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US900763A - Non-explosive closure for tanks. - Google Patents

Non-explosive closure for tanks. Download PDF

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Publication number
US900763A
US900763A US1906343991A US900763A US 900763 A US900763 A US 900763A US 1906343991 A US1906343991 A US 1906343991A US 900763 A US900763 A US 900763A
Authority
US
United States
Prior art keywords
disk
tanks
cap
ring
tank
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
Inventor
William H Mcnutt
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.)
WILLIAM E ROCHE
Original Assignee
WILLIAM E ROCHE
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by WILLIAM E ROCHE filed Critical WILLIAM E ROCHE
Priority to US1906343991 priority Critical patent/US900763A/en
Application granted granted Critical
Publication of US900763A publication Critical patent/US900763A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • B65D51/00Closures not otherwise provided for
    • B65D51/16Closures not otherwise provided for with means for venting air or gas
    • B65D51/1605Closures not otherwise provided for with means for venting air or gas whereby the interior of the container is maintained in permanent gaseous communication with the exterior
    • B65D51/1611Closures not otherwise provided for with means for venting air or gas whereby the interior of the container is maintained in permanent gaseous communication with the exterior by means of an orifice, capillary or labyrinth passage
    • 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
    • Y10T137/00Fluid handling
    • Y10T137/1624Destructible or deformable element controlled
    • Y10T137/1632Destructible element
    • Y10T137/1789Having pressure responsive valve
    • 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
    • Y10T137/00Fluid handling
    • Y10T137/1624Destructible or deformable element controlled
    • Y10T137/1797Heat destructible or fusible
    • Y10T137/1812In fluid flow path

Definitions

  • WILLIAM HLMONUTT OF NEW YORK, N. Y., ASSIGNOR TO WILLIAM E. ROCHE, OF NEW -YORK, 'N. Y.
  • FIG. 1 is a side elevation of the tank cap.
  • Fig. 2 is a plan view of the cap.
  • Fig. 3 is a'partial cross section.
  • Fig. 4 is a plan view of the safety disk.
  • Figs. 5, 6 and 7 show the several apertured members permitting escape of the gas without back fire of the flame; and
  • Fig. 8 is a vertical section showing a modified form of cap and indicator.
  • the cap is secured to the tank in any desired manner. It is shown as-comprising a sleeve 15 having an external threaded port1on 16 by which it may be screwed into the tank 17.
  • the cap may be provided with a polygonal rim portion 18 for engagement by a wrench.
  • the cap has an annular rabbet portion 19 in which is fitted safety cap 20, shown separately in Fig. 4.
  • the diameter-of the cap is somewhat smaller than the rabbet portion leaving a space between the opposite curved walls. And these latter walls are shown as provided with annular channels.
  • the wall 21 of the rabbet portion being shown as having a channel 22; while the periphery of the disk. 20 is shown as having a channel 23, that is located opposite the channel 22,. as shown in Fig. 3.
  • Any suitable fusible binding material is placed in the space between the periphery of the disk 20 and the opposite wall 21, such as a fusible cement 24- as shown. This cement will flow or is forced into the two channels and serves as locking means to prevent removal of the disk -or cover 20 by ordinary pressure. But
  • this fusible ring 24 will melt or become plastic and lose its rigidity, thereby permitting the pressure in the tank, that will be elevated by the gases generated from the heat, to blow off the cap 20.
  • the gases issuing from the tank would be at once ignited, and if the burning gases should reach the surface of the fluid in the tank, all-explosion would occur.
  • one -or more finely apertured partitions are located below the position of the cover 20. In the construction illustrated there are shown three apertured plates. A disk 25 of coarse wire gauze is placed a short distance removed from the cover 20; thereupon a second disk of wire gauze 26 of somewhat finer mesh, is
  • This invention is of great utility in connection with the use of gasolene or naphtha for explosive engines, or for generating steam for engines, carried by motor vehicles or launches.
  • the fusible ring Upon a fire starting in either of such places, the fusible ring will permit the cap to blow out, and gas will burn outside of the perforated plates, without reaching the gasolene or naphtha; and thereby prevent an explosion.
  • the burning gas can be readily extinguished by cutting off the air and covering it'as with a cloth or the like; and it will not be necessary to draw off the gasolene or naphtha from the lower part of the tank, thereby tending to cause an explosion.
  • the cap 20 can be readily replaced after being blown out, by the use of'a new fusible ring.
  • a fusible closing device can be used in connection with the apertured plate or plates that will yield or blow out upon the application of heat, permitting escape of the vapors from the contents of the tank.
  • Fig. 8 is shown a modification in which a glass plate 32 is used instead of the disk 20. The plate 32 being located above the wire plate 25, and separated therefrom by a ring 33. Upon undue pressure being generated by heat reaching the tank, this glass plate will be readily broken, permitting escape of the gases. And the heat will ignite the gases outside of the apertured plate or plates, that will prevent the flame passing back into thetank.
  • the intermediate diaphragm 26 of fine mesh acts as a safety plate to prevent passage of flame protect-ed on both sides from injury by a foreign body, or from extreme pressure.
  • a closure for tanks comprising a bushing provided with an annular shouldered portion at its outer part, a closure disk lo cated in said shouldered portion and of less diameter than the shouldered portion, "the disk being provided with an annular channel in its periphery, the opposite wall of the shouldered portion being also provided with an annular channel, a fusible ring arranged between the periphery of the disk and the channel portion whereby the disk is normally locked in position, the bushing having its aperture threadedat one portion, a plurality of apertured diaphragms extending across the aperture, ring members separating the diaphragms at their margins, and a ring nut threaded in the aperture of said bushing clamping the diaphragm and ring members in position.
  • a closure for tanks comprising a bushing, fusible means arranged to close the aperture in the bushing at normal temperature, said bushing being internally threaded at its opposite end, a series of apertured diaphragans located in the bushing, ring members inserted between the diaphragms at their margins to separate the diaphragms, and a ring nut member screwed into the threaded aperture to clamp the diaphragm and ring members in position.

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

Description

' W. H. MONUTT'. NON-EXPLOSIVE CLOSURE FOE TANKS.
I i APPLICATION FILED NOV. 19, 1906.
Patented 001;. 13,1908.
Inventor; Zbdlz'amH/Mc/Yutt.
UNITED STATES} PATENT OFFICE.
WILLIAM HLMONUTT, OF NEW YORK, N. Y., ASSIGNOR TO WILLIAM E. ROCHE, OF NEW -YORK, 'N. Y.
,Specification of Letters Patent.
Patented Oct. 13, 1908.
Application filed November 19,1996. Serial No. 348,991
To all whom it mag concern:
Be it known that I, WILLIAM H. MoNU'rr, a citizen of the United States, residing in New York city, in the county of New York and State of New York, have invented oer-, tain new and useful improvementsin Non- Explosive Closures for Tanks, of which the in %n the accompanying drawings is illus trated embodiments of the invention, in which Figure 1 is a side elevation of the tank cap. Fig. 2 is a plan view of the cap. Fig. 3 is a'partial cross section. Fig. 4is a plan view of the safety disk. Figs. 5, 6 and 7 show the several apertured members permitting escape of the gas without back fire of the flame; and Fig. 8 is a vertical section showing a modified form of cap and indicator.
The cap is secured to the tank in any desired manner. It is shown as-comprising a sleeve 15 having an external threaded port1on 16 by which it may be screwed into the tank 17. The cap may be provided with a polygonal rim portion 18 for engagement by a wrench. p r
At the upper portion the cap has an annular rabbet portion 19 in which is fitted safety cap 20, shown separately in Fig. 4. The diameter-of the cap is somewhat smaller than the rabbet portion leaving a space between the opposite curved walls. And these latter walls are shown as provided with annular channels. The wall 21 of the rabbet portion being shown as having a channel 22; while the periphery of the disk. 20 is shown as having a channel 23, that is located opposite the channel 22,. as shown in Fig. 3. Any suitable fusible binding material is placed in the space between the periphery of the disk 20 and the opposite wall 21, such as a fusible cement 24- as shown. This cement will flow or is forced into the two channels and serves as locking means to prevent removal of the disk -or cover 20 by ordinary pressure. But
upon the tank being subjected to heat, this fusible ring 24 will melt or become plastic and lose its rigidity, thereby permitting the pressure in the tank, that will be elevated by the gases generated from the heat, to blow off the cap 20. The gases issuing from the tank would be at once ignited, and if the burning gases should reach the surface of the fluid in the tank, all-explosion would occur. In order toprevcnt the gas from igniting at the surface of the liquid, one -or more finely apertured partitions are located below the position of the cover 20. In the construction illustrated there are shown three apertured plates. A disk 25 of coarse wire gauze is placed a short distance removed from the cover 20; thereupon a second disk of wire gauze 26 of somewhat finer mesh, is
placed below the disk 25, and may be separated therefrom by a ring 27. Finally a disk 28 of perforated sheet metal is placed below the disk 26, and spaced therefrom by a. ring 29. All of these members may be locked in place by a threaded locking rim 30, screwing into the internal threaded portion 31 of the sleeve 15. By this construction, when the heat shall have melted the fusible locking ring 24, and the plate 20 shall have been blown off, the gas will issue through the several perforated or foraminous disks, and thereupon will be ignited by the heat. But these disks will effectually prevent the gas igniting below them, on the principle of the Davy safety lamp, wherein fire damp in mines will burn on the outside of a anze chimney, but will be prevented from 1gniting inside and causing an explosion.
This invention is of great utility in connection with the use of gasolene or naphtha for explosive engines, or for generating steam for engines, carried by motor vehicles or launches. Upon a fire starting in either of such places, the fusible ring will permit the cap to blow out, and gas will burn outside of the perforated plates, without reaching the gasolene or naphtha; and thereby prevent an explosion. Upon the fire being extinguished, the burning gas can be readily extinguished by cutting off the air and covering it'as with a cloth or the like; and it will not be necessary to draw off the gasolene or naphtha from the lower part of the tank, thereby tending to cause an explosion. The cap 20 can be readily replaced after being blown out, by the use of'a new fusible ring.
Any desired or suitable form of a fusible closing device can be used in connection with the apertured plate or plates that will yield or blow out upon the application of heat, permitting escape of the vapors from the contents of the tank. In Fig. 8 is shown a modification in which a glass plate 32 is used instead of the disk 20. The plate 32 being located above the wire plate 25, and separated therefrom by a ring 33. Upon undue pressure being generated by heat reaching the tank, this glass plate will be readily broken, permitting escape of the gases. And the heat will ignite the gases outside of the apertured plate or plates, that will prevent the flame passing back into thetank.
By the construction of the three diaphragms as shown in Fig. 3, the intermediate diaphragm 26 of fine mesh acts as a safety plate to prevent passage of flame protect-ed on both sides from injury by a foreign body, or from extreme pressure.
Having thus described my invention, I claim:
1. A closure for tanks comprising a bushing provided with an annular shouldered portion at its outer part, a closure disk lo cated in said shouldered portion and of less diameter than the shouldered portion, "the disk being provided with an annular channel in its periphery, the opposite wall of the shouldered portion being also provided with an annular channel, a fusible ring arranged between the periphery of the disk and the channel portion whereby the disk is normally locked in position, the bushing having its aperture threadedat one portion, a plurality of apertured diaphragms extending across the aperture, ring members separating the diaphragms at their margins, and a ring nut threaded in the aperture of said bushing clamping the diaphragm and ring members in position.
2. A closure for tanks comprising a bushing, fusible means arranged to close the aperture in the bushing at normal temperature, said bushing being internally threaded at its opposite end, a series of apertured diaphragans located in the bushing, ring members inserted between the diaphragms at their margins to separate the diaphragms, and a ring nut member screwed into the threaded aperture to clamp the diaphragm and ring members in position.
Signed at Numbers 9-15 Murray street, New York, N. Y., this 2nd day of July, 1906.
WILLIAM H. MCNUTT.
Witnesses:
. FRnmJ. DOLE,
WILLIAM H. REID.
US1906343991 1906-11-19 1906-11-19 Non-explosive closure for tanks. Expired - Lifetime US900763A (en)

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Application Number Priority Date Filing Date Title
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US1906343991 US900763A (en) 1906-11-19 1906-11-19 Non-explosive closure for tanks.

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426808A (en) * 1943-12-14 1947-09-02 Auer Gustavus Safety valve
US2500119A (en) * 1945-06-29 1950-03-07 Standard Oil Dev Co Fluid container
US2822961A (en) * 1954-06-25 1958-02-11 Nels W Seaquist Aerosol bomb
US2998018A (en) * 1959-07-06 1961-08-29 Lockheed Aircraft Corp Electro thermal valve
US3334780A (en) * 1963-05-24 1967-08-08 Metal Containers Ltd Pressure fluid container
US3450305A (en) * 1966-10-12 1969-06-17 Continental Can Co Venting means for containers
US4273251A (en) * 1979-02-01 1981-06-16 The Commonwealth Industrial Gases Limited Safety device
US5762091A (en) * 1996-08-01 1998-06-09 Sarne; Daniel L. Thermal-pressure relief device
US5791367A (en) * 1996-01-25 1998-08-11 Gas Research Institute Pressure relief device
US6866057B1 (en) * 2002-04-02 2005-03-15 Buehrle, Ii Harry W. Thermal-pressure relief device
US9096355B2 (en) * 2011-10-10 2015-08-04 Jensen Metal Products, Inc. Flame arresting and dispensing cap for gel and liquid fuels for ventless fireplaces
WO2023215451A1 (en) * 2022-05-04 2023-11-09 Rieke Llc Container and closure systems with flame mitigation

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426808A (en) * 1943-12-14 1947-09-02 Auer Gustavus Safety valve
US2500119A (en) * 1945-06-29 1950-03-07 Standard Oil Dev Co Fluid container
US2822961A (en) * 1954-06-25 1958-02-11 Nels W Seaquist Aerosol bomb
US2998018A (en) * 1959-07-06 1961-08-29 Lockheed Aircraft Corp Electro thermal valve
US3334780A (en) * 1963-05-24 1967-08-08 Metal Containers Ltd Pressure fluid container
US3450305A (en) * 1966-10-12 1969-06-17 Continental Can Co Venting means for containers
US4273251A (en) * 1979-02-01 1981-06-16 The Commonwealth Industrial Gases Limited Safety device
US5791367A (en) * 1996-01-25 1998-08-11 Gas Research Institute Pressure relief device
US5762091A (en) * 1996-08-01 1998-06-09 Sarne; Daniel L. Thermal-pressure relief device
US6866057B1 (en) * 2002-04-02 2005-03-15 Buehrle, Ii Harry W. Thermal-pressure relief device
US9096355B2 (en) * 2011-10-10 2015-08-04 Jensen Metal Products, Inc. Flame arresting and dispensing cap for gel and liquid fuels for ventless fireplaces
WO2023215451A1 (en) * 2022-05-04 2023-11-09 Rieke Llc Container and closure systems with flame mitigation

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