Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.


  1. Advanced Patent Search
Publication numberUS3645596 A
Publication typeGrant
Publication dateFeb 29, 1972
Filing dateDec 30, 1969
Priority dateDec 30, 1969
Also published asDE2064241A1
Publication numberUS 3645596 A, US 3645596A, US-A-3645596, US3645596 A, US3645596A
InventorsRussell-French Harry M
Original AssigneeBoothe Airside Services
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Cargo container construction
US 3645596 A
This application discloses a cargo container construction which provides an erection and knockdown arrangement which keeps the parts together in knockdown condition so that no parts will be lost and so that all parts needed for reerection will be carried by the units handy for use when reassembly is desired; also a construction designed to form a package of minimum size in the dismantled or knockdown condition with full assurance that no parts will be lost and that no components will be crushed or marred if the dismantled packages are stacked on each other or with other goods for return shipment; and especially a construction which can be quickly and easily erected with full assurance that no parts will be missing.
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

United States Patent Russell-French Feb. 29, 1972 [54] CARGO CONTAINER CONSTRUCTION 3,414,156 12/1968 Felldin ..220/6 Inventor: igzrry- M. Russell-French, Philadelphia, Primary Examiner FranciS K. zugel Assistant Examiner-Darrell Marquette [73] Assignee: Boothe Airslde Services, Inc. Attorney-Stowe" & Stowell Y [22] Filed: Dec. 30, 1969 ABSTRACT 21 A l. N .2 889108 I l pp 0 I This application discloses a cargo container construction which provides an erection and knockdown arrangement U-S. CL. .t ..312/258,3l2/108,220/6 which keeps the parts together in knockdown condition SO 43/00,]365 7/28 that no parts will be lost and so that all parts needed for [58] Field of Search ..3l2/258,259,262, I08, 5, reflection will be carried by the units handy f use when 312/6; 220/6 reassembly is desired; also a construction designed to form a g package of minimum size in the dismantled or knockdown [56] I References cued condition with full assurance that no parts will be lost and that UNITED STATES PATENTS no components will be crushed or marred if the dismantled packages are stacked on each other or with other goods for 1,632,476 6/ 1927 Holderman et al. ..3l2/258 r t r hipment; and especially a construction which can be 212741048 2/1942 Denna" -312/259 quickly and easily erected with full assurance that no parts will 2,360,452 10/1944 Stone 312/259 be missing 3,064,569 11/1962 Rosenthal... ..220/6 2/1967 Nickel et al ..220/34 1 Claim, 13 Drawing Figures Patented. Feb. 29, 1972 q- Sheets-Sheet 1 INVENTOR. HARRY M. RUSSELL-FRENCH ATTORNEY Patented Feb. 29, 1972 4 Sheets-Sheet 5 HARRY M- RUSSELL-FRENCH ATTORNEY Patented Feb. 29, 1.972 3,645,596

4 Sheets-Sheet 4 W I {II l I I '"I I.

i M i i I 52 I I I u I I "1 I 53 I I J 50 I "I I I 52 l 53 I II I 52 I F/g.//

'mvsmom WM/Z.

ATTORNEY HARRY M. RUSSELL-FRENCH CARGO CONTAINER CONSTRUCTION BACKGROUND OF INVENTION Cargo containers of the general type dealt with in the presentinvention have previously been provided but for the most. part they have been assembled withloose parts such as bolts, screws, and the like, which are subject to loss when the container is dismantled for return, with the result that the containers often cannot be reassembled until missing units and assembly elements have been replaced; besides, the construction taking too much time to erect and dismantle.

SUMMARY OF THE INVENTION The present invention provides a container construction in which mostof the panels forming the-walls of the container are permanently-connected together in foldable condition, with other panels readily shiftable from assembled to dismantled condition and in which all of the units carry permanently with them captive-elements needed-.for securement in assembly so that no securement elements can be lost; also the panel units are so designed that they fit together to form a knockdown return package of minimum size and one which will readily stack with safety against damage.

DESCRIPTION OF DRAWINGS The objects, features, and advantages of the invention will be apparent fromthe following description of an exemplary embodiment, reference being made to the accompanying drawings thereof, wherein:

FIG. 1 is'a perspective view, largely diagrammatic, showing,

a container construction embodying the invention, the fore and aft doors being folded on top to show the interior;

FIG. 2 is an end elevation of the assembled knockdown package formed of the dismantled units;

FIG..3 is a longitudinal elevation of the knockdown package shown in FIG. 2;

FIG. 4 is an enlarged section of a typical inboard end-bottom corner construction, the view being taken about on the line 44 of FIG. 1;

FIG. 5.'is a view similar to FIG. 4 but showing an outboard corner construction, the view being taken about on the line 5-5 of-FIG. 1;

FIG. 6 is a view similar to FIG. 4 but showing a side construction with the door closed, the view being taken about on the line 66 of FIG. 1;

FIG. 7 is anenlarged section at the inboard top comer, the view being taken about on the line 7-7 of FIG. 1;

FIG. 8 is an enlarged section at the forward top corner with the door closed, taken about on the line 88 of FIG. 1;

FIG. 9 is a vertical section showing elevation of the shear panel;

FIG 10 is a vertical section showing the shelf mounting arrangement;

FIG. 11 is an enlarged horizontal partial section taken on the line 1lll ofFlG. 10;

FIG. 12 is an enlarged horizontal section at the side edge of the door, taken on the line l212 of FIG. 1;

FIG. 13 is a broken vertical longitudinal section showing a modified shelf mounting.

DESCRIPTION OF EXEMPLARY EMBODIMENT The container shown diagrammatically in FIG. 1 is of a shape adapted to fit in the cargo space of aircraft having sides sloping outward and upward from the floor. The container includes a base or floor panel 10, an inboard end panel 11, an outboard end panel 12 with lower inclined panel portion 12a hinged at 12b to anupper generally vertical panel portion 120, a top or roof .panel 13, a forward folding door panel 14, an aft or rear folding door panel 15, a vertical rigidifying shear panel 16, and shelves 17.

In the exemplary container shown, the top panel 13 has the greatest area, say 60 inches wide and 80 inches long, and is selected as a preferred foundation unit for the knockdown packageunit shown in FIGS. 2 and 3. The shelves fit within the interior space of the assembled erected container so they can be placed beneath the top panel to be completely covered by it while lying clear of the mounting elements on the top panel for the doors and end panels.

The top panel has depending end wall stub projection elements 20 and 21 at its ends, the vertically narrower of whichhere the inboard projection 20-is deep enough to provide space for the shelf members below the end member which is first folded over. To this projection the inboard end panel 11 is swingably connected, as by a piano-type hinge 22. The outboard stub projection element 21 is enough wider than the inboard one to accommodate for thefolded thickness of the first-folded end panel; andto the lower edge of this projection element 21 the upper panel portion 120 of the outboard end panell2 is swingably connected, as by a piano-type hinge 23.

The hinge 12b of the outboard end panel provides that the panel as a whole will lie flat when folded up.

While the inboard panel is shown to be folded-up before the outboard panel, the arrangement may be reversed.

The end panel units are shorter vertically than the top panel and narrower horizontally than the overall width of. the container with the doors closed, so are covered within the area of the top panel .when folded into knockdown assembly position.

The doors 14, 15 are permanently secured to the sides of the top panel by piano-type hinges 24. Each door comprises a pluralityof panel portions, three as shown, hinged together along adjacent horizontal edges but it is not necessary to consider these details except to-note that they may have resilient sealing'strips to form tight joints when closed. The top main hinge joint will be described hereinafter as an example.

The bottom or floor panel 10 and the shear panel 16 are separably vconnectedto associated parts in the erected assembly by captive fasteners carried by associated parts to be described, and when dismantled are placed on top of the assembly. The floor panel is shown below the shear panel in the knockdown assembly but the order may be changed if desired.

Theknockdown assembly can be held together as a unitary package in various ways, such as by strapping, clamping together, enclosing in protective coverings, or various other ways and it is not believed essential to describe any particular packaging securement for an understanding of the present invention.

The knockdown package of a container which, when erected, is about 60 inches wide by inches long and about 66 inches high is relatively light, say about 250 pounds when made largely of corrugated aluminum sheet material about I inch thick, and the depth of the knockdown package is less than 10 inches. The floor is preferably made of a strong light material, such as laminated balsa wood.

FIG. 4 shows a typical quick connection for the inboard end. Here the floor or base panel mat the ends is provided with an extruded stringer 30 of light material, such as aluminum, having spaced holes with female fastener elements 31 and an undercut goods-hold-down groove 32. The bottom of the inboard end panel II is provided with an extended stringer .33 which at spaced pointscarries captive tumable fastener clamping bolts 34, such as Simmons plate-type receptacle P-2, adapted to enter the holes and engage with the elements 31 to clamp the parts together when the elements 34 are turned.

The outboard connection is the same and the same reference characters are used, except that the stringer 33' is angular to conform to the inclined lower panel portion 12a.

On the sides for the doors, as shown in FIG.'6, the stringer 35 is quite similar to the end-stringers 30, having the same kind of goods-tie-down groove, but does not have fasteners for the door, these being on the sides of the doors.

The doors 14, 15, when closed, assist inholding the container in shape and for this purpose, as shown inFIG. 6, have shear pins 36 along the lower edge which enter holes in the rail or stringer 35 when the door is brought down. A plate 37 is secured to the inner side of the lower edge of the door and this plate wedges against the side of a flexible sealing strip 38 secured to the stringer 35 to seal against the entry of water. However, air can pass up corrugations of the door, which are open at the bottom, for ventilation; screening being provided over the corrugation ends to exclude vermin, if desired.

n the sides of the doors, FIG. 12, they are provided with edge strips 39 and shear pins 40 which enter holes in an edge strip 41 of the end panels, a resilient sealing strip 42 being provided between adjacent surfaces. The doors at various places,

at least at one place at each end of each subpanel portion of the doors, are pulled tight against the edges of the end panels by suitable latches of known swing-over and pull-in type, only the ends of the latches being shown. The latches are of such design that they lie within the thickness of the panels so as to avoid adding thickness in the knockdown package.

FIG. 9 shows in a general way how the shear panel 16 is secured in position when the container is erected. It is strengthened and rigidified by strip elements 45 around its edges. At the top it carries shear pins 46 which enter holes in a rib strip 47 carried by the top panel 13. The end panel 12 on each portion 120, 120 is provided with a rib 48 and between the elements 45 and the ribs 48 there are secured captive fastener elements, such as those already mentioned for securing the end panels to the floor panel. Herein such fastener connections are indicated at 49, in places without detail, the particular fastening means being subject to wide selection, the important point being that quick-acting captive fasteners which do not project to any extend from the sides of the panels will be used.

If the shear panel should extend out to the floor panel the floor panel can be provided with a medial strip and the'lower edge of the shear panel secured thereto in a manner like that described for securement to the end panel.

The shelves 17 need not be fastened down, merely supported on the end wall panels, desirablyby means which do not increase the panel thickness appreciably in knockdown assembly. In one form, shown in FIGS. 10, 11, the shelf support means comprises a ledge plate 50 hinged to the end panel at 51 and having end projections 52 which swing up when the ledge plate 50 is swung down, the projections 52 engaging stop elements 53 fixed to the end panel corrugations in the valleys. The ledge plates 50 and their projections 52 swing'around to lie flat against the end panels in the knockdown assembly.

The shelf supporting means described is merely suggestive of a wide variety of possible means which might be provided. It is important that the shelf length should not be so long as to prevent placement in the knockdown package between the depending projections 20, 21 of the top panel, as shown in FIG. 3, unless, of course, some other knockdown package assembly arrangement is used. 7

FIG. 13 shows a modified shelf supporting arrangement in which the shelf 17 is provided with end projections 50 which enter corrugation valleys of the end panels and rest on ledges 53 secured therein. The projections could be shortened by bending them down, in which case they could hook over a sup port plate secured across the corrugations of the end panels.

In dismantling, the shelves are removed first and, with the doors folded on top of the top panel, the shelves are inserted beneath the top panel 13, angular elements 54 being provided beneath the top panel for supporting them. The shearand floor panels are disconnected and removed. The end panels are swung up in position beneath the top panel. It is noted that the assembly is relatively light so can be tumed'over or on edge or otherwise handled in making the layup. After stacking, the parts can be secured in a pack in any convenient way, as mentioned, as by strapping, clamping, or the like.

While one embodiment, with slight variations in detail, has been described for purposes of illustration, it is to be understood that there may be various embodiments and modifierection and knockdown assembly without loss of parts, comprising in combination, a top panel, end panels hinged to the ends of the top panel with the hinge lines at different distances from the top panel to cause one end panel to lie over the other end panel when they are folded up with the top panel, folding door panels hinged to side edges of the top panel for folding above the top panel at opposite sides thereof, a bottom panel, detachable connections between the lower edges of the end panels and bottom panel for quickly connecting them to and disconnecting them from the bottom panel, said connections including captive fastener elements carried by one of the panels at each connection edge which cooperate with mating fastener elements carried by the other panel, means including captive fastener elements for securing the door panels to the end and bottom panels, a shear panel detachably secured to the top and bottom panels and to at least one end panel by captive fastener elements when the container is erected, and a shelf panel detachably secured to the end panels when the container is erected, and shear panel and shelf panel being disposed flatwise in the knockdown package assembly when the container is dismantled, said shelf panel being disposed on one side of said top panel and said bottom and shear panels being disposed on the other side of said top panel over said door panels in the knockdown package assembly.

lOlOZS 0063

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1632476 *Jun 30, 1924Jun 14, 1927Cryder Ray EStudent's portable desk
US2274048 *Apr 3, 1940Feb 24, 1942Harry DermanContainer, cabinet, and the like
US2360452 *Jan 30, 1943Oct 17, 1944Abraham StoneKnockdown utility cabinet
US3064569 *Jan 28, 1957Nov 20, 1962Manuel RosenthalFolding napalm land mine
US3303949 *Dec 23, 1964Feb 14, 1967Nickel Dennis DRefuse truck
US3414156 *Apr 30, 1965Dec 3, 1968Interlund SaCollapsible container for fluid or powder
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3784054 *Aug 27, 1971Jan 8, 1974Mautz FLoading container means
US4008936 *Jan 23, 1975Feb 22, 1977Goodyear Aerospace CorporationLD-3 Cargo container
US4046186 *Feb 12, 1976Sep 6, 1977Transequip Inc.Cargo container opening cover
US4089574 *Oct 6, 1976May 16, 1978Neville George FordPackaging of electrical or electronic components
US4289362 *Jun 12, 1979Sep 15, 1981Kramer Daniel ESegmented door for enclosure
US4646928 *Jan 10, 1985Mar 3, 1987Nisso Sangyo Co., Ltd.Folding container
US4726486 *Nov 14, 1986Feb 23, 1988Nisso Sangyo Co. Ltd.Collapsible container
US4802600 *Nov 25, 1987Feb 7, 1989Swiss AluminumFreight container for air transport
US5601201 *Jun 6, 1995Feb 11, 1997Satco Inc.Air cargo container
US5890612 *Nov 12, 1996Apr 6, 1999European Aviation Products--S.R.L.Collapsible aircraft container
US5941405 *Dec 3, 1996Aug 24, 1999Scales; Peter BruceCollapsible airline cargo container
US6299009 *Jun 13, 2000Oct 9, 2001Alusuisse Technology & Management Ltd.Collapsible freight container for air transport
US6378172Nov 28, 2000Apr 30, 2002Fabri-Craft, Inc.Airplane container door hinge
US6510589Apr 4, 2002Jan 28, 2003Fabri-Craft, Inc.Airplane container door hinge
US8256635Sep 2, 2010Sep 4, 2012Aero Containers International, LLCCollapsible cargo container assembly
US8763834 *Aug 25, 2010Jul 1, 2014Gregory SkoviraModular enclosure
US8905254 *Jun 23, 2009Dec 9, 2014Mechana CcTransport of goods
US8973769Jun 6, 2012Mar 10, 2015Telair International GmbhCargo holding device in particular for loading aircraft, and method for the production of a cargo holding device
US20110049140 *Aug 25, 2010Mar 3, 2011Gregory SkoviraModular Enclosure
US20110186568 *Jun 23, 2009Aug 4, 2011Simon John JoubertTransport of goods
WO2007035464A2 *Sep 14, 2006Mar 29, 2007Bradford CoCollapsible container for air shipment cargo and method of use
WO2008033668A2 *Aug 29, 2007Mar 20, 2008Bradford CoCollapsible container for air shipment cargo and method of use
WO2012168305A1 *Jun 6, 2012Dec 13, 2012Telair International GmbhCargo holding device in particular for loading aircraft, and method for the production of a cargo holding device
U.S. Classification312/258, 220/1.5, 312/108, 220/6, 217/15
International ClassificationB65D88/52, B65D88/14, A47B43/00, B65D6/16, B65D88/00, B65D6/18
Cooperative ClassificationB65D88/14, B65D9/14, B65D7/28, A47B43/00, B65D88/522
European ClassificationB65D88/14, B65D7/28, A47B43/00, B65D9/14, B65D88/52A