating the temperature and humidity of the cargo compartment 50 of the container 1 is placed (not shown in the figure for the sake of clarity).
  • the climate equipment may e.g. comprise a heater, a cooler and a humidity controlling device.
  • these components may be driven either by an electric motor or a diesel motor, depending on the available electrical connections. During flight, the motors have to be turned off due to safety regulations.
  • the control compartment 44 is separated from the cargo compartment 50 by a separating wall 46.
  • a blow out panel 48 is arranged at the separating wall 46.
  • the pressure drop will rapidly evacuate the control compartment 44, which is connected with the outside by large ventilation openings.
  • the pressure difference between the cargo compartment 50 and the control compartment 44 will be the same as the pressure different over any other of the walls of the cargo compartment 50.
  • the blow out panel 48 is arranged to be released at a certain pressure difference, and the air of the container evacuates easily through the control compartment 44.
  • the blow out panel 48 When the blow out panel 48 releases, the pressure at the blow out panel 48 is so high that the blow out panel 48 will be thrown with a large force out from the separating wall 46.
  • the outer wall 18 of the control compartment 44 will prevent the blow out panel 48 from leaving the container 1 , thus also preventing it from damaging the air plane itself or any persons within the cargo room of the air plane. By letting the blow out panel 48 be released into the control compartment 44, the external damage caused by such an action will be reduced.
  • the base 10 comprises a lower, outer base portion 80 and an upper, inner base portion 86.
  • the outer base portion 80 is structurally rigid and preferably formed as a framework of beams 82.
  • the interspaces 84 within the outer base portion 80 are preferably filled with thermally insulating material.
  • the inner base portion 86 is secured to the outer base portion 80 e.g. by means of screwing it to the beams 82 of the outer base portion 80.
  • the inner base portion 86 is as shown in fig. 6a and 6b (which are detail drawings of the encircled part in fig.
  • the plates 96 are preferably formed and positioned in closed geometrical patterns, with the plates 96 directed in at least two distinctive directions.
  • a simple and preferred arrangement is a honeycomb pattern, as illustrated by fig. 6b.
  • Such an arrangement creates an inner base portion 86, which has a high rigidity for local strains.
  • a closer arrangement of vertical plates 96 gives a higher load carrying capacity and a stiffer inner base portion 86. Since the inner base portion 86 furthermore is firmly fixed to the rigid outer base portion 80, the assembly achieves a property of distributing point loads in an efficient way.
  • Attachment means 90 are provided at the inner base portion 86.
  • the attachment means 90 are reachable from above, i.e. from the inside of the container 1 , available for firmly fixing the load to the container floor.
  • the attachment means 90 are firmly secured against the lower cover sheet 94 of the inner base portion 86, preferably from below, in order to use the rigidity and bending properties of the inner base portion 86.
  • the attachment means comprises a base plate 98, screwed or riveted 102 to the bottom side of the lower cover sheet 94. From the base plate 98, a tube member 100 with inner threads extends through the inner base portion 86. The threaded tube 100 hence offering a secure attachment point for heavy point loads.
  • the attachment means 90 will withstand a vertical load of 60 kN and a horizontal load of 150 kN.
  • the floor should carry 2 tons per point and withstand collision forces of 2 G.
  • the present construction will carry 15 tons per point and withstand 6 G.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Packages (AREA)
  • Body Structure For Vehicles (AREA)
  • Laminated Bodies (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Liquid Crystal (AREA)
  • Wrappers (AREA)

Abstract

La présente invention concerne un conteneur de frêt aérien scellé pour obtenir des conditions de salle propre pendant le transport. Ce conteneur est doté à une extrémité d'un compartiment de commande (44). Un panneau éjectable (48) est situé au niveau de la paroi séparant le compartiment à marchandises (50) du compartiment de commande (44). Le conteneur a, de préférence, une hauteur dépassant les hauteurs normales des conteneurs de frêt aérien. La hauteur augmentée du plafond est obtenue par un élément central (22) du conteneur, tandis que des parties (24, 26, 28) de hauteur réduite sont situées au moins le long d'une des parois latérales (12, 14) et d'une des parois terminales (16, 18) sur toute la longueur de la paroi. Le conteneur est constitué d'un cadre de profilés reliés par des panneaux thermiquement isolés. Les profilés sont, de préférence, constitués de deux éléments principalement métalliques reliés par des profilés raccords polymère.
PCT/SE2000/002202 1999-11-12 2000-11-10 Conteneur pour cargaisons sensibles WO2001034501A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE60013908T DE60013908T2 (de) 1999-11-12 2000-11-10 Behälter für empfindliche fracht
AU13225/01A AU1322501A (en) 1999-11-12 2000-11-10 Container for sensitive cargo
JP2001536457A JP2003513865A (ja) 1999-11-12 2000-11-10 繊細な貨物用コンテナ
EP00975132A EP1248738B1 (fr) 1999-11-12 2000-11-10 Conteneur pour cargaisons sensibles
AT00975132T ATE276170T1 (de) 1999-11-12 2000-11-10 Behälter für empfindliche fracht

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE9904127-9 1999-11-12
SE9904127A SE516656C2 (sv) 1999-11-12 1999-11-12 Container lämplig för flygfrakt och känsligt gods

Publications (1)

Publication Number Publication Date
WO2001034501A1 true WO2001034501A1 (fr) 2001-05-17

Family

ID=20417724

Family Applications (2)

Application Number Title Priority Date Filing Date
PCT/SE2000/002203 WO2001034502A1 (fr) 1999-11-12 2000-11-10 Conteneur pour cargaisons sensibles
PCT/SE2000/002202 WO2001034501A1 (fr) 1999-11-12 2000-11-10 Conteneur pour cargaisons sensibles

Family Applications Before (1)

Application Number Title Priority Date Filing Date
PCT/SE2000/002203 WO2001034502A1 (fr) 1999-11-12 2000-11-10 Conteneur pour cargaisons sensibles

Country Status (7)

Country Link
EP (2) EP1248739B1 (fr)
JP (2) JP2003513865A (fr)
AT (2) ATE276170T1 (fr)
AU (2) AU1322601A (fr)
DE (2) DE60013908T2 (fr)
SE (1) SE516656C2 (fr)
WO (2) WO2001034502A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013077992A1 (fr) * 2011-11-25 2013-05-30 Thermo King Corporation Procédé d'essai en service d'un système de conditionnement d'air pour un conteneur

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE0300683L (sv) * 2003-03-13 2004-09-14 Aircontainer Ac Ab Flygfraktcontainer med temperaturregleringsenhet samt sådan temperaturregleringsenhet

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DE1816800A1 (de) * 1968-01-03 1969-07-31 Pressoturn Ltd Behaelter fuer Schuettgueter
DE1601899A1 (de) * 1967-09-07 1970-05-06 Linde Ag Luftfracht-Kuehlbehaelter
DE3151998A1 (de) * 1981-12-29 1983-07-07 Oskar Dittrich GmbH & Co KG Kiesgrubenbetrieb und Erdbewegungen, 1000 Berlin Wasserpflanzen-container mit klappenschliessvorrichtung
DE3709247A1 (de) * 1987-03-20 1988-10-06 Lonza Ag Frachtcontainer, insbesondere fuer luftfracht
WO1991007337A1 (fr) * 1989-11-08 1991-05-30 Royal Ordnance Plc Conteneurs utilises sur des avions pour la protection des structures de l'appareil
WO1992015507A1 (fr) * 1991-03-05 1992-09-17 Eurotainer Ab Conteneur de transport pour marchandises sensibles a la temperature
WO1992015506A1 (fr) * 1991-03-05 1992-09-17 Eurotainer Ab Conteneur de transport pour marchandises sensibles a la temperature
US5183176A (en) * 1989-11-14 1993-02-02 Meier & Niehaus Gmbh Lining for receptacles
WO1993022223A1 (fr) * 1992-04-29 1993-11-11 Royal Ordnance Plc Ameliorations relatives a des conteneurs amortissant le souffle d'une explosion
US5564599A (en) * 1995-03-15 1996-10-15 Hoover Group, Inc. Foldable shipping container
WO1997012195A1 (fr) * 1995-09-25 1997-04-03 Alliedsignal Inc. Conteneurs resistant aux explosions et canalisant l'onde de choc, et procedes de fabrication

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JPS6062095U (ja) * 1983-09-30 1985-04-30 昭和飛行機工業株式会社 コンテナにおけるフレキシブルドアの下縁フレ−ム
JPS63138933U (fr) * 1987-03-04 1988-09-13
JPS63162199U (fr) * 1987-04-14 1988-10-24
JPH0455193A (ja) * 1990-06-22 1992-02-21 Yokohama Rubber Co Ltd:The 燃料タンクコンテナーの衝撃吸収支持装置
JPH04270642A (ja) * 1991-02-06 1992-09-28 Mitsubishi Electric Corp 埋込部材を有するサンドイッチパネル
JP2510677Y2 (ja) * 1992-06-02 1996-09-18 槙雄 矢崎 保冷航空コンテナ
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Publication number Priority date Publication date Assignee Title
DE1601899A1 (de) * 1967-09-07 1970-05-06 Linde Ag Luftfracht-Kuehlbehaelter
DE1816800A1 (de) * 1968-01-03 1969-07-31 Pressoturn Ltd Behaelter fuer Schuettgueter
DE3151998A1 (de) * 1981-12-29 1983-07-07 Oskar Dittrich GmbH & Co KG Kiesgrubenbetrieb und Erdbewegungen, 1000 Berlin Wasserpflanzen-container mit klappenschliessvorrichtung
DE3709247A1 (de) * 1987-03-20 1988-10-06 Lonza Ag Frachtcontainer, insbesondere fuer luftfracht
WO1991007337A1 (fr) * 1989-11-08 1991-05-30 Royal Ordnance Plc Conteneurs utilises sur des avions pour la protection des structures de l'appareil
US5183176A (en) * 1989-11-14 1993-02-02 Meier & Niehaus Gmbh Lining for receptacles
WO1992015507A1 (fr) * 1991-03-05 1992-09-17 Eurotainer Ab Conteneur de transport pour marchandises sensibles a la temperature
WO1992015506A1 (fr) * 1991-03-05 1992-09-17 Eurotainer Ab Conteneur de transport pour marchandises sensibles a la temperature
WO1993022223A1 (fr) * 1992-04-29 1993-11-11 Royal Ordnance Plc Ameliorations relatives a des conteneurs amortissant le souffle d'une explosion
US5564599A (en) * 1995-03-15 1996-10-15 Hoover Group, Inc. Foldable shipping container
WO1997012195A1 (fr) * 1995-09-25 1997-04-03 Alliedsignal Inc. Conteneurs resistant aux explosions et canalisant l'onde de choc, et procedes de fabrication

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013077992A1 (fr) * 2011-11-25 2013-05-30 Thermo King Corporation Procédé d'essai en service d'un système de conditionnement d'air pour un conteneur
CN104053613A (zh) * 2011-11-25 2014-09-17 冷王公司 对集装箱的气候控制系统在服务中进行测试的方法
US9097456B2 (en) 2011-11-25 2015-08-04 Thermo King Corporation Method for in-service testing a climate control system for a container
US9971366B2 (en) 2011-11-25 2018-05-15 Thermo King Corporation Method for in-service testing a climate control system for a container

Also Published As

Publication number Publication date
EP1248738A1 (fr) 2002-10-16
ATE276170T1 (de) 2004-10-15
EP1248738B1 (fr) 2004-09-15
SE9904127L (sv) 2001-05-13
EP1248739B1 (fr) 2005-02-09
JP2003513866A (ja) 2003-04-15
EP1248739A1 (fr) 2002-10-16
JP2003513865A (ja) 2003-04-15
SE516656C2 (sv) 2002-02-12
WO2001034502A1 (fr) 2001-05-17
ATE288866T1 (de) 2005-02-15
DE60013908T2 (de) 2005-11-10
DE60018113T2 (de) 2006-03-30
SE9904127D0 (sv) 1999-11-12
AU1322601A (en) 2001-06-06
AU1322501A (en) 2001-06-06
DE60013908D1 (de) 2004-10-21
DE60018113D1 (de) 2005-03-17

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