US2462064A - Pressure vessel for storage of liquids at abnormally high or low temperatures - Google Patents
Pressure vessel for storage of liquids at abnormally high or low temperatures Download PDFInfo
- Publication number
- US2462064A US2462064A US557842A US55784244A US2462064A US 2462064 A US2462064 A US 2462064A US 557842 A US557842 A US 557842A US 55784244 A US55784244 A US 55784244A US 2462064 A US2462064 A US 2462064A
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- US
- United States
- Prior art keywords
- liquids
- storage
- pressure vessel
- low temperatures
- abnormally high
- 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
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/12—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge with provision for thermal insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/08—Mounting arrangements for vessels
- F17C13/083—Mounting arrangements for vessels for medium-sized mobile storage vessels, e.g. tank vehicles or railway tank vehicles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0152—Lobes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0157—Polygonal
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/014—Suspension means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0375—Thermal insulations by gas
- F17C2203/0383—Air
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0639—Steels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0648—Alloys or compositions of metals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/221—Welding
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0107—Single phase
- F17C2223/013—Single phase liquid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/035—High pressure (>10 bar)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
Definitions
- the present'invention is particularly adapted for the storage of liquids at low temperaturesand high pressures. It may also be used for the storage of hot liquids at high pressure.
- the ordinary carbon steel loses a great deal of its impact strength at very low or very high temperatures.
- Monel metal or other high nickel alloys For example, at temperatures suitable for the storage of liquefied hydrocarbons it is desirable to employ Monel metal or other high nickel alloys.
- a relatively thin inner shell member of temperature-resistant metal, such as Monel metal may be employed in the form of a fluid-tight shell of intersecting spherical segments.
- This outward stresses of these segments are transmitted along the lines of intersection to insulating supports of non-metallic material such as Marinite to an outer shell which is preferably fluid-tight and is preferably in the form of a regular polyhedron.
- This outer shell may be made of common carbon steel.
- Fig. 1 is a plan view of one form of the improved tank
- Fig. 2 is a vertical section taken along the line 2-2 in Fig. 1'
- Fig. 3 is a section taken along the line 3-3 in Fig. 1
- Fig. 4 is a perspective view of the outside of the inner shell
- Fig. 5 is a plan view of a modified form of the invention
- F g. 6 is a section taken along the line 6-5 in Fig. 5.
- the spherical segments in intersect along the lines II which all fall in the planes of the diagonals of the cubical outer shell l2.
- the radially outward components of the stresses of the spherical segments are carried by. non-metallic insulating supporting members I3 which extend to theedg'es of the cube [2.
- the cube I2 is made up of welded plates of ordinary carbon steel.
- the space 84 between the inner and outer shells is preferably evacuated in any suitable manner. Liquid may be introduced to and withdrawn from the inner shell in the usual manner by any pipe (not shown).
- the foundations for the vessel are not part of the present invention and accordingly are not shown. It will be observed that the apex I5 of each circular segment lies on the perpendicular from the center of the adjoining side l6 of the cube, and that planes connecting the adjacent corners of the intersections would form an inscribed cube.
- the exterior shell 12a is dodecahedral in shape, and the intersecting spherical segments Illa are twelve in number, the center of each segment again, however, being located on a perpendicular beneath the center of each side.
- the spherical segments are supported along the lines of intersection Ha by the Marinite supports I311. which extend in each. case to, and only to. an edge of the outer dodecahedral shell.
- the thin inner shell is free to expand and contract between the points of support, changing its radius of curvature as it does so.
- the spherical segments need not have the sameradius of curvature or the same thickness. Differences in the stresses which must be carried by the various segments may be adjusted by varying the thickness and holding the radius of curvature constant, or by varying the radius of curva-
- a pressure vessel for storing liquids at extremely high or low temperatures comprising an outer shell in the form of a polyhedron of carbon steel, diagonal insulating supports extending inwardly from the edges of said polyhedron to the intersections of spherical segments equal in number to the faces of the polyhedron and arranged symmetrically with respect to the sides thereof, the spherical segments being composed of a metal capable of retaining a substantial part of its strength at extreme temperatures, and forming a fluid-tight shell.
- a pressure vessel for storing liquids at extremely high or low temperatures comprising: an outer shell in the form of a regular polyhedron; an inner shell made up of. a plurality of spherical segments, said spherical segments being composed of a metal capable of retaining a substantial part of its strength at extreme temperatures and said spherical segments intersecting in lines lying in the plane of the diagonals of said outer shell, and a plurality of insulating su ports disposed only along said intersections,
- said insulating supports transmitting to the outer inner shell comprises six spherical segments and t the outer shell is made up of six correspondingly disposed equal plane sides forming a cube.
- a vessel as set forth in claim 4 in which the outer shell is in the form of a regular dodecahedron and each face of the dodacahedron is subtended by one spherical segment.
Description
Feb. 22, 1949.
H. C BOARDMAN 1 PRESSURE VESSEL FOR STORAGE 0F LIQUIDS AT ABNORMALLY HIGH 0R LOW TEMPERATURES 4 Sheets-Sheet 1 Filed Oct. 9, 1944 I 1949- H; (2. BOARDMAN PRESSURE VESSEL FOR STORAGE 0F LIQUIDS AT ABNORMALLY HIGI'IOR LOW TEMPERATURES Filed Oct. 9, 1944 4 Sheets-Sheet 2 G aara 2% Feb. 22, 1949. H. c BOARDMAN 2,462,064
- PRESSURE VESSEL FOR STORAGE OF LIQUIDS I AT ABNORMALLY HIGH OR LOW TEMPERATURES Filed 001.- 9, 1944 4 Sheets-Sheet 4 arr 67,5047" mar;
Patented Feb. 22, 1949 sures QFFlQE PRESSURE VESSEL FOR STORAGE OF LIQUIDS AT ABNORMALLY EEGH R LOW TEMPERATURES Harry G. Boardman, Chicago, 111., assignor to Chi. cago Bridge & Iron Company, a corporation of Illinois This invention relates to a pressure vessel for the storage of liquids at abnormally high or low temperatures.
The present'invention is particularly adapted for the storage of liquids at low temperaturesand high pressures. It may also be used for the storage of hot liquids at high pressure. The ordinary carbon steel loses a great deal of its impact strength at very low or very high temperatures. For example, at temperatures suitable for the storage of liquefied hydrocarbons it is desirable to employ Monel metal or other high nickel alloys. In accordance with the present invention, a relatively thin inner shell member of temperature-resistant metal, such as Monel metal may be employed in the form of a fluid-tight shell of intersecting spherical segments. The outward stresses of these segments are transmitted along the lines of intersection to insulating supports of non-metallic material such as Marinite to an outer shell which is preferably fluid-tight and is preferably in the form of a regular polyhedron. This outer shell may be made of common carbon steel.
The invention is illustrated in the drawings, in which Fig. 1 is a plan view of one form of the improved tank; Fig. 2 is a vertical section taken along the line 2-2 in Fig. 1'; Fig. 3 is a section taken along the line 3-3 in Fig. 1; Fig. 4 is a perspective view of the outside of the inner shell; Fig. 5 is a plan view of a modified form of the invention; and F g. 6 is a section taken along the line 6-5 in Fig. 5.
In the form of the invention shown in Figs. 1 to 4, the spherical segments in intersect along the lines II which all fall in the planes of the diagonals of the cubical outer shell l2. The radially outward components of the stresses of the spherical segments are carried by. non-metallic insulating supporting members I3 which extend to theedg'es of the cube [2. The cube I2 is made up of welded plates of ordinary carbon steel. The space 84 between the inner and outer shells is preferably evacuated in any suitable manner. Liquid may be introduced to and withdrawn from the inner shell in the usual manner by any pipe (not shown). The foundations for the vessel are not part of the present invention and accordingly are not shown. It will be observed that the apex I5 of each circular segment lies on the perpendicular from the center of the adjoining side l6 of the cube, and that planes connecting the adjacent corners of the intersections would form an inscribed cube.
In the form shown in Figures 5 and 6, the exterior shell 12a is dodecahedral in shape, and the intersecting spherical segments Illa are twelve in number, the center of each segment again, however, being located on a perpendicular beneath the center of each side. The spherical segments are supported along the lines of intersection Ha by the Marinite supports I311. which extend in each. case to, and only to. an edge of the outer dodecahedral shell.
The thin inner shell is free to expand and contract between the points of support, changing its radius of curvature as it does so.
The spherical segments need not have the sameradius of curvature or the same thickness. Differences in the stresses which must be carried by the various segments may be adjusted by varying the thickness and holding the radius of curvature constant, or by varying the radius of curva- The foregoing detailed description has been given for clearness of understanding only, and no unnecessary limitations should be understood therefrom.
What I claim as new, and desire to secure by Letters Patent, is: l
1. A pressure vessel for storing liquids at extremely high or low temperatures comprising an outer shell in the form of a polyhedron of carbon steel, diagonal insulating supports extending inwardly from the edges of said polyhedron to the intersections of spherical segments equal in number to the faces of the polyhedron and arranged symmetrically with respect to the sides thereof, the spherical segments being composed of a metal capable of retaining a substantial part of its strength at extreme temperatures, and forming a fluid-tight shell.
2. A vessel as set forth in claim 1, in which the polyhedron is a cube. I
3. A vessel as set forth in clainr-l, in which the polyhedron is a dodecahedron.
4. A pressure vessel for storing liquids at extremely high or low temperatures comprising: an outer shell in the form of a regular polyhedron; an inner shell made up of. a plurality of spherical segments, said spherical segments being composed of a metal capable of retaining a substantial part of its strength at extreme temperatures and said spherical segments intersecting in lines lying in the plane of the diagonals of said outer shell, and a plurality of insulating su ports disposed only along said intersections,
said insulating supports transmitting to the outer inner shell comprises six spherical segments and t the outer shell is made up of six correspondingly disposed equal plane sides forming a cube.
8. A vessel as set forth in claim 4 in which the outer shell is in the form of a regular dodecahedron and each face of the dodacahedron is subtended by one spherical segment.
HARRY C. BOARDMAN.
REFERENCES CITED The following references are of record in the flle of this patent:
UNITED STATES PATENTS Number Number Name Date Place Mar. 31, 1908 Salmon Dec. 27, 1927 Williams May 1, 1928 Zenner Feb. 20, 1934 Cornelius July 29, 1941 I Hansen Sept. 23, 1941 Jackson et a1 Sept. 21, 1943 Jackson et al Feb. 8, 1944 Morrow i. Mar. 13, 1945 FOREIGN PATENTS Country Date France 15, 1933
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US557842A US2462064A (en) | 1944-10-09 | 1944-10-09 | Pressure vessel for storage of liquids at abnormally high or low temperatures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US557842A US2462064A (en) | 1944-10-09 | 1944-10-09 | Pressure vessel for storage of liquids at abnormally high or low temperatures |
Publications (1)
Publication Number | Publication Date |
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US2462064A true US2462064A (en) | 1949-02-15 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US557842A Expired - Lifetime US2462064A (en) | 1944-10-09 | 1944-10-09 | Pressure vessel for storage of liquids at abnormally high or low temperatures |
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US (1) | US2462064A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2557990A (en) * | 1946-08-09 | 1951-06-26 | Chicago Bridge & Iron Co | Vessel for external pressure |
US4343409A (en) * | 1979-10-22 | 1982-08-10 | Ford Motor Company | Large high temperature plastic vacuum reservoir |
US4615452A (en) * | 1984-07-03 | 1986-10-07 | The Boeing Company | Compound toroidal tanks |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US883479A (en) * | 1908-03-31 | American Air Liquefying Co | Insulated container for liquid air, &c. | |
US1654016A (en) * | 1925-11-20 | 1927-12-27 | Rene L Salmon | Large-sized reservoir for liquids |
US1668179A (en) * | 1926-07-15 | 1928-05-01 | Arthur H T Williams | Container |
FR750066A (en) * | 1932-04-26 | 1933-08-03 | Forges Ateliers Const Electr | Underground metal tank |
US1948477A (en) * | 1932-09-23 | 1934-02-20 | Linde Air Prod Co | Lined container |
US2250749A (en) * | 1939-04-06 | 1941-07-29 | Richard T Cornelius | Barrel |
US2256673A (en) * | 1939-08-19 | 1941-09-23 | Linde Air Prod Co | Support for double-walled containers |
US2329765A (en) * | 1941-11-12 | 1943-09-21 | James O Jackson | Low temperature storage tank |
US2341044A (en) * | 1941-07-28 | 1944-02-08 | Pittsburgh Des Moines Company | Intersecting spherical pressure tank |
US2371347A (en) * | 1942-08-22 | 1945-03-13 | Hotstream Heater Co | Jacket for water heaters |
-
1944
- 1944-10-09 US US557842A patent/US2462064A/en not_active Expired - Lifetime
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US883479A (en) * | 1908-03-31 | American Air Liquefying Co | Insulated container for liquid air, &c. | |
US1654016A (en) * | 1925-11-20 | 1927-12-27 | Rene L Salmon | Large-sized reservoir for liquids |
US1668179A (en) * | 1926-07-15 | 1928-05-01 | Arthur H T Williams | Container |
FR750066A (en) * | 1932-04-26 | 1933-08-03 | Forges Ateliers Const Electr | Underground metal tank |
US1948477A (en) * | 1932-09-23 | 1934-02-20 | Linde Air Prod Co | Lined container |
US2250749A (en) * | 1939-04-06 | 1941-07-29 | Richard T Cornelius | Barrel |
US2256673A (en) * | 1939-08-19 | 1941-09-23 | Linde Air Prod Co | Support for double-walled containers |
US2341044A (en) * | 1941-07-28 | 1944-02-08 | Pittsburgh Des Moines Company | Intersecting spherical pressure tank |
US2329765A (en) * | 1941-11-12 | 1943-09-21 | James O Jackson | Low temperature storage tank |
US2371347A (en) * | 1942-08-22 | 1945-03-13 | Hotstream Heater Co | Jacket for water heaters |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2557990A (en) * | 1946-08-09 | 1951-06-26 | Chicago Bridge & Iron Co | Vessel for external pressure |
US4343409A (en) * | 1979-10-22 | 1982-08-10 | Ford Motor Company | Large high temperature plastic vacuum reservoir |
US4615452A (en) * | 1984-07-03 | 1986-10-07 | The Boeing Company | Compound toroidal tanks |
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