US3213913A - Flexible containers - Google Patents
Flexible containers Download PDFInfo
- Publication number
- US3213913A US3213913A US198954A US19895462A US3213913A US 3213913 A US3213913 A US 3213913A US 198954 A US198954 A US 198954A US 19895462 A US19895462 A US 19895462A US 3213913 A US3213913 A US 3213913A
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- Prior art keywords
- container
- flexible
- resin
- modulated
- pressure
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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
- B65D88/00—Large containers
- B65D88/54—Large containers characterised by means facilitating filling or emptying
- B65D88/58—Large containers characterised by means facilitating filling or emptying by displacement of walls
- B65D88/60—Large containers characterised by means facilitating filling or emptying by displacement of walls of internal walls
- B65D88/62—Large containers characterised by means facilitating filling or emptying by displacement of walls of internal walls the walls being deformable
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/917—Corrosion resistant container
Definitions
- the upper hemispherical sections 3 and 3' are provided with polymer modified latitudinal reinforced bands 6 and 6 that direct the pattern of collapse under interstitial pressure, that is pressure applied pneumatically or hydrodynamically between outer portion of the flexible inner container 1 and the inner portion of a rigid outer container or shell 5 as shown in FIG. 3.
- the internal layers 212 are predominantly made of the resin, while the external layers 1424 are made of resin and alumium flake to impart the desired higher modulus.
- the flexible portions all layers are of resin.
- Each layer is sintered at 340400 C. for 10-30 minutes thereby fusing it to the preceding layer.
- Each layer is cooled to room temperature before applying the next layer. This sintering process is described in my Patent No. 2,852,811 granted September 23, 1958.
- the regions 6 FIG. 5 will oppose the pressure while regions 7 will, with its lower effective modulus, undergo flexure.
- the upper hemispherical section comprised a series of 9 latitudinal bands approximately l-inch in width alternating between the nickel-resin interlayer and plain resin layer.
- a flexible, modulated container comprising a hemispherical structure according to claim 1 made of polyhaloethylene resins.
Description
Oct. 26, 1965 J. v. PETRIELLO 3,213,913
FLEXIBLE CONTAINERS Filed May 31, 1962 3 Sheets-Sheet l FIG I FIGZ INVENTOR.
JOHN V. PETRIELLO BYslmzwm Oct. 26, 1965 Filed May 31, 1962 J. V. PETRIELLO FLEXIBLE CONTAINERS 5 Sheets-Sheet 2 TIME MIN.
FIG 4c LBS. SQ.IN.
5 l0 TIME MIN.
FIG 4A INVENTOR.
JOHN V. PETRIELLO Oct. 26, 1965 J. v. PETRIELLO FLEXIBLE CONTAINERS 3 Sheets-Sheet 3 Filed May 31, 1962 INVENTOR.
JQHN V- PETRIELLO BY 7 yaw/n14 United States Patent 3,213,913 FLEXIBLE CONTAINERS John V. Petriello, North Babylon, N.Y., assignor to Dilectrix Corporation, Farmingdale, NY. Filed May 31, 1962, Ser. No. 198,954 4 Claims. (Cl. 150.5)
This invention relates to novel and simple flexible containers for handling reactive liquids.
It is a primary object of this invention to provide a flexible chemically-inert container designed for storing, transferring, and metering reactive propellants and fuels used in positive propulsion systems. A further object of this invention is to provide a container constructed in such a manner that the transfer, dispensing and otherwise releasing of the reactive propulsion fuel is accomplished with improved reliability. A still further object is to provide a flexible, pressure-dispensing container having unique construction characteristics that will assure steady, stable emergence or dispensing of the contents on demand.
A fuel container of the type with which this invention is concerned is generally termed a bladder in the field of rocket or missile propulsion. The bladder is used to positively expel a stored liquid or propellant. The flexible container or bladder is usually designed to fit the inside of a rigid tank with provision to mount and seal the flexible container or bladder within the tank so that a fuel or propellant may be contained either within a fully expanded bladder or outside of a deflated bladder. Positive expulsion is then achieved by introducing, under pressure, an expellant gas on that side of the bladder opposite the fuel or propellant thereby causing a deflection of the bladder and forcing the fuel or propellant out of the system through a properly arranged discharge line.
Since the bladder is fully collapsing it is susceptible to random wrinkling and folding over most of the surface. Such wrinkling and folding usually results in sharp creases, weak areas, pinholes and eventual failing of the bladder in the expelling operation.
The flexible container or bladder of the type with which this invention is concerned has the unique feature of dispensing various gases, liquids, fuels, propellants under an expellant gas pressure with a pre-arranged, pre-devised pattern and array of fold lines, channels and troughs which precludes the random wrinkling patterns and significantly prolongs the usefulness of the container.
A singular feature of this invention is the rather surprising observation that, the flexible liner as it is made to collapse according to these pre-arranged fold lines, at-
tains a fixed or stabilized volume that does not collapse or otherwise distort to cause irregular dispensing rates, as will be described hereinafter. Another feature is the observation that the flexible plastic container having prearranged fold lines retains its collapsing pattern even on intense and random positioning including erratic cycling and attitudes.
This invention is particularly advantageous in storing, handling, metering and otherwise dispensing a wide variety of gases, fluids and solid slurries that are highly corrosive and cannot be handled in conventional rigid containers. The flexible container described in this invention is constructed of a variety of flexible polymeric or plastic materials selected on the basis of ability to withstand chemical attack or dissolution. These plastic materials include high molecular weight resins made from polyethylene, polypropylene, natural and synthetic rubber, and other unique polymers such as polytetrafluoroethylene polychlorotrifluoroethylene, polyvinyl fluoride, polyvinylidene fluoride, and copolymers of tetrafluoroethylene and hexafluoropropylene, vinylidene fluoride and hexafluoro- "Ice propylene, and such modifications as induced by known methods of cross-linking and grafting with other polymeric components. Any other plastic materials are included which are characterized as having two important attributes; flexibility and chemical inertness to the contained fluid.
These flexible containers are useful and valuable in storing compartmented fluids, for instance, as tank liners, darn storage, positive metering or propulsion systems, and the like, and are provided with simple pressuring means that collapses the flexible container away from an outer casing which is made of rigid, non-flexing material. The containers are also useful in storing and metering on command liquid propellant fuels in missile and spacecrafts. Finally they are useful in metering reactive chemicals in many industrial processes.
It is therefore an object of this invention to provide an improved and novel flexible chemical container which through controlled and precise collapsing is used to carry out efficient mixing, diverse chemical reactions, and positive metering of fluids. Other objects and advantages of this invention are made apparent in the following description by reference to the accompanying drawings.
FIG. 1 is a side view of an embodiment of the invention.
FIG. 2 is a side view of another embodiment of the invention.
FIG. 3 is a sectional assembly view of the embodiment of FIG. 1.
FIGS. 4 and 4B are sectional diagrammatic views illustrating the operation of the invention.
FIGS. 4A and 4C are graphs representing pressure relations for the embodiments of FIGS. 4 and 4B.
FIG. 5 is a sectional view of the embodiment of FIG. 1.
FIG. 6 is a diagrammatic view of the multi-layer construction.
FIG. 1 is a perspective view of a typical modular design of general type of flexible inner containers 1 made principally in the form of a sphere provided with an emergent outlet 2.
It generally comprises a lower portion 20 which is of rigid construction and an upper portion having alternate reinforced strips 6 and non-reinforced strips 7. The container is formed by spraying onto a form many layers of resin material as will be described. The reinforced layers are sprayed on with reinforced material incorporated with suitable masking as will be described hereafter. The form is later dissolved out.
Referring to FIG. 3 the inner container 1 is mounted inside a rigid outer container 5 which has a valve 5' for introducing a pressure between the inner and outer containers for the purpose of collapsing the inner container and expelling its contents, with a predetermined flow.
FIG. 2 is a similar perspective view of an inner container 1 made in the form of cylinder with hemispherical geometry at each end of the cylinder.
Referring specifically to FIGS. 1 and 2, the upper hemispherical sections 3 and 3' are provided with polymer modified latitudinal reinforced bands 6 and 6 that direct the pattern of collapse under interstitial pressure, that is pressure applied pneumatically or hydrodynamically between outer portion of the flexible inner container 1 and the inner portion of a rigid outer container or shell 5 as shown in FIG. 3. The latitudinal bands 6 and interposed alternately with unmodified latitudinal bands 7 which comprise the basic polymeric component of the flexible containers such as shown in FIGS. 1 and 2.
In this invention, the alternating latitudinal bands are constructed with distinct differences in flexural stiffness and modulus. It has been discovered that with a difference of as low as 25 percent in flexural or tensile modulus as measured by appropriate procedures, a highly efcal arrangement with that of an unmodified flexible coutainer 8 FIG. 43 made of identical dimensions. In this operation, a pressure P of 15 lb./sq. in. per gauge is valved rapidly through valve 9 into the interstitial region between the flexible containers, filled with water, and the transparent Lucite shell 5. The interior containe collapses and expels its contents through pressure gage 11 to tank 13. p
' The unmodified flexible container 8 FIG. 4B assumes a highly random, squashed form whereas the modular banded container 1 FIG. 4 assumes a perfectly symmetrical inversion. The term modular as used in this sense is defined as the existence of regular pre-arranged different moduli or other rigidity constants.
Referring to FIGS. 4A and 4C a remarkable feature is that at the emergent side, the output pressure P profile with respect to time measured on gauge 11 is extremely erratic or irregular as shown in graph FIG. 4C for the non-modular normal type of flexible container, whereas that of the container latitudinally modified FIG. 4B as detailed herein is extremely regular and precise. The irregularity is indicated at 15a FIG. 4C as the range of variability of about 9 to 17 lbs/sq. in. gauge for with the regular type of container compared to smooth flat pressure of less than 1 lb./sq. in. gauge pressure for the modulated container. This will also be evident in the marked difference in flow rate during the expulsion of liquid contents to be described in ensuing examples.
Inspection of the containers following a series of twelve such pressure operations revealed marked creases and cracks in the non-modulated container during the expulsion of ice-cold water (0 C.) compared to complete absence of any such defects in the hemispherically modulated container. More detailed features are described as follows:
Example I A 24-inch diameter spherical flexible container FIG. 5 suitable for storage and pressure-expulsion of concentrated fuming nitric acid is constructed of sintered 0.012 inch polytetrafluoroethylene, applied over a replicating aluminum form, which is later dissolved out, corresponding to FIG. 1 by a series of spray-coatings using a commercial aqueous dispersion of the polymer identified as Teflon te'trafluoroethylene fluorocarbon resin, Grade 30, sold commercially by E. I. du Pont de Nemours and Co.,' Inc., Wilmington, Delaware. The spray coatings are alternately interspersed With admixture of fine aluminum flake F averaging 2-10 microns in diameter at a thickness of 0.5 microns, and a co-dispersion volume loading, ingredient bases, of 25 volume percent of aluminum flake to 75 volume percent of dry, sintered resin, indicated by the broken lines in FIG. 5.
The layers were masked to provide two distinct hemispherical characteristics:
(a) Lower, rigid emergent hemispherical section 4 with a relatively high modulus of 145,000 lb./sq. in., as measured by ASTM procedure D1530-58T, attained by admixture of the aluminum flake, and
(b) Upper, modular-rigid pressure folding hemispherical section 3 comprising alternate latitudinal bands approximately 1 inchiV in width. The most flexible, non-filledv bands 7 comprise basic sintered resin made to a modulus of 70,000 lb./sq. in. The rigid latitudinal bands 6 are reinforced and have a modulus of 145,000 lb./sq. inv v For the lower rigid hemispherical portion 4 and latitudinal stiffening bands 6, a cross sectional buildup 16 of the total 0.012-inch was made according to the description shown in FIG. 6 comprising 24 layers in the following sequence.
Layer: Composition 24 (external) Resin. 22 Resin-l-aluminum flake. 20 Resin. 18 Resin+aluminum flake. 16 Resin. 14 Resin+aluminum flake. 12 Resin.
10 Resin.
8 Resin. 6 Resin. 4 Resin. 2 (internal) Resin.
wherein the internal layers 212 are predominantly made of the resin, while the external layers 1424 are made of resin and alumium flake to impart the desired higher modulus. For the flexible portions all layers are of resin. Each layer is sintered at 340400 C. for 10-30 minutes thereby fusing it to the preceding layer. Each layer is cooled to room temperature before applying the next layer. This sintering process is described in my Patent No. 2,852,811 granted September 23, 1958. Thus as the interstitial pressure P is imposed, the regions 6 FIG. 5 will oppose the pressure while regions 7 will, with its lower effective modulus, undergo flexure.
Under a liquid propulsion operation comprising concentrated nitric acid made to emerge through a nominal -inch stainless steel nozzle under a pressure difference of 15 lb./ sq. in. gauge, the following volumeric sequence was measured as compared to an identical design of a container made without the latitudinal, high modular bands.
Expulsion flow [Volumetric expulsion pressure: 15 lb./sq. in. gauge] Modulated Container Regular container (control) (cubic centimeters) (cubic centimeters) Time (min) Accumulated Incremental Accumulated Incremental The unique feature is the regular dispensing obtained from the modulated container, especially after the first 0.5 minute, in increments of 40 cc. in contrast to the variable expulsion; a feature that cannot be tolerated in situations where accurate time-metering is necessary.
Example 11 A 12-inch diameter, 0.012-inch thick cylindrical container of the general design shown in FIG. 2 was constructed with 6-inch radial hemispherical ends, one of which was closed while the other was provided with an emergent opening. The loWer,-emergent hemisphere and the main cylindrical portion were constructed of a 24 layer coating of polytetrafluoroethylene with 25 volume percent nickel flake interspersed at layers 14, 18, and 20 listed in Example I. The nickel comprised particles with an average flat diameter of microns with an average thickness of 10 microns made by the Metals Disintegrating Company, and identified commercially as their product code MD-750 nickel flake leafing grade.
The upper hemispherical section comprised a series of 9 latitudinal bands approximately l-inch in width alternating between the nickel-resin interlayer and plain resin layer.
The expulsion characteristics of this container filled initially with unsymmetrical dimethylhydrazine under a pressure head of 15 lb./sq. in. gauge are shown in the following tabulation compared with a non-modular expulsion container of equivalent thickness.
T able-Expulsion performance [Pressure: 15 lb./sq. in. Temperature 27.5 0.]
Modulated Container Non-modulated Volume ume (cc.) (00.) Time (min) Accumulated Incremental Accumulated Incremental These results are typical of the differences observed with modulated and non-modulated containers. The modulated container remains substantially the same in providing the time-metered expulsion increment whereas the non-modulated shows serious, erratic expulsion. Of particular significance is the even or constant expulsion after a pause of 96 minutes in the case of the modulated container in contrast to the extremely variable increment in the case of the non-modulated container. It cannot be over-emphasized that the dependable, constant metering in the case of the modulated container is highly important in spacecraft flight where impulses to change or adjust the orbital direction are pre-arranged based on metered reactants serving to provide the necessary propulsion. The performance of the non-modulated container, which undergoes random or crenulated collapse, would be most disastrous if the spacecraft propulsion systems were dependent upon the erratic expulsion.
The above examples merely illustrate the performance characteristics are not intended to be restrictive to the rather obvious modifications and equivalents.
For chemically reactive and corrosive fluids, including gases and mobile slurries, the preferred resins for attaining flexible containers are those derived from fluorinate polymers and elastomers, the latter term applying to a class of rubber-like materials having a higher order of yield and recovery than ordinary resins or polymers. For example, fluorinated polymers are referred to those having a recoverable yield strain of to 30 percent, whereas the elastomers as intended in this invention have a recoverable yield strain of 100 to 300 percent. The most preferred fluorocarbon polymers include polytetrafluoroethylene and the related copolymer with hexafluoropropylene produced by E. I. du Pont de Nemours and Co., Inc. as Teflon 100 PEP series of polymers. These are applied either as single polymer dispersions or as mixed or co-dispersions in ranges from 1 to 99 or 99 to 1 percent of the respective polymer and copolymer. Flexible containers made of elastomer fluorocarbon such as the copolymer of vinylidene fluoride and hexafiuoropropylene, made by E. I. du Pont de Nemours under the trade name Viton, are also intended in this invention comprising hemispherically modulated construction.
The layered arrangement shown in FIG. 6 is also modified by various sequences of the metal-dispersion interlayers to include any variation including symmetrical or exponential buildup. For instance, high reliability in the expulsion performance has been attained by rearranging the layers shown in FIG. 6 to include diagonal and stagger patterns across the latitudinal bands. Additionally the cross-sectional width has been modified to provide feathered, or humped lay-up of the dispersed metal component.
In addition to aluminum and nickel in flaked form, a variety of metals and metal alloys can be used including silver, lead, iron, platinum, stainless steels, tantalum, titanium and gold to provide the increased modulus. These can be not only in flake form but also in microscopic and submicroscopic fibrous, acicular and isometric form. Besides metals themselves, a variety of metal oxides, silicides, and other chemically inert materials with respect to the contained fluid can be used to stiffen the structure.
While the uses have been illustrated with pressured expulsion systems, the flexible containers can be used in submersed metering of reagents including incremental introduction in storage tanks and process reactors. Accordingly the present invention shall not be limited to the specific examples shown or described therein.
I claim:
1. A flexible, modulated container comprising a hemispherical structure of uniform thickness consisting of latitudinal bands with alternating materials of different flexural modulus.
2. A flexible, modulated container comprising a hemispherical structure of uniform thickness comprising alternating latitudinal bands of different materials having at least 5/4 ratio of flexural modulus developed by layered inclusion of metallic components.
3. A flexible, modulated container comprising a hemispherical structure according to claim 1 made of polyhaloethylene resins.
4. A flexible, modulated container comprising a hemispherical structure according to claim 3 made of multiple applications of polytetrafluoroethylene with occluded interlayers built up from added metallic flakes, fibers, and spheres in a volume ratio of at least 5/1 to the polymer component.
References Cited by the Examiner UNITED STATES PATENTS 2,139,143 12/38 Wiswell 222 2,285,502 6/42 Dreyfus 1858 2,347,379 4/44 Teeter 220-85 2,360,590 10/44 Schweller 13830 2,387,486 10/45 Zellos 9247 2,459,317 1/49 Granberg 13830 2,480,558 8/49 De Kiss 138-30 2,685,316 8/54 Krasno 5 2,817,878 12/57 Anspon 1858 2,880,902 4/59 Owsen 150-0.5 2,886,084 5/59 Davison 1505 3,035,302 5/62 Lysobey 185 3,038,199 6/62 Bartow et al 18-5 JOSEPH R. LECLAIR, Primary Examiner.
LAVERNE D. GEIGER, FRANKLIN T. GARRETT,
Examiners.
Claims (1)
1. A FLEXIBLE, MODULATED CONTAINER COMPRISING A HEMISPHERICAL STRUCTURE OF UNIFORM THICKNESS CONSISTING OF LATITUDINAL BANDS WITH ALTERNATING MATERIALS OF DIFFERENT FLEXURAL MODULUS.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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US198954A US3213913A (en) | 1962-05-31 | 1962-05-31 | Flexible containers |
US428823A US3229014A (en) | 1962-05-31 | 1965-01-28 | Methods of making a flexible container |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US198954A US3213913A (en) | 1962-05-31 | 1962-05-31 | Flexible containers |
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US3213913A true US3213913A (en) | 1965-10-26 |
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US198954A Expired - Lifetime US3213913A (en) | 1962-05-31 | 1962-05-31 | Flexible containers |
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Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3339803A (en) * | 1965-03-05 | 1967-09-05 | Arde Inc | Fluid storage and expulsion system |
US3592360A (en) * | 1967-06-28 | 1971-07-13 | Arde Inc | Cylindrical fluid storage and expulsion tank |
US4757917A (en) * | 1986-06-04 | 1988-07-19 | Arde, Inc. | Fluid storage and expulsion system |
US5176178A (en) * | 1991-02-20 | 1993-01-05 | Aos Holding Company | Accumulator with randomly uniplanar bladder collapse |
US5447142A (en) * | 1994-12-06 | 1995-09-05 | Caterpillar Inc. | Method and apparatus for maintaining reservoir pressure of a consumable, compressible fuel |
WO2000009938A1 (en) * | 1998-08-10 | 2000-02-24 | Alliedsignal Inc. | Vessel with a bladder for reducing vaporization of fluids blends |
WO2002032788A1 (en) * | 2000-10-19 | 2002-04-25 | Korrotech Gmbh & Co. Kg | Container with a rubber coating, for holding aggressive media |
EP1201567A1 (en) | 2000-10-27 | 2002-05-02 | General Trailers France | Container tank as well as method for emptying the same |
US20040188449A1 (en) * | 2003-03-31 | 2004-09-30 | Thompson Scott R. | Pressure vessel for compressed gases utilizing a replaceable and flexible liner |
US20060180678A1 (en) * | 2005-01-07 | 2006-08-17 | Meyer Products, Inc. | Deicing apparatus |
EP3146250A4 (en) * | 2014-05-20 | 2018-01-17 | AMTROL Licensing Inc. | Pressure absorber for a fluid system and method of use |
US9933100B2 (en) | 2014-05-20 | 2018-04-03 | Amtrol Licensing, Inc. | Multi-layered gas-filled bladder for accommodating changes in fluid characteristics within a fluid delivery system |
US11097871B2 (en) * | 2017-05-31 | 2021-08-24 | Yoshino Kogyosho Co., Ltd. | Synthetic resin container |
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---|---|---|---|---|
US2139143A (en) * | 1937-03-27 | 1938-12-06 | Norman N Wiswell | Collapsing container and collapsing device |
US2285502A (en) * | 1937-11-04 | 1942-06-09 | Celanese Corp | Manufacture of tubes and other hollow articles |
US2347379A (en) * | 1942-11-30 | 1944-04-25 | Gen Motors Corp | Pressure tank |
US2360590A (en) * | 1942-11-30 | 1944-10-17 | Gen Motors Corp | Pressure tank |
US2387486A (en) * | 1944-08-15 | 1945-10-23 | Zellos Andrew | Bellows |
US2459317A (en) * | 1944-02-07 | 1949-01-18 | Albert J Granberg | Fueling system |
US2480558A (en) * | 1944-03-09 | 1949-08-30 | Bendix Aviat Corp | Accumulator |
US2685316A (en) * | 1952-05-12 | 1954-08-03 | Louis R Krasno | Vacuum container |
US2817878A (en) * | 1953-05-22 | 1957-12-31 | Gen Aniline & Film Corp | Production of polymeric alpha-chloro-acrylate sheets |
US2880902A (en) * | 1957-06-03 | 1959-04-07 | Owsen Peter | Collapsible article |
US2886084A (en) * | 1958-07-30 | 1959-05-12 | Delphine L Davison | Collapsible double wall container |
US3035302A (en) * | 1959-03-11 | 1962-05-22 | Lysobey John | Extrusion and forming of plastic tubing |
US3038199A (en) * | 1960-01-27 | 1962-06-12 | Western Electric Co | Method and apparatus for pressing moldable material |
-
1962
- 1962-05-31 US US198954A patent/US3213913A/en not_active Expired - Lifetime
Patent Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
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US2139143A (en) * | 1937-03-27 | 1938-12-06 | Norman N Wiswell | Collapsing container and collapsing device |
US2285502A (en) * | 1937-11-04 | 1942-06-09 | Celanese Corp | Manufacture of tubes and other hollow articles |
US2347379A (en) * | 1942-11-30 | 1944-04-25 | Gen Motors Corp | Pressure tank |
US2360590A (en) * | 1942-11-30 | 1944-10-17 | Gen Motors Corp | Pressure tank |
US2459317A (en) * | 1944-02-07 | 1949-01-18 | Albert J Granberg | Fueling system |
US2480558A (en) * | 1944-03-09 | 1949-08-30 | Bendix Aviat Corp | Accumulator |
US2387486A (en) * | 1944-08-15 | 1945-10-23 | Zellos Andrew | Bellows |
US2685316A (en) * | 1952-05-12 | 1954-08-03 | Louis R Krasno | Vacuum container |
US2817878A (en) * | 1953-05-22 | 1957-12-31 | Gen Aniline & Film Corp | Production of polymeric alpha-chloro-acrylate sheets |
US2880902A (en) * | 1957-06-03 | 1959-04-07 | Owsen Peter | Collapsible article |
US2886084A (en) * | 1958-07-30 | 1959-05-12 | Delphine L Davison | Collapsible double wall container |
US3035302A (en) * | 1959-03-11 | 1962-05-22 | Lysobey John | Extrusion and forming of plastic tubing |
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Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3339803A (en) * | 1965-03-05 | 1967-09-05 | Arde Inc | Fluid storage and expulsion system |
US3592360A (en) * | 1967-06-28 | 1971-07-13 | Arde Inc | Cylindrical fluid storage and expulsion tank |
US4757917A (en) * | 1986-06-04 | 1988-07-19 | Arde, Inc. | Fluid storage and expulsion system |
US5176178A (en) * | 1991-02-20 | 1993-01-05 | Aos Holding Company | Accumulator with randomly uniplanar bladder collapse |
US5447142A (en) * | 1994-12-06 | 1995-09-05 | Caterpillar Inc. | Method and apparatus for maintaining reservoir pressure of a consumable, compressible fuel |
EP0716224A1 (en) * | 1994-12-06 | 1996-06-12 | Caterpillar Inc. | Method and apparatus for maintaining reservoir pressure of a consumable, compressible fuel |
WO2000009938A1 (en) * | 1998-08-10 | 2000-02-24 | Alliedsignal Inc. | Vessel with a bladder for reducing vaporization of fluids blends |
US6234352B1 (en) | 1998-08-10 | 2001-05-22 | Alliedsignal Inc. | Method and apparatus to reduce fractionation of fluid blend during storage and transfer |
WO2002032788A1 (en) * | 2000-10-19 | 2002-04-25 | Korrotech Gmbh & Co. Kg | Container with a rubber coating, for holding aggressive media |
EP1201567A1 (en) | 2000-10-27 | 2002-05-02 | General Trailers France | Container tank as well as method for emptying the same |
FR2815948A1 (en) * | 2000-10-27 | 2002-05-03 | Gen Trailers France | TANK FOR AN INDUSTRIAL VEHICLE AND METHOD FOR DRAINING SUCH A TANK |
US20040188449A1 (en) * | 2003-03-31 | 2004-09-30 | Thompson Scott R. | Pressure vessel for compressed gases utilizing a replaceable and flexible liner |
US7021488B2 (en) * | 2003-03-31 | 2006-04-04 | Matheson Tri-Gas, Inc. | Pressure vessel for compressed gases utilizing a replaceable and flexible liner |
US20060180678A1 (en) * | 2005-01-07 | 2006-08-17 | Meyer Products, Inc. | Deicing apparatus |
US7588195B2 (en) * | 2005-01-07 | 2009-09-15 | Louis Berkman Winter Products | Deicing apparatus |
EP3146250A4 (en) * | 2014-05-20 | 2018-01-17 | AMTROL Licensing Inc. | Pressure absorber for a fluid system and method of use |
US9933100B2 (en) | 2014-05-20 | 2018-04-03 | Amtrol Licensing, Inc. | Multi-layered gas-filled bladder for accommodating changes in fluid characteristics within a fluid delivery system |
US10247347B2 (en) | 2014-05-20 | 2019-04-02 | Amtrol Licensing Inc. | Multi-layered gas-filled bladder for accommodating changes in fluid characteristics within a fluid delivery system |
US11097871B2 (en) * | 2017-05-31 | 2021-08-24 | Yoshino Kogyosho Co., Ltd. | Synthetic resin container |
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