US3194365A - Baggage - Google Patents

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US3194365A
US3194365A US24059762A US3194365A US 3194365 A US3194365 A US 3194365A US 24059762 A US24059762 A US 24059762A US 3194365 A US3194365 A US 3194365A
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Prior art keywords
shell
strip
edge
baggage
portions
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Jr James M Herring
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ThyssenKrupp Budd Co
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Budd Co
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/53Joining single elements to tubular articles, hollow articles or bars
    • B29C66/534Joining single elements to open ends of tubular or hollow articles or to the ends of bars
    • AHUMAN NECESSITIES
    • A45HAND OR TRAVELLING ARTICLES
    • A45CPURSES; LUGGAGE; HAND CARRIED BAGS
    • A45C5/00Rigid or semi-rigid luggage
    • A45C5/02Materials therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C57/00Shaping of tube ends, e.g. flanging, belling or closing; Apparatus therefor, e.g. collapsible mandrels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/44Joining a heated non plastics element to a plastics element
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/12Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/124Tongue and groove joints
    • B29C66/1244Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue
    • B29C66/12441Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue being a single wall
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832Reciprocating joining or pressing tools
    • B29C66/8322Joining or pressing tools reciprocating along one axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0044Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping edges or extremities
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/74Joining plastics material to non-plastics material
    • B29C66/742Joining plastics material to non-plastics material to metals or their alloys
    • B29C66/7422Aluminium or alloys of aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2705/00Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B29K2705/02Aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/7418Suitcases

Definitions

  • one of the objects of the invention is to provide a simple, inexpensive, lightweight baggage.
  • FIG. 1 is a perspective view of a piece of baggage embodying the invention
  • FIG. 2 is an enlarged cross sectional view taken along lines 22 of FIG. 1;
  • FIGS. 3-6 are enlarged cross sectional views illustrating various steps in the method of manufacturing the baggage illustrated in FIG. 1.
  • Valise 10 includes a carrying handle 13 and a pair of latches 14 of any suitable conventional construction and operation.
  • Base 11 and cover 12 are shape similarly and, when closed, enclose a space for carrying articles in the valise.
  • Each of the case sections comprises a shallow pan-dishor cup-shaped plastic shell 15 joined at its edge to a metal reinforcing rim or strip 16.
  • This strip is of generally U-shaped cross section and includes a longitudinal, coextensive groove or slot 17 which receives the edge of shell 15 and interlocks therewith.
  • Side walls 22 are spaced transversely a greater distance than walls 19 whereby cavity 20 is wider than throat 18.
  • Each strip 16 also has a flat face 25 adapted to abut the flat face 25 of the other strip (FIG. 2) to seal with the valise when closed.
  • the angle of oblique walls 23 is such that a force tending to separate shell 15 and strip 16 (that is, tending to pull them apart) causes that portion of the enlarged section 24 entrained between the oblique walls 23 and the adjacent portions of the side walls to wedge against the oblique walls and force or wedge the walls 19 of the throat into tighter engagement with the shell.
  • This wedging action permits the use of thinner walls 22 and thereby affords a lighter weight construction than in the case if such wedging action were not present.
  • the edge of shell 15 positively locks or interlocks with strip 16 and it is not necessary to join these parts by using additional filler material, rivets, clamps, adhesives, etc.
  • valise 10 is constructed by first forming base 11 and cover 12 and then pivotally connecting them together and attaching a handle 13 and latches 14.
  • Each case section, i.e., base 11 and cover 12, is constructed in a similar fashion so that only the method of constructing one of them need be described in detail.
  • strip 16 and shell 15 are formed separately.
  • Strip 16 is of a metal, such as aluminum, that is lightweight and strong enough to reinforce the edge of the shell and has a higher softening or melting temperature than the shell.
  • Strip 16 is preferably formed by extruding it to first form a length of bar stock having the desired transverse cross section. Next, the bar stock is cut to length. Each piece thus formed is then bent or stretch formed into a rectangular, annular shape corresponding to the shape of the edge of the shell. Then the ends of the bent strip are joined to fasten them. This last step can be eliminated by placing the rectangularly bent strip in a fixture or platen during the assembly process whereby the platen holds the ends in proper alignment so that the shell can be assembled or attached.
  • Shell 15 is of a thermoplastic material having suitable properties for use as a valise.
  • the material softens or becomes plastic at a temperature below the melting or softening point of strip 16 so that it can be softened without softening FOX melting the strip.
  • the shell can be an acrylonitrile-butadiene-styrene (ABS) polymer such as Kralastic SS sold under this trade name by the Naugatuck Chemical Division of the United States Rubber Company.
  • ABS acrylonitrile-butadiene-styrene
  • Shell 15 is preferably formed from sheet material by vacuum drawing, blowing or stretch forming techniques. In each of these methods, the sheet is heated above its softening point and force against the mold of the desired shape, and then cooled to retain the shape.
  • shell 15 and strip 16 are assembled so that the edge of the shell extends through throat 17 and abuts end wall 21.
  • the edge is softened by heating it to its softening temperature.
  • heat is applied to strip 16 whereby the heat is conducted through the strip and into the edge.
  • One way to supply the heat would be to embed an electrical resistance heater 28 in fixture 27 whereby operation of the heater heats strip 16.
  • the softened portions are upset to fill cavity 20 as by pushing the shell into the slot, in the direction of the arrow in FIG. 5, so that the hard (unsoftened) portions of the shell push downwardly through the throat and expand the softened portions transversely until the cavity is filled.
  • the edge of shell 15 Prior to upsetting, the edge of shell 15 is of substantially uniform thickness.
  • the distance between side walls 19 is made slightly greater than the thickness of shell 15 to provide suitable clearance so that when the shell is initially inserted into the strip, the edge does not contact walls 19.
  • the upper edges of walls 19 can be beveled as illustrated.
  • Strip 16 is heated at its bottom to produce a temperature gradient along the strip whereby the bottom wall 21 is at a higher temperature than side walls 19.
  • the edge heats from the pended claim.
  • the softened portions are hardened and solidi-r fiedby cooling them belowthe softening point; This can' be accomplished rapidly by spraying the strip 16 'withia liquid coolant'w, such as water, as illustrated in FIG. 6, a toquench the softened portions and securely join strip 16 and shell 15.1
  • This application or coolant might be desir-v ablein high speed productionwhere it might also be delsirable to continuously heatthe platensbysheater28, as'op posed to intermittent heating thereof.
  • the now completed case section is removed and then assembled with another case section; in the-'rnanner: previously indicated, toiform' a valise, v s.
  • said U-shaped strip including a closed bottom wall'and 'a' pair of spaced apart continuous upstanding side walls to f define a cavity therebetween', each of said side walls'shaving l at its upperwend 'a first portion extending jnwardly'toward i 'the opposite; side wall offsaid pair and parallel to said;

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)

Description

July 13, 1965 J. M. HERRING, JR
BAGGAGE Filed Nov. 28, 1962 INVENTOR.
- JAMES M. HERRING, JR. BY
ATTORNEY United States Patent 3,194,365 BAGGAGE James M. Herring, Jr., Rosemont, Pa., assignor to The Budd Company, Philadelphia, Pa., a corporation of Pennsylvania Filed Nov. 28, 1962, Ser. No. 240,597
1 Claim. '(Cl. 190- 19) This invention relates to baggage.
Presently, there are commercially available a large number of different types of carrying cases or bags, valises, suitcases, etc., which are expensive bothto manufacture and to buy. However, there appears to be a potential market for inexpensive baggage designed to be sold on an optional basis in conjunction with the sale of some other article or even provided free-of-charge. Examples are a set of custom suitcases designed to fill a car trunk as completely as possible and a carrying case specially fitted to carry the article which is the primary object of the sale, such asa typewriter, camera, microscope, etc.
Accordingly, one of the objects of the invention is to provide a simple, inexpensive, lightweight baggage.
Other objects and advantages will be apparent from the following description taken in connection with the accompanying drawing wherein:
FIG. 1 is a perspective view of a piece of baggage embodying the invention;
FIG. 2 is an enlarged cross sectional view taken along lines 22 of FIG. 1; and
FIGS. 3-6 are enlarged cross sectional views illustrating various steps in the method of manufacturing the baggage illustrated in FIG. 1.
Referring now to the drawing, the invention is illustrated as embodied in a suitcase or valise comprising a pair of case sections designated a base 11 and a cover 12 that are hinged or pivotally connected in the usual fashion for movement between open and closed positions. Valise 10 includes a carrying handle 13 and a pair of latches 14 of any suitable conventional construction and operation. Base 11 and cover 12 are shape similarly and, when closed, enclose a space for carrying articles in the valise.
Each of the case sections comprises a shallow pan-dishor cup-shaped plastic shell 15 joined at its edge to a metal reinforcing rim or strip 16. This strip is of generally U-shaped cross section and includes a longitudinal, coextensive groove or slot 17 which receives the edge of shell 15 and interlocks therewith.
Slot 17 comprises: a throat 18 defined by a pair of parallel side walls 19; and a central chamber or cavity 20 defined by a bottom wall 21, a pair of parallel side walls I 22=and a pair of oblique walls 23 that extend between the outer ends of side walls 22 and the inner ends of side walls 19. Side walls 22 are spaced transversely a greater distance than walls 19 whereby cavity 20 is wider than throat 18.
The edge of shell 15 extends through throat 15 and substantially fills cavity 29 whereby the extreme edge of the shell forms an enlarged portion 24 which is wider than throat 18 and cannot pass therethrough. Each strip 16 also has a flat face 25 adapted to abut the flat face 25 of the other strip (FIG. 2) to seal with the valise when closed.
The angle of oblique walls 23 is such that a force tending to separate shell 15 and strip 16 (that is, tending to pull them apart) causes that portion of the enlarged section 24 entrained between the oblique walls 23 and the adjacent portions of the side walls to wedge against the oblique walls and force or wedge the walls 19 of the throat into tighter engagement with the shell. This wedging action permits the use of thinner walls 22 and thereby affords a lighter weight construction than in the case if such wedging action were not present. Thus, the edge of shell 15 positively locks or interlocks with strip 16 and it is not necessary to join these parts by using additional filler material, rivets, clamps, adhesives, etc.
In accordance with the invention, valise 10 is constructed by first forming base 11 and cover 12 and then pivotally connecting them together and attaching a handle 13 and latches 14. Each case section, i.e., base 11 and cover 12, is constructed in a similar fashion so that only the method of constructing one of them need be described in detail.
As the first step of the method, strip 16 and shell 15 are formed separately. Strip 16 is of a metal, such as aluminum, that is lightweight and strong enough to reinforce the edge of the shell and has a higher softening or melting temperature than the shell. Strip 16 is preferably formed by extruding it to first form a length of bar stock having the desired transverse cross section. Next, the bar stock is cut to length. Each piece thus formed is then bent or stretch formed into a rectangular, annular shape corresponding to the shape of the edge of the shell. Then the ends of the bent strip are joined to fasten them. This last step can be eliminated by placing the rectangularly bent strip in a fixture or platen during the assembly process whereby the platen holds the ends in proper alignment so that the shell can be assembled or attached.
Shell 15 is of a thermoplastic material having suitable properties for use as a valise. The material softens or becomes plastic at a temperature below the melting or softening point of strip 16 so that it can be softened without softening FOX melting the strip. As an example, the shell can be an acrylonitrile-butadiene-styrene (ABS) polymer such as Kralastic SS sold under this trade name by the Naugatuck Chemical Division of the United States Rubber Company.
Shell 15 is preferably formed from sheet material by vacuum drawing, blowing or stretch forming techniques. In each of these methods, the sheet is heated above its softening point and force against the mold of the desired shape, and then cooled to retain the shape.
Next, shell 15 and strip 16 are assembled so that the edge of the shell extends through throat 17 and abuts end wall 21. This can be done by first placing strip 16 in a fixture or platen 2'7 and then aligning and inserting the edge of the shell into the slot causing the edge to abut end wall 21 as shown in FIG. 4.
After the shell and strip have been thus assembled, the edge is softened by heating it to its softening temperature. To do this, heat is applied to strip 16 whereby the heat is conducted through the strip and into the edge. One way to supply the heat would be to embed an electrical resistance heater 28 in fixture 27 whereby operation of the heater heats strip 16.
Next, the softened portions are upset to fill cavity 20 as by pushing the shell into the slot, in the direction of the arrow in FIG. 5, so that the hard (unsoftened) portions of the shell push downwardly through the throat and expand the softened portions transversely until the cavity is filled.
Prior to upsetting, the edge of shell 15 is of substantially uniform thickness. The distance between side walls 19 is made slightly greater than the thickness of shell 15 to provide suitable clearance so that when the shell is initially inserted into the strip, the edge does not contact walls 19.
To facilitate insertion of the edge and upsetting the softened portions, the upper edges of walls 19 can be beveled as illustrated.
Strip 16 is heated at its bottom to produce a temperature gradient along the strip whereby the bottom wall 21 is at a higher temperature than side walls 19. When the shell edge is inserted into the slot so that the bottom of the edge abuts the bottom wall 21, the edge heats from the pended claim.
2 bottom upwhereby lower portions soften portions.v The thermal conductivity of the plastic shelleis sufficiently 10w whereby, although the immediate, lower before upper portions of the edge are soft, the upper portions, becauseof the temperature gradient, are hard and lean-be pushed .7 downwardly through the throat to expand the softened I portions.- This upsetting continues after cavity 20 issubl stantially filled until the throat is filled and. the shell begins to bulge or exapnd slightly above thestrip whereupon'the upsetting force is removed or discontinued. During the upsetting,a small air cavity would probably be ff0rrned,-
in theabsence of any tap or bleed hole, at'the-intersections ofobliqueflwalls 23 and sidewalls 22'above enlarged portion 24. va v Finally, the softened portionsare hardened and solidi-r fiedby cooling them belowthe softening point; This can' be accomplished rapidly by spraying the strip 16 'withia liquid coolant'w, such as water, as illustrated in FIG. 6, a toquench the softened portions and securely join strip 16 and shell 15.1 This application or coolant might be desir-v ablein high speed productionwhere it might also be delsirable to continuously heatthe platensbysheater28, as'op posed to intermittent heating thereof. Afterfthesoftened portions havecooled sufficiently, the now completed case section" is removed and then assembled with another case section; in the-'rnanner: previously indicated, toiform' a valise, v s.
It. is to be understoodfthatjvarious changesmcan be made in thedetailsjand arrangementsof parts without departing from the scope of the invention as What is claimed is:
In a valis'e, .the conibinationsofz 'a pair of case-set ions defined in the ap-? at leastone of-said case sections comprising a sheet meinber andareinforcing U-shaped' strip bonded, to vits V edge,:
said U-shaped strip including a closed bottom wall'and 'a' pair of spaced apart continuous upstanding side walls to f define a cavity therebetween', each of said side walls'shaving l at its upperwend 'a first portion extending jnwardly'toward i 'the opposite; side wall offsaid pair and parallel to said;
bottom wall," and a secondportion extending downwardlyl toward v said bottom Wall, said-secondportions of thexside wallsibeingin opposedrelatiolnship oneto; another to'jde j fine .a v throatto receive the i edgefofa e men membe therein,--each'said secondjpor'tion having a planar surfac l extending from,itsifree end jarid'inclin'ed toward: theF'iO P' V 7, portion ofthe side Wall of 1Whichthesam'e torms a part; ,said edge-of said sheet member having anenlarged portion i filling saidfcavity and eirtendingbetween said planar sur-" 1 a es and their respective said sidewalls References Citedhy'the-Exarniner;
' FRANIQIN E A RETTQ; i
US24059762 1962-11-28 1962-11-28 Baggage Expired - Lifetime US3194365A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3432012A (en) * 1966-10-11 1969-03-11 Samsonite Corp Luggage cases
US5168968A (en) * 1991-01-08 1992-12-08 Samsonite Corporation Valence for luggage case

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2672224A (en) * 1948-12-08 1954-03-16 Horwitz Leo Luggage and method of making same
US2743029A (en) * 1950-05-05 1956-04-24 Skydyne Inc Shipping case or the like
US2758682A (en) * 1954-09-16 1956-08-14 Shwayder Bros Inc Luggage moldings
US2803368A (en) * 1954-12-06 1957-08-20 Maurice P Koch Thermal insulated carrying cases and sealing means for same
US2828844A (en) * 1955-08-26 1958-04-01 Jr William H Arlitt Reinforcing means for an article of luggage
US2859483A (en) * 1957-01-11 1958-11-11 Roy F High Coalescence of pre-molded parts
US2946096A (en) * 1954-08-19 1960-07-26 William F Stahl Method of making a coil form
US2974383A (en) * 1955-09-16 1961-03-14 Bright Thomas John Robert Clips or tags and draught-excluding strips, beadings, mouldings or the like for use therewith
US3088623A (en) * 1961-07-20 1963-05-07 Thermo Plastic Products Compan Fastening and sealing means for containers
US3093526A (en) * 1961-02-07 1963-06-11 Goodyear Aircraft Corp Method of plastic edge attachment

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2672224A (en) * 1948-12-08 1954-03-16 Horwitz Leo Luggage and method of making same
US2743029A (en) * 1950-05-05 1956-04-24 Skydyne Inc Shipping case or the like
US2946096A (en) * 1954-08-19 1960-07-26 William F Stahl Method of making a coil form
US2758682A (en) * 1954-09-16 1956-08-14 Shwayder Bros Inc Luggage moldings
US2803368A (en) * 1954-12-06 1957-08-20 Maurice P Koch Thermal insulated carrying cases and sealing means for same
US2828844A (en) * 1955-08-26 1958-04-01 Jr William H Arlitt Reinforcing means for an article of luggage
US2974383A (en) * 1955-09-16 1961-03-14 Bright Thomas John Robert Clips or tags and draught-excluding strips, beadings, mouldings or the like for use therewith
US2859483A (en) * 1957-01-11 1958-11-11 Roy F High Coalescence of pre-molded parts
US3093526A (en) * 1961-02-07 1963-06-11 Goodyear Aircraft Corp Method of plastic edge attachment
US3088623A (en) * 1961-07-20 1963-05-07 Thermo Plastic Products Compan Fastening and sealing means for containers

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3432012A (en) * 1966-10-11 1969-03-11 Samsonite Corp Luggage cases
US5168968A (en) * 1991-01-08 1992-12-08 Samsonite Corporation Valence for luggage case

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