US2833029A - Process of making high pressure fluid containers - Google Patents

Process of making high pressure fluid containers Download PDF

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Publication number
US2833029A
US2833029A US582610A US58261056A US2833029A US 2833029 A US2833029 A US 2833029A US 582610 A US582610 A US 582610A US 58261056 A US58261056 A US 58261056A US 2833029 A US2833029 A US 2833029A
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United States
Prior art keywords
wire
liner
high pressure
mesh
container
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Expired - Lifetime
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US582610A
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Thomas F Kearns
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Individual
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Priority claimed from US441957A external-priority patent/US2827195A/en
Application filed by Individual filed Critical Individual
Priority to US582610A priority Critical patent/US2833029A/en
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Publication of US2833029A publication Critical patent/US2833029A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D51/00Making hollow objects
    • B21D51/16Making hollow objects characterised by the use of the objects
    • B21D51/24Making hollow objects characterised by the use of the objects high-pressure containers, e.g. boilers, bottles
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4981Utilizing transitory attached element or associated separate material
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49863Assembling or joining with prestressing of part
    • Y10T29/49874Prestressing rod, filament or strand

Definitions

  • This invention relates to containers for high pressure fluids.
  • a container of high pressure fluids is an important necessity, as, for example, oxygen bottles for aircraft.
  • these containers both large and small, have usually been formed of wrought steel or aluminum alloy and require, in the large units, heavy sections and welded joints which introduce inherent strength limitations.
  • the heavy homogenous walls which form the major strength elements in these containers when highly stressed, are subject to crack propagation and fragmentation as a result of gunfire or explosion.
  • the invention consists in forming a container of a relatively weak sealing liner contained in a mesh of wire of relatively greater strength.
  • An important object of the invention is to provide a container for high pressure fluids which contains relatively light materials but is strongly resistant to internal pressures. Another object is to provide a container which eliminates use of heavy castings or forgings and Welds with their limitations on strength.
  • Still another object is to provide a high pressure container which is free of crack formation and fragmentation on rupture. Additional objects relate to reduction of critical materials, increased flexibility, reduced complexity in methods of manufacture in relation to high pressure containers, elimination of wear factors in reinforcing mesh wires resulting in breakdown, and use of wire winding procedure insuring uniform stresses on the wire mesh at all radial angles and layer distances from the center of the container.
  • Fig. 1 is a view in elevation of a typical container of spherical shape
  • Fig. 2 is a sectional vew of the container taken along lines 2-2 of Fig. 1;
  • Fig. 3 is a detail view showing the mesh formation
  • Fig. 4 is a detail view showing a. section of flexed sealing shell susceptible to elastic take-up when stressed by the expansive contents of the container.
  • a typical container unit is illustrated, the structure of the unit being shown more clearly in Fig. 2 to include the inner sealing liner 14 and the mesh shell 15 enclosing the liner.
  • the sealing liner is formed preferably in two sections 17 and 18 fitted and welded or otherwise attached together to form a closed spherical cavity with the adjoining edges engaging in overlying relationship.
  • the liner is of flexible material such as brass, copper or aluminum alloys. At the pole points of each half section, fittings 20 and 21 particularly likely at the inner mesh layers.
  • each fitting includes an arced root member 27 attachable to the liner, a short tube 28 having attachment means such as the screw thread 29 at the outer end thereof for connection to inlet or outlet pipe lines, and a clamp element 30 attached to the tube and having an extended flange for overlying the mesh layer and resisting side im-' pact on'the tube end.
  • the wire mesh 15 is constructed of a metalwire 16 having a relatively high tensile strength, such as piano or music wire.
  • the shell is first filled with solid material in particle form, e. g., sand, in order to give solid support to the yieldable shell wall during the wire winding step, this material being removed after the mesh is completed.
  • the wire is carried around the great circumference of the liner, with the angular relationship of liner surface and wire progressivly varying after each loop by approximately equal increments so that consecutive wire layers are formed with a strand section at any point being angularly disposed relative to adjacent strand sections, as indicated in Fig. 3.
  • the wire ends are secured in any suitable manner and the mesh impregnated with a filler, such as the phenolic or other resins, e. g., acrylic resin.
  • a filler such as the phenolic or other resins, e. g., acrylic resin.
  • the purpose of this plastic embedment is not only to insure immobilization of the wire strand structure but also aid in the prevention of corrosion and injury from impact.
  • the clamp elements 30 are forced closely on the mesh.
  • the shell is susceptible to marked deformation, or merely to permit use of thinner gauge metal
  • the flexible liner tends to flatten as the mesh layer yields.
  • lighter shell metal may be used.
  • Metal wires for the mesh are indicated as desirable for the reason that with wires of reduced strength either i the wire must be so large as to be bulky, or a coating of substantial thickness must be provided, as in glass fiber,
  • the casing 10 is spherical in shape, it is apparent that cylindrical or other shapes are feasible depending on the requirements of use. Also, while a solid granular material, such as sand, is indicated to provide pressure resistance in the wire wrapping step, any pressure resistant removable material may be used.
  • a high pressure fluid container comprising forming a sealed inner liner of flexible material having at least one transport duct connected thereto and communicating with the liner interior, filling said liner only with removable pressure resistant material through said transport duct to give support to said liner during subsequent wire winding of said liner, wrapping the liner exterior with reinforcing wire under tension to form a pressure resistant layer external to said liner, and removing said pressure resistant material from the interior of said liner.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Description

May 6, 1958 T. F. KEARNS 2,833,029
PROCESS OF MAKING HIGH PRESSURE FLUID CONTAINERS Original Filed July 7. 1954 I N VEN TOR mamas E ram/vs ATTORNEYS PROCESS OF MAKING their PRESSURE FLUID CONTAINERS 7 Thomas FrKearns, Arlington, Va.
Original application July 7, 1954, Serial No. 441357. Divided and this application May 3, 1956, Serial No. 582,610 r -4 Claims. or. 29-423 (Grantedunder Title 35, U. s. Code 1952 see. 266) The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
This invention relates to containers for high pressure fluids.
In many fields, a container of high pressure fluids is an important necessity, as, for example, oxygen bottles for aircraft. Heretofore, these containers, both large and small, have usually been formed of wrought steel or aluminum alloy and require, in the large units, heavy sections and welded joints which introduce inherent strength limitations. Moreover, the heavy homogenous walls which form the major strength elements in these containers, when highly stressed, are subject to crack propagation and fragmentation as a result of gunfire or explosion.
Broadly stated, the invention consists in forming a container of a relatively weak sealing liner contained in a mesh of wire of relatively greater strength.
An important object of the invention is to provide a container for high pressure fluids which contains relatively light materials but is strongly resistant to internal pressures. Another object is to provide a container which eliminates use of heavy castings or forgings and Welds with their limitations on strength.
Still another object is to provide a high pressure container which is free of crack formation and fragmentation on rupture. Additional objects relate to reduction of critical materials, increased flexibility, reduced complexity in methods of manufacture in relation to high pressure containers, elimination of wear factors in reinforcing mesh wires resulting in breakdown, and use of wire winding procedure insuring uniform stresses on the wire mesh at all radial angles and layer distances from the center of the container.
Other objects and features of the invention will become apparent on consideration of the following description of a preferred form of the invention and of the accompanying drawing, in which:
Fig. 1 is a view in elevation of a typical container of spherical shape;
Fig. 2 is a sectional vew of the container taken along lines 2-2 of Fig. 1;
Fig. 3 is a detail view showing the mesh formation; and
Fig. 4 is a detail view showing a. section of flexed sealing shell susceptible to elastic take-up when stressed by the expansive contents of the container.
In Fig. 1, a typical container unit is illustrated, the structure of the unit being shown more clearly in Fig. 2 to include the inner sealing liner 14 and the mesh shell 15 enclosing the liner.
The sealing liner is formed preferably in two sections 17 and 18 fitted and welded or otherwise attached together to form a closed spherical cavity with the adjoining edges engaging in overlying relationship. The liner is of flexible material such as brass, copper or aluminum alloys. At the pole points of each half section, fittings 20 and 21 particularly likely at the inner mesh layers.
r r a are inserted in apertures formed at these points, fitting 20 serving, for example, as an inlet to the interior chamber 25 and fitting 21 as an outlet. Permanent connection between liner and fitting is made by brazingor welding. As shown, each fitting includes an arced root member 27 attachable to the liner, a short tube 28 having attachment means such as the screw thread 29 at the outer end thereof for connection to inlet or outlet pipe lines, and a clamp element 30 attached to the tube and having an extended flange for overlying the mesh layer and resisting side im-' pact on'the tube end.
The wire mesh 15 is constructed of a metalwire 16 having a relatively high tensile strength, such as piano or music wire. 'In forming the mesh the shell is first filled with solid material in particle form, e. g., sand, in order to give solid support to the yieldable shell wall during the wire winding step, this material being removed after the mesh is completed. The wire is carried around the great circumference of the liner, with the angular relationship of liner surface and wire progressivly varying after each loop by approximately equal increments so that consecutive wire layers are formed with a strand section at any point being angularly disposed relative to adjacent strand sections, as indicated in Fig. 3.
When the mesh winding is completed the wire ends are secured in any suitable manner and the mesh impregnated with a filler, such as the phenolic or other resins, e. g., acrylic resin. The purpose of this plastic embedment is not only to insure immobilization of the wire strand structure but also aid in the prevention of corrosion and injury from impact. On the completion of the wire impregnation the clamp elements 30 are forced closely on the mesh.
Where due to large size of the shell or high pressures in use the shell is susceptible to marked deformation, or merely to permit use of thinner gauge metal, it may be advantageous to form the liner with furrows or depressions as indicated by 40, in Fig. 4, the wire 41 lying tangent to the shell ridges. On application of internal pressure the flexible liner tends to flatten as the mesh layer yields. Thus, the likelihood'of liner fracture is diminished and lighter shell metal may be used.
In the winding operation it is usually desirable to increase the wire tension in successive layers so that in use all the wire layers are under the same radial stress. This arises from the fact that the inner shells of a spherical layer of substantial thickness are subject to higher pressures, and hence, with progressively increased layer tensions, moving radially outwardly, the possibility of shell fracture is reduced.
Metal wires for the mesh are indicated as desirable for the reason that with wires of reduced strength either i the wire must be so large as to be bulky, or a coating of substantial thickness must be provided, as in glass fiber,
these inner layers lose the support of the layer material and break progressively outwardly until the sealing shell is disrupted.
While in the preferred form of the disclosure the casing 10 is spherical in shape, it is apparent that cylindrical or other shapes are feasible depending on the requirements of use. Also, while a solid granular material, such as sand, is indicated to provide pressure resistance in the wire wrapping step, any pressure resistant removable material may be used.
Obviously, modifications other than these described may be made and hence it is understood that the invention 7 Patented May 6, 1958 Eventually, I
1. The process of making a high pressure fluid container comprising forming a sealed inner liner of flexible material having at least one transport duct connected thereto and communicating with the liner interior, filling said liner only with removable pressure resistant material through said transport duct to give support to said liner during subsequent wire winding of said liner, wrapping the liner exterior with reinforcing wire under tension to form a pressure resistant layer external to said liner, and removing said pressure resistant material from the interior of said liner.
2. The process of making a high pressure resistant container as defined in claim 1 including additionally the step Cir a '4 of impregnating the wire layer with a protective and immobilizing coating.
3. The process of making a high pressure resistant container as defined in claim 1 with said wrapping continued to form a wall of several Wire layers, and applying progressively increased tension to the Wire as each layer is applied to the liner exterior.
4. The process of making a high pressure resistant container as defined in claim 3 and impregnating the wire layers with a protective and immobilizing coating.
References Cited in the file of this patent UNITED STATES PATENTS Lindsay Apr. 3, 1945
US582610A 1954-07-07 1956-05-03 Process of making high pressure fluid containers Expired - Lifetime US2833029A (en)

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Application Number Priority Date Filing Date Title
US582610A US2833029A (en) 1954-07-07 1956-05-03 Process of making high pressure fluid containers

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US441957A US2827195A (en) 1954-07-07 1954-07-07 Container for high pressure fluids
US582610A US2833029A (en) 1954-07-07 1956-05-03 Process of making high pressure fluid containers

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3040426A (en) * 1958-10-30 1962-06-26 Philip K Horrigan Method of fabricating miniature bellows by electroless chemical deposition
US3304138A (en) * 1964-08-14 1967-02-14 Gen Motors Corp Antifriction bearing
US3471920A (en) * 1967-08-28 1969-10-14 United Aircraft Corp Pressure vessel construction

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1804888A (en) * 1926-12-02 1931-05-12 Monsch Simon Pierre Pipe coiled with steel wire for pressure conduits and vessels under pressure
US2366141A (en) * 1943-06-25 1944-12-26 Edward D Andrews Method of making pressure containers
US2371107A (en) * 1945-03-06 Method of and apparatus fob winding
US2373038A (en) * 1943-03-03 1945-04-03 American La France Fomaite Cor Process of making reinforced gas flasks

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2371107A (en) * 1945-03-06 Method of and apparatus fob winding
US1804888A (en) * 1926-12-02 1931-05-12 Monsch Simon Pierre Pipe coiled with steel wire for pressure conduits and vessels under pressure
US2373038A (en) * 1943-03-03 1945-04-03 American La France Fomaite Cor Process of making reinforced gas flasks
US2366141A (en) * 1943-06-25 1944-12-26 Edward D Andrews Method of making pressure containers

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3040426A (en) * 1958-10-30 1962-06-26 Philip K Horrigan Method of fabricating miniature bellows by electroless chemical deposition
US3304138A (en) * 1964-08-14 1967-02-14 Gen Motors Corp Antifriction bearing
US3471920A (en) * 1967-08-28 1969-10-14 United Aircraft Corp Pressure vessel construction

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