US2737453A - Gas storage apparatus - Google Patents

Gas storage apparatus Download PDF

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US2737453A
US2737453A US333431A US33343153A US2737453A US 2737453 A US2737453 A US 2737453A US 333431 A US333431 A US 333431A US 33343153 A US33343153 A US 33343153A US 2737453 A US2737453 A US 2737453A
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Prior art keywords
diaphragm
weight
vessel
storage apparatus
gas storage
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US333431A
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Lyle V Larsen
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Chicago Bridge and Iron Co
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Chicago Bridge and Iron Co
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Priority to US333431A priority Critical patent/US2737453A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17BGAS-HOLDERS OF VARIABLE CAPACITY
    • F17B1/00Gas-holders of variable capacity
    • F17B1/02Details
    • 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
    • B65D90/00Component parts, details or accessories for large containers
    • B65D90/22Safety features
    • B65D90/38Means for reducing the vapour space or for reducing the formation of vapour within containers

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  • This invention relates to fiuid storage vessels and more particularly to a control weight for a flexible diaphragm in a breather type fluid storage vessel.
  • control weight shown and described in this application is adaptable for use in connection with a flexible diaphragm in any breather type liquid storage vessel, it has been found to be particularly useful to control the operation of a hemispherical or substantially hemispherical flexible diaphragm such as shown and described in Wissmiller applications, Serial No. 638,302, filed December 29, 1945, and Serial No. 702,625, filed October 11, 1946, both of which are now abandoned.
  • the deflation pattern of the diaphragm from its fully inflated condition is quite irregular.
  • the diaphragm starts downward on one side, pivoting about the opposite side. During the latter stages of the deflation this causes a sweeping action in the bottom of the vessel which tends todecrease the life of the diaphragm.
  • the off-side loop has a tendency to collect and hold water which because of its weight is retained in the loop inasmuch as the weight of the water prevents the diaphragm from becoming fully inflated and thus eliminating the loop containing the water.
  • the weight necessary to control the configurations is but a fraction of the total weight of the whole diaphragm. Atmospheric air pressure is always present above the diaphragm and the pressure of the stored gas is only slightly above atmospheric.
  • FIGs. 1 and 2 are vertical sections through a breather type vessel substantially of the type disclosed in the said application, Serial No. 638,302, modified in accordance with this invention and showing the flexible breather diaphragm at various positions during the operation of the vessel.
  • the fluid storage vessel comprises a substantially spherical tank open at its top to the atmosphere through a covered vent 11 and being provided with a combination inlet and outlet 12 located below the equator of the vessel.
  • a flexible diaphragm 13 Secured across the interior of the vessel along the equator thereof is a flexible diaphragm 13.
  • the diaphragm is constructed 2,737,453 Patented Mar. 6, 1956 of nylon impregnated with a vaporproof material such as synthetic rubber, and has substantially the same shape as that portion of the vessel above the equator, that is, is substantially hemispherical in shape so that in its extreme upward and downward positions, as shown by the solid lines in Figs.
  • the diaphragm is substantially entirely backed up by the vessel and hence is not subject to strain because of pressures or vacuums therein.
  • a weight 14 Located in the center of the diaphragm, that is, at its pole is a weight 14.
  • the weight is a disc-like member secured to the diaphragm by any suitable means.
  • the weight in a spherical tank, such as shown in the drawings, having a diameter of 27 feet, the weight consisted of a metal disc of 14 inches in diameter and weighing 30 pounds.
  • the fabric of a 27 foot diameter tank will weigh about 47 ounces per square yard whereas the weight of that portion under the weight 14 is 30 pounds or 480 ounces on an area of just slightly more than one square foot.
  • the diaphragm has a surface area of about 127.3 square yards and a total weight of about 375 pounds whereas the control weight is 30 pounds, which is less than 10% of the total weight of the diaphragm.
  • the breather vessel as shown in the drawings is adapted to be connected to a liquid storage tank by means of the connection 12.
  • vapors such as gasoline vapors are directed into the interior of the vessel 10 where they may be accumulated.
  • vapors are withdrawn from the vessel 10 and returned thereto.
  • the pressure of the vapor under the diaphragm is generally one-eighth inch of water which is sufiicient to move the diaphragm upwardly to admit more vapor.
  • the downward force over the area of the control weight greatly exceeds the upward force of the vapor on that same area.
  • the control weight is supported by the diaphragm and thus controls the configuration of the diaphragm.
  • the diaphragm 13 assumes the position shown in the solid lines of Fig. 1.
  • the diaphragm moves downwardly assuming the configuration shown in the dotted lines. It will be noted that the configuration is quite regular with the pole bearing the weight preceding the rest of the diaphragm in its downward movement.
  • the diaphragm continues to move downward to the position shown in the dotted lines of Fig. 2. Any further contraction will result in the diaphragm collapsing against the sides of the vessel 10 to assume the position shown in the solid lines of Fig. 2.
  • a gas storage apparatus comprising a shell, a flexible diaphragm secured at its periphery across the interior of the shell along a substantially horizontal plane, said diaphragm forming with the portion of the shell below said plane a gas tight expansible chamber, the portion of the shell above the diaphragm having open communication with the atmosphere, said diaphragm being preformed to have substantially the same size and shape as the portion of the shell above said plane and being substantially completely backed up by said last mentioned portion in its extreme upward position without stressing the diaphragm and a control weight carried by the diaphragm and having a total weight exceeding the total upward force exerted by stored gas on the area under the weight so that the weight may lead the rest of the diaphragm in downward movement and may lag behind the rest of the diaphragm in upward movement, said control weight being substantially centrally located on the diaphragm for movement along a substantially vertical path within the shell so that the diaphragm assumes a regular predetermined configuration at all positions 10 thereof within

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Diaphragms And Bellows (AREA)

Description

March 6, 1956 v. LARSEN GAS STORAGE APPARATUS Filed Jan. 27, 1953 United States Patent GAS STORAGE APPARATUS Lyle V. Larsen, Chicago, Ill., assignor to Chicago Bridge & Iron Company, a corporation of Illinois Application January 27, 1953, Serial No. 333,431
1 Claim. (Cl. 48-178) This invention relates to fiuid storage vessels and more particularly to a control weight for a flexible diaphragm in a breather type fluid storage vessel.
This application is a continuation-in-part of my copending application Serial No. 93,987, filed May 18, 1949, now abandoned.
While the control weight shown and described in this application is adaptable for use in connection with a flexible diaphragm in any breather type liquid storage vessel, it has been found to be particularly useful to control the operation of a hemispherical or substantially hemispherical flexible diaphragm such as shown and described in Wissmiller applications, Serial No. 638,302, filed December 29, 1945, and Serial No. 702,625, filed October 11, 1946, both of which are now abandoned.
In the operation of hemispherical breather diaphragms of the type disclosed in said applications the deflation pattern of the diaphragm from its fully inflated condition is quite irregular. The diaphragm starts downward on one side, pivoting about the opposite side. During the latter stages of the deflation this causes a sweeping action in the bottom of the vessel which tends todecrease the life of the diaphragm. In addition the off-side loop has a tendency to collect and hold water which because of its weight is retained in the loop inasmuch as the weight of the water prevents the diaphragm from becoming fully inflated and thus eliminating the loop containing the water.
I have found that by placing a weight at the pole of a hemispherical diaphragm to force the pole to precede the outer edge of the diaphragm during deflation the weight will travel straight downward and the deflation pattern of the diaphragm is quite regular. By a regular deflation pattern I mean that the diaphragm will assume a regular and predetermined configuration at each position in the vessel. Inasmuch as the weight eliminates the sweeping action, the life of the diaphragm is increased and if water is trapped on the upper surface of the diaphragm it will be located at the center and readily accessible for removal either manually or mechanically.
The weight necessary to control the configurations is but a fraction of the total weight of the whole diaphragm. Atmospheric air pressure is always present above the diaphragm and the pressure of the stored gas is only slightly above atmospheric.
In the accompanying drawings Figs. 1 and 2 are vertical sections through a breather type vessel substantially of the type disclosed in the said application, Serial No. 638,302, modified in accordance with this invention and showing the flexible breather diaphragm at various positions during the operation of the vessel.
Referring now to the drawings, the fluid storage vessel comprises a substantially spherical tank open at its top to the atmosphere through a covered vent 11 and being provided with a combination inlet and outlet 12 located below the equator of the vessel. Secured across the interior of the vessel along the equator thereof is a flexible diaphragm 13. The diaphragm is constructed 2,737,453 Patented Mar. 6, 1956 of nylon impregnated with a vaporproof material such as synthetic rubber, and has substantially the same shape as that portion of the vessel above the equator, that is, is substantially hemispherical in shape so that in its extreme upward and downward positions, as shown by the solid lines in Figs. 1 and 2 respectively, the diaphragm is substantially entirely backed up by the vessel and hence is not subject to strain because of pressures or vacuums therein. Located in the center of the diaphragm, that is, at its pole is a weight 14. In the particular embodiment shown the weight is a disc-like member secured to the diaphragm by any suitable means. As a specific example of the invention in a spherical tank, such as shown in the drawings, having a diameter of 27 feet, the weight consisted of a metal disc of 14 inches in diameter and weighing 30 pounds. The fabric of a 27 foot diameter tank will weigh about 47 ounces per square yard whereas the weight of that portion under the weight 14 is 30 pounds or 480 ounces on an area of just slightly more than one square foot. The diaphragm has a surface area of about 127.3 square yards and a total weight of about 375 pounds whereas the control weight is 30 pounds, which is less than 10% of the total weight of the diaphragm.
It should be understood that the breather vessel as shown in the drawings is adapted to be connected to a liquid storage tank by means of the connection 12. During periods of evaporation in the tank, vapors such as gasoline vapors are directed into the interior of the vessel 10 where they may be accumulated. Upon contraction of the vapors within the storage tank, vapors are withdrawn from the vessel 10 and returned thereto. Thus, it is not necessary to vent such expanding vapors to the atmosphere with a consequent loss thereof. The pressure of the vapor under the diaphragm is generally one-eighth inch of water which is sufiicient to move the diaphragm upwardly to admit more vapor. The downward force over the area of the control weight greatly exceeds the upward force of the vapor on that same area. The control weight is supported by the diaphragm and thus controls the configuration of the diaphragm.
When the vessel is full of vapors the diaphragm 13 assumes the position shown in the solid lines of Fig. 1. As contraction of vapors occurs in the liquid storage tank the diaphragm moves downwardly assuming the configuration shown in the dotted lines. It will be noted that the configuration is quite regular with the pole bearing the weight preceding the rest of the diaphragm in its downward movement. As contraction continues the diaphragm continues to move downward to the position shown in the dotted lines of Fig. 2. Any further contraction will result in the diaphragm collapsing against the sides of the vessel 10 to assume the position shown in the solid lines of Fig. 2.
While I have shown and described certain embodiments of my invention, it is to be understood that it is capable of many modifications. Changes, therefore, in the construction and arrangement may be made without departing from the spirit and scope of the invention as disclosed in the appended claim.
I claim:
A gas storage apparatus comprising a shell, a flexible diaphragm secured at its periphery across the interior of the shell along a substantially horizontal plane, said diaphragm forming with the portion of the shell below said plane a gas tight expansible chamber, the portion of the shell above the diaphragm having open communication with the atmosphere, said diaphragm being preformed to have substantially the same size and shape as the portion of the shell above said plane and being substantially completely backed up by said last mentioned portion in its extreme upward position without stressing the diaphragm and a control weight carried by the diaphragm and having a total weight exceeding the total upward force exerted by stored gas on the area under the weight so that the weight may lead the rest of the diaphragm in downward movement and may lag behind the rest of the diaphragm in upward movement, said control weight being substantially centrally located on the diaphragm for movement along a substantially vertical path within the shell so that the diaphragm assumes a regular predetermined configuration at all positions 10 thereof within the shell avoiding sweeping of the diaphragm against the shell.
References Cited in the file of this patent UNITED STATES PATENTS McFarlan Sept. 27, 1859 Ellis Oct. 7, 1941 De Kiss June 19, 1945 Trautman June 19, 1945 Wiggins Feb. 5, 1952 FOREIGN PATENTS France Mar. 10, 1947 Great Britain Mar. 7, 1929
US333431A 1953-01-27 1953-01-27 Gas storage apparatus Expired - Lifetime US2737453A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2925014A1 (en) * 1978-06-23 1980-01-10 Arakawa Chem Ind METHOD FOR PRODUCING A STABILIZED COLOPHONIUM ESTER AND COMPOSITIONS CONTAINING IT
US4723577A (en) * 1986-10-22 1988-02-09 Sundstrand Corporation Thermal expansion reservoir
US4784181A (en) * 1985-10-07 1988-11-15 Flamco B.V. Expansion tank with a bladder-type diaphragm
US4806098A (en) * 1985-07-16 1989-02-21 Ramm Eric J Heat transfer and stabilizing apparatus

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US25607A (en) * 1859-09-27 James mcfarlan
GB307179A (en) * 1928-02-08 1929-03-07 Roland Wynn Broadhead An improved type of gasholder
US2257941A (en) * 1939-05-10 1941-10-07 Clifford A Ellis Breather reservoir
US2378467A (en) * 1943-07-22 1945-06-19 Bendix Aviat Corp Accumulator bladder
US2378517A (en) * 1943-08-16 1945-06-19 Bendix Aviat Corp Accumulator
FR924422A (en) * 1945-12-29 1947-08-05 Chicago Bridge & Iron Co Improvements to fluid accumulator devices
US2584953A (en) * 1949-01-24 1952-02-05 John H Wiggins Sealing element ventilating means for dry seal gas holders

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US25607A (en) * 1859-09-27 James mcfarlan
GB307179A (en) * 1928-02-08 1929-03-07 Roland Wynn Broadhead An improved type of gasholder
US2257941A (en) * 1939-05-10 1941-10-07 Clifford A Ellis Breather reservoir
US2378467A (en) * 1943-07-22 1945-06-19 Bendix Aviat Corp Accumulator bladder
US2378517A (en) * 1943-08-16 1945-06-19 Bendix Aviat Corp Accumulator
FR924422A (en) * 1945-12-29 1947-08-05 Chicago Bridge & Iron Co Improvements to fluid accumulator devices
US2584953A (en) * 1949-01-24 1952-02-05 John H Wiggins Sealing element ventilating means for dry seal gas holders

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2925014A1 (en) * 1978-06-23 1980-01-10 Arakawa Chem Ind METHOD FOR PRODUCING A STABILIZED COLOPHONIUM ESTER AND COMPOSITIONS CONTAINING IT
US4806098A (en) * 1985-07-16 1989-02-21 Ramm Eric J Heat transfer and stabilizing apparatus
US4784181A (en) * 1985-10-07 1988-11-15 Flamco B.V. Expansion tank with a bladder-type diaphragm
US4723577A (en) * 1986-10-22 1988-02-09 Sundstrand Corporation Thermal expansion reservoir

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