US2505348A - Flexible container - Google Patents

Flexible container Download PDF

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Publication number
US2505348A
US2505348A US610289A US61028945A US2505348A US 2505348 A US2505348 A US 2505348A US 610289 A US610289 A US 610289A US 61028945 A US61028945 A US 61028945A US 2505348 A US2505348 A US 2505348A
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US
United States
Prior art keywords
container
sides
joints
fabric
cell
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
US610289A
Inventor
Marion M Cunningham
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Uniroyal Inc
Original Assignee
United States Rubber Co
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Filing date
Publication date
Application filed by United States Rubber Co filed Critical United States Rubber Co
Priority to US610289A priority Critical patent/US2505348A/en
Application granted granted Critical
Publication of US2505348A publication Critical patent/US2505348A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS 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
    • B65D11/00Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of plastics material
    • B65D11/10Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of plastics material of polygonal cross-section and all parts being permanently connected to each other
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/06Constructional adaptations thereof
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S220/00Receptacles
    • Y10S220/30Biodegradable

Definitions

  • My inventionk relates to liquid containers and more particularly to fuel cells of the coated flexible fabric type, one form of which is extensively used in carrying fuel in airplanes.
  • FIG. 1 is a broken perspective View of the container mounted on a forming frame and turned bottom side upwards;
  • Fig. 2 is a cross-sectional view of the container after removal of a form taken substantially along the section line 2--2 of Fig. l and Fig. 3 is a cross-sectional view of a portion of an airplane wing, with a container mounted therein, the container being shown on the crosssection line 3-3 of Fig. 1, and Without the form.
  • a liquid container preferably of the fuel cell type is provided with side Walls I, 2, 3 and il, a top wall 5 and a bottom wall 6, some of which are united by reinforced seams i which are underlaid by flexible reinforcing and stiffening strips 3.
  • the seams and reinforcing strips are described and claimed in said application Serial No. 573,128.
  • the side walls and top and bottom walls are given an outward or convex curvature such that when the container with the seams 'l and the reinforcing strips 8 is inserted in a metal housing 9 formed in part by the structural elements l0, l I, and I2 of a metallic 3 Claims. (Cl. 220-63) structure, which is illustrated in Fig.
  • a form I4 of a soluble cardboard construction is provided in which the side, top and bottom walls are given an outward or convex curvature, or dome shape, with reference to the corners of the y container as is particularly 'shown in Fig. 2.
  • reinforcing strips 8 are placed along the desired edges of the form 'M Provisionis made in the form for a manhole mounting I 5 and pipe ttings, one of which is shown at i6.
  • the coated fabric forming the side, top and bottom walls of the container is then stretched over and around the frame ill so that the fabric conforms to the shape of the frame.
  • the seams 'I are completed to unite them to the strips 8.
  • Reinforcing stitching l1 may be employed.
  • the edges of the fabric are trimmed to the resulting shape. As is shown in Fig. 2, the seams 1 lie within the projection of the outwardly curved portions of the side, top and bottom walls of the containers.
  • the container is cured on the frame i4, which is thereafter removed by a dissolving and washing operation which is well known in the art.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Packages (AREA)

Description

Patented Apr. 25M, 1950 FLEXIBLE CONTAINER Marion M.A Cunningham, South Bend, Ind., as-
signor to United States Rubber Company, New York, N. Y., a corporation of New Jersey i Application August 11, 1945', Serial N0. 610,289
My inventionk relates to liquid containers and more particularly to fuel cells of the coated flexible fabric type, one form of which is extensively used in carrying fuel in airplanes.
In the Gray and Zivi Patent No. 2,102,590,
issued December 2l, 1937, there is shown and described a liquid container for aircraft in which the general dimensions of the confining structural elements are such that the Weight and impact forces of the liquid content ultimately react with the structural elements of the aircraft, rather than being resisted solely by the material of the container.
In 'somercontainers it is desirable toluse reinforcing strips of the character shown in a prior application, in which I am a joint applicant, Serial No. 573,128, led January 16, 1945, wherein the reinforcing strips are shaped to closely conform to the corners or edges defined by the plane structural members. Also, in general, the supporting aircraft structural members have greater flexibility in the areas intermediate their edges than at the edges. Accordingly, I have found that the advantages of the Gray and Zivi construction can be obtained by making the edges of the panels of the container substantially conform to the shape defined by the structural elements of the plane and'by doming the areas of the panels intermediate the edges thereof.
The accompanying drawings illustrate a present preferred form of the invention, in Which- Fig. 1 is a broken perspective View of the container mounted on a forming frame and turned bottom side upwards;
Fig. 2 is a cross-sectional view of the container after removal of a form taken substantially along the section line 2--2 of Fig. l and Fig. 3 is a cross-sectional view of a portion of an airplane wing, with a container mounted therein, the container being shown on the crosssection line 3-3 of Fig. 1, and Without the form.
A liquid container preferably of the fuel cell type is provided with side Walls I, 2, 3 and il, a top wall 5 and a bottom wall 6, some of which are united by reinforced seams i which are underlaid by flexible reinforcing and stiffening strips 3. The seams and reinforcing strips are described and claimed in said application Serial No. 573,128. In the present application the side walls and top and bottom walls are given an outward or convex curvature such that when the container with the seams 'l and the reinforcing strips 8 is inserted in a metal housing 9 formed in part by the structural elements l0, l I, and I2 of a metallic 3 Claims. (Cl. 220-63) structure, which is illustrated in Fig. 3 as a por- 55 tion of an airplane wing, the corners of the container fit snugly into the corners of the housing while the side walls and top and bottom walls are free toengage and be supported by the housing S, thereby obtaining the advantages of the structures described in the Gray and Zivi Patent No. 2,102,590.
In the manufacture of my improved container a form I4 of a soluble cardboard construction is provided in which the side, top and bottom walls are given an outward or convex curvature, or dome shape, with reference to the corners of the y container as is particularly 'shown in Fig. 2. The
reinforcing strips 8 are placed along the desired edges of the form 'M Provisionis made in the form for a manhole mounting I 5 and pipe ttings, one of which is shown at i6. The coated fabric forming the side, top and bottom walls of the container is then stretched over and around the frame ill so that the fabric conforms to the shape of the frame. The seams 'I are completed to unite them to the strips 8. Reinforcing stitching l1 may be employed. The edges of the fabric are trimmed to the resulting shape. As is shown in Fig. 2, the seams 1 lie within the proiection of the outwardly curved portions of the side, top and bottom walls of the containers. The container is cured on the frame i4, which is thereafter removed by a dissolving and washing operation which is well known in the art.
As is shown in Fig. 3, when the container is mounted in the supporting structure, the seams 1 snugly t into the corners or joints of the housing 9 and the intermediate fabric of the side, top and bottom walls or panels, which have the resultant domed shapes` are confined bv the structural elements so that the weight of' their contents is transmitted to the structural elements without imposing extensive strains on the fabric. In such construction the joints between the sides of the supporting construction resist distortion to a greater degree than the areas of the sides away from the joints, and such areas are sometimes expanded or domed outwardly by the kinetic force of the fluid contents. Since the fabric panels of the exible container have been pre-domed, they are adapted to follow the outward movement of the walls of the supporting structure without staining the fabric. Since the joints of the supporting construction are relatively free from distortion, the joints of the flexible container closely fitting therein are continuously supported without making them oversize in respect to the supporting joints, which oversize dimension would tend to cause them to leak as a result of the wrinkling.
Furthermore, with the above construction the advantage of the reinforced corners or seams is obtained Without sacrificing any of the space vavailable in the supporting housing and Without excessively stressing the fabric.
While havshoWn-land described at present preferred embodiment -of my"'in"vention, itis to be understood that the invention may be other- Wise embodied within the spirit of the invention and the scope of the appended claims.
Having thus described my invention, vv'lfiat claim and desire to protectfbylLettes-Patetfis:
1. The combination of "ae'ell'i aving 'iiibl sides and a confining structure *having ""sid'es adapted to support the sides' of'lsaidf cell-.sides, the joints between said cell sides being preformed to t the corresponding joints-*between said supporting structure sides, and the sides of 52.-'51-he-1cornbinaticnz of a `cell''for1f'cori-tamine liquids and a supporting structure, saidis'up'porftcenters, preformed joints uniting said flexible panels, and the outside length of said joints in said cell being substantially equal to the inside length of the corresponding joints in said sup- 5 porting structure.
3. The combination of a cell having ilexible sides and a confining structure having sides :adapted to support the``r s'izles` of said cell sides, A"the:junc'turerbetween the' sides of `said ncell being 10 preformed and of a length substantially equal i 'rft'o the length of the corresponding juncture of @thegs-idesof said supporting structure, and each sidev oi said cell having a substantially greater 'fsuiifacefarea than the surface area of the correfl spcr'idin'gfside'4 lof Vthe supporting structure, which :Number Name Date `:1,1395g976 meDornier 1..-.-- vJan. 31, 1933 @2341,450 `irdains .l- ..v May 19, 1936 $102,590 Gray etal. 1 Dec. 21, 1937 1.230: 12,331-09'7 Watter v c Oct. 5, 1943 FOREIGN -`#PATENTS Number' Country Date i 117,765 Australia May I28,- 1942
US610289A 1945-08-11 1945-08-11 Flexible container Expired - Lifetime US2505348A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638138A (en) * 1949-01-07 1953-05-12 Goodyear Aircraft Corp Fuel cell supporting enclosure
US2720998A (en) * 1951-12-06 1955-10-18 Clifford S Potter Collapsible container
DE1161210B (en) * 1959-11-19 1964-01-09 Soudure Autogene Francaise Large capacity container with expansion brackets
DE1187988B (en) * 1961-02-07 1965-02-25 Knut Valter Ringblom Container
US4345698A (en) * 1980-03-25 1982-08-24 The United States Of America As Represented By The Secretary Of The Air Force Aircraft self-sealing fuel tank
US4368086A (en) * 1980-03-25 1983-01-11 The United States Of America As Represented By The Secretary Of The Air Force Method of fabricating an aircraft self-sealing fuel tank

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1895976A (en) * 1930-07-26 1933-01-31 Dornier Metallbauten Gmbh Storage of liquids in aircraft
US2041450A (en) * 1932-07-30 1936-05-19 Adams Herbert Luther Safety fuel tank
US2102590A (en) * 1936-12-02 1937-12-21 Glenn L Martin Co Aircraft construction
US2331097A (en) * 1941-04-11 1943-10-05 Budd Edward G Mfg Co Liquid receptacle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1895976A (en) * 1930-07-26 1933-01-31 Dornier Metallbauten Gmbh Storage of liquids in aircraft
US2041450A (en) * 1932-07-30 1936-05-19 Adams Herbert Luther Safety fuel tank
US2102590A (en) * 1936-12-02 1937-12-21 Glenn L Martin Co Aircraft construction
US2331097A (en) * 1941-04-11 1943-10-05 Budd Edward G Mfg Co Liquid receptacle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638138A (en) * 1949-01-07 1953-05-12 Goodyear Aircraft Corp Fuel cell supporting enclosure
US2720998A (en) * 1951-12-06 1955-10-18 Clifford S Potter Collapsible container
DE1161210B (en) * 1959-11-19 1964-01-09 Soudure Autogene Francaise Large capacity container with expansion brackets
DE1187988B (en) * 1961-02-07 1965-02-25 Knut Valter Ringblom Container
US4345698A (en) * 1980-03-25 1982-08-24 The United States Of America As Represented By The Secretary Of The Air Force Aircraft self-sealing fuel tank
US4368086A (en) * 1980-03-25 1983-01-11 The United States Of America As Represented By The Secretary Of The Air Force Method of fabricating an aircraft self-sealing fuel tank

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