US1966241A - Electrically welded high pressure gas container - Google Patents
Electrically welded high pressure gas container Download PDFInfo
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- US1966241A US1966241A US421012A US42101230A US1966241A US 1966241 A US1966241 A US 1966241A US 421012 A US421012 A US 421012A US 42101230 A US42101230 A US 42101230A US 1966241 A US1966241 A US 1966241A
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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
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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
- F17C2201/0128—Shape spherical or elliptical
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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
- F17C2201/05—Size
- F17C2201/054—Size medium (>1 m3)
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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
- F17C2203/0614—Single wall
- F17C2203/0617—Single wall with one layer
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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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0308—Protective caps
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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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
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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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0335—Check-valves or non-return valves
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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
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0388—Arrangement of valves, regulators, filters
- F17C2205/0394—Arrangement of valves, regulators, filters in direct contact with the pressure vessel
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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
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/228—Assembling processes by screws, bolts or rivets
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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
- F17C2209/23—Manufacturing of particular parts or at special locations
- F17C2209/232—Manufacturing of particular parts or at special locations of 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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/016—Noble gases (Ar, Kr, Xe)
- F17C2221/017—Helium
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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
- F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
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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
- F17C2223/036—Very high pressure (>80 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
- F17C2260/012—Reducing weight
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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
- F17C2260/04—Reducing risks and environmental impact
- F17C2260/042—Reducing risk of explosion
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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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
- F17C2270/0171—Trucks
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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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
- F17C2270/0173—Railways
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- 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
- Y10S220/29—Welded seam
Definitions
- This invention relates to an electrically welded ever, the great wall thickness required in the high pressure gas container.
- cylindrical, shaped vessels in order to withstand The container is particularly adapted for the the high pressures employed makes the use of transportation, under high pressures, of relatively such forged vessels expensive and almost pro- 5 light gases such as helium, as set forth in my hibi'tive in the case of transporting light gases,
- the object of the invention is to provide a con-
- the present invention adapts the spherical tainer which will withstand the high pressures tank construction to the transportation of required more safely. helium under high pressure and thereby provides 10
- Another object is to provide a high pressure gas an economical and safe transportation for this container which has a greater capacity per unit and other valuable gases.
- the invention of weight of metal, giving consideration to the incourse may be employed in the transportation creased capacity due togreater gas pressures of other gases and for other purposes. employed, and which is simple in construction In the manufacture of the container, two flat 15 and more economical to manufacture.
- the container is an that of the minimum required thickness of the integral metal sphere formed from two hemivessel, for example, one and one-half inches, are spheres welded together at their meeting cirspun or otherwise pressed into complemental hemcumferential edges, the hemispheres having a ispherical shape.
- the hemispheres 1 and 2 thus the centers or common axis to the outer periphof -the'original plate at their centers and a graderal welded edges of the hemispheres.
- FIG. 1 is a perspective view of a container and one-half inches in thickness at their centers, embodying the invention.
- marked A in the drawing, Fig. 2, and approxi- Fig. 2 is a vertical central section through the mettle about two inches in thickness at the pecontainer. rip eral edges thereof, marked B in Fig. 2.
- This 30 Fig. 3 is an enlarged detail transverse section al increase in thickness y be readily th parts arranged for welding, tained in the spinning or pressingoperation.
- Fig. 4 is a similar section showing the finished h
- the container is substantially spherical and Slight angular relationship.
- the container is particularly adapted to the forms the base of the welding groove and provides Star e and trans ortation of n ht as'es such a groove of greater depth than the wall thickness fi d p 1 1 i g of the hemispheres.
- the containers are approximately locating lugs may be secured to the interior zfi fi n in diameteltand have mlglmum K 1 face in any suitable manner such as by spot weldic ess approxima ing one an onea ing. inches.
- the edges are welded toportation of gases have been forged from a single gether preferably by electric arc welding. wherein 55 steel ingot into cylindrical shaped vessels. Howa fusible electrode is employed.
- the electrode is preferably of a composition such that the weld metal deposited has substantially the same composition as that of the hemispheres.
- the welding metal is deposited in layers and the first layer penetrates into the backing or chill ring and integra1lyunites the same with the edges being welded.
- the subsequent layers are interfused and substantially fill the welding groove 6.
- the weld thus produced is substantially 25 to 30% thicker than the required minimum thickness of the vessel and thereby provides a greater margin of safety.
- the container is provided with a valve controlled inlet and outlet 8, as shown in Fig. 5.
- the control valve comprises a cap 9 bolted to the sphere and. having a screw plug 10.
- the screw plug 10 has a conical valve seat l l, and a central passage 12 for receiving the valve 13 and valve stem 14.
- the valve stem 14 is threaded into the plug 10 and is provided with'a squared head 15 at its outer end.
- a cover 16 normally encloses the outer end of the valve stem 14. During charging or discharging of the fluid contents of the sphere, the cover 16 is removed and apipe connection having a valve control mechanism, which engages the head 15 of the valve stem, is secured to the plug 10.
- a high pressure storage tank comprising two thick walled hemispherical shells, the walls of the shells being of a predetermined thickness at the apexes suflicient to stand the maximum pressure to be applied and gradually increasing in thickness from the apexes to the bases, a weld uniting the thick edges of the" bases of the hemisphericalshells to form a spherical tank, one of said shells having an opening at the apex, and a safety valve mounted in said opening.
- a high pressure storage tank comprising two thick walled hemisphericalshells, the walls of the shells being of a predetermined thickness at the ape res suilicient to stand the maximum pressure to be applied and gradually increasing in thickness from the apexes to the bases, a weld uniting the thick edges of the bases of the hemispherical shells to form a spherical container, and a boss formed on one of the shells, said boss having an opening therethrough leading to the interior of the container and a valve mounted in said opening and attached to said boss.
- -A high pressure storage tank comprising two thick walled hemispherical shells, the walls of'the shells being of a predetermined thickness at the 'apexes sufilcient to 'standthe maximum 11 pressureto-be applied and gradually increasing in thickness from the apexes to the bases and a weld uniting the thick edges of the bases of the hemispherical shells, a boss formed on one of the shells,- the boss having a threaded opening 1.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
July 10, 1934.
R. FURRER Filed Jan. 15, 1930 ELECTRICALLY WELDED HIGH PRESSURE GAS CONTAINER INVENTOR. Rudolph Furrer ATTORNEY.
wall thickness which gradually increases from formed have a wall thickness approximating that 7 mama July 10, 1934 Q I Q 1,966,241
UNITED STATES PATENT OFFICE ELECTRICALLY WELDED HIGH PRESSUR GAS CONTAINER Rudolph Furrer, Wauwatosa, Wis., assignor to A. 0. Smith Corporation, Milwaukee, Wis., a corporation of New York Application January 15, 1930, Serial No. 421,012 5 Claims. (Cl. 220-3) This invention relates to an electrically welded ever, the great wall thickness required in the high pressure gas container. cylindrical, shaped vessels in order to withstand The container is particularly adapted for the the high pressures employed makes the use of transportation, under high pressures, of relatively such forged vessels expensive and almost pro- 5 light gases such as helium, as set forth in my hibi'tive in the case of transporting light gases,
copending application, Serial No. 374,713 such as helium.
The object of the invention is to provide a con- The present invention adapts the spherical tainer which will withstand the high pressures tank construction to the transportation of required more safely. helium under high pressure and thereby provides 10 Another object is to provide a high pressure gas an economical and safe transportation for this container which has a greater capacity per unit and other valuable gases. The invention of weight of metal, giving consideration to the incourse may be employed in the transportation creased capacity due togreater gas pressures of other gases and for other purposes. employed, and which is simple in construction In the manufacture of the container, two flat 15 and more economical to manufacture. plates of metal having a thickness approximating According to the invention, the container is an that of the minimum required thickness of the integral metal sphere formed from two hemivessel, for example, one and one-half inches, are spheres welded together at their meeting cirspun or otherwise pressed into complemental hemcumferential edges, the hemispheres having a ispherical shape. The hemispheres 1 and 2 thus the centers or common axis to the outer periphof -the'original plate at their centers and a graderal welded edges of the hemispheres. ualy iiicrelasinihwallfthi tl llrlness Itlowards title pe- The invention may be more readily understood p e a 9 88 e e 115 W ere & D 8 pin its various features by reference to the accom- DrOXimflting O a O e-half inches in thickness 25 panying drawing in which: I is employed, the hemispheres approximate one Figure 1 is a perspective view of a container and one-half inches in thickness at their centers, embodying the invention. marked A in the drawing, Fig. 2, and approxi- Fig. 2 is a vertical central section through the mettle about two inches in thickness at the pecontainer. rip eral edges thereof, marked B in Fig. 2. This 30 Fig. 3 is an enlarged detail transverse section al increase in thickness y be readily th parts arranged for welding, tained in the spinning or pressingoperation.
Fig. 4 is a similar section showing the finished h The lfl 31 E 51 g 4 0f l a p i r l i eld, I emisp eres are en m e or p ane so a Fig. 5 is an enlargedsection of the valve d when the hemispheres are arranged in assembled 35 connections for the container. relation, as shown in Fig. 3, the edges will bein The container is substantially spherical and Slight angular relationship. is preferably constructed of a high tensile tfi' g gh ii p gres g1: assembled 1: sulcli mannelr .stren th steel, such as chrome vanadium alloy ee ges an new space re 1011 an steel, which will provide a more economical togelfher with a Chill backing ring a, form a 40 manufacture, having consideration for the re- T backlng {mg 5 1s preferquired strength, capacity and weight of the tank. ably provided wlth clrcumferentla'l groove wlimh The container is particularly adapted to the forms the base of the welding groove and provides Star e and trans ortation of n ht as'es such a groove of greater depth than the wall thickness fi d p 1 1 i g of the hemispheres. In order to properly posi as 8 un er re W Y 1g tnessures as tion the chill ring 5 within the sphere and space zooo or more pounds per Square when the edges of the two hemispheres uniformly, it Fonstructed for use on tafnk as a has been found desirable to provide locating lugs Illustrated m my COPePdmg, evpllcetlon above 7 on the interior surface of the hemispheres. The referred to, the containers are approximately locating lugs may be secured to the interior zfi fi n in diameteltand have mlglmum K 1 face in any suitable manner such as by spot weldic ess approxima ing one an onea ing. inches. After assembling the hemispheres in the man-- Heretofore. containers for high pressure transner above indicated, the edges are welded toportation of gases have been forged from a single gether preferably by electric arc welding. wherein 55 steel ingot into cylindrical shaped vessels. Howa fusible electrode is employed. The electrode is preferably of a composition such that the weld metal deposited has substantially the same composition as that of the hemispheres.
The welding metal is deposited in layers and the first layer penetrates into the backing or chill ring and integra1lyunites the same with the edges being welded. The subsequent layers are interfused and substantially fill the welding groove 6. The weld thus produced is substantially 25 to 30% thicker than the required minimum thickness of the vessel and thereby provides a greater margin of safety.
The gradual increase in wall thickness of the hemispheres from the center or pole towards the welded edges and from the minimum required thickness of the vessel to the thickness of theweld-provides a more uniform stress condition in the container than would be the case were theweld metal substantially thicker than the r'netal of the edges of the hemispheres. This is particularly important in the use of these spherical containers on tank cars, such as that shown in my above mentioned copending application, for railway transportation, as it is essential to provide a container having greater safety in case of railway wrecks. On the other hand, it is important from the standpoint of economical transportation of helium to provide a container which has a minimum weight per unit capacity.
The container is provided with a valve controlled inlet and outlet 8, as shown in Fig. 5. The control valve comprises a cap 9 bolted to the sphere and. having a screw plug 10. The screw plug 10 has a conical valve seat l l, and a central passage 12 for receiving the valve 13 and valve stem 14. The valve stem 14 is threaded into the plug 10 and is provided with'a squared head 15 at its outer end.
A cover 16 normally encloses the outer end of the valve stem 14. During charging or discharging of the fluid contents of the sphere, the cover 16 is removed and apipe connection having a valve control mechanism, which engages the head 15 of the valve stem, is secured to the plug 10.
The valve 13 has a central pin 17 projecting inwardly therefrom for the purpose of engaging and opening a ball check valve 18 at the time the control valve 13 is opened. This check valve 18 is located in a plug 19 secured in the spherical tank wall and serves as a safety valve in case of injury to the outer control valve mechanism. Thus in a railway wreck the outer control valve mechanism may be entirely broken away from the sphere without allowing, the escape of the valuable fluid contents of the sphere, due to the check valve 15 which functions independently of the outer valve to seal the tank outlet.
Variousmodifications of the invention may be -maximum pressure to be applied and gradually employed within the scope of the following claims.
increasing in thickness from the apexes tothe bases, and a weld uniting the thick edges of the bases of. the hemispherical'shells to form a spherical tank.
1}. A high pressure storage tank comprising two thick walled hemispherical shells, the walls of the shells being of a predetermined thickness at the apexes suflicient to stand the maximum pressure to be applied and gradually increasing in thickness from the apexes to the bases, a weld uniting the thick edges of the" bases of the hemisphericalshells to form a spherical tank, one of said shells having an opening at the apex, and a safety valve mounted in said opening.
4. A high pressure storage tank comprising two thick walled hemisphericalshells, the walls of the shells being of a predetermined thickness at the ape res suilicient to stand the maximum pressure to be applied and gradually increasing in thickness from the apexes to the bases, a weld uniting the thick edges of the bases of the hemispherical shells to form a spherical container, and a boss formed on one of the shells, said boss having an opening therethrough leading to the interior of the container and a valve mounted in said opening and attached to said boss.
5. -A high pressure storage tank comprising two thick walled hemispherical shells, the walls of'the shells being of a predetermined thickness at the 'apexes sufilcient to 'standthe maximum 11 pressureto-be applied and gradually increasing in thickness from the apexes to the bases and a weld uniting the thick edges of the bases of the hemispherical shells, a boss formed on one of the shells,- the boss having a threaded opening 1. 5 extending therethrough to the interior of the container, and threaded holes extending into it at a distance from said opening, a valve threaded into said opening, and studs engaged in said threaded holes cooperative to'retain the valve in a position in the threaded opening. j
RUDOLPH
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US421012A US1966241A (en) | 1930-01-15 | 1930-01-15 | Electrically welded high pressure gas container |
Applications Claiming Priority (1)
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US421012A US1966241A (en) | 1930-01-15 | 1930-01-15 | Electrically welded high pressure gas container |
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US1966241A true US1966241A (en) | 1934-07-10 |
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US421012A Expired - Lifetime US1966241A (en) | 1930-01-15 | 1930-01-15 | Electrically welded high pressure gas container |
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Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE748096C (en) * | 1937-07-21 | 1944-10-26 | Ball stick bottle | |
US2489903A (en) * | 1946-01-21 | 1949-11-29 | Lummus Co | Flash chamber |
US2596233A (en) * | 1946-04-06 | 1952-05-13 | Bell & Gossett Co | Pressure vessel |
US2609964A (en) * | 1947-04-04 | 1952-09-09 | American Pipe & Steel Corp | Recess mounting for valves and fittings for liquefied petroleum gas containers |
US2630942A (en) * | 1948-03-24 | 1953-03-10 | John E Shaffer | Home rechargeable liquid wax insecticide and fire-fighting bomb |
US2637521A (en) * | 1949-03-01 | 1953-05-05 | Elliott Co | Gas turbine rotor and method of welding rotor disks together |
US2657564A (en) * | 1949-03-17 | 1953-11-03 | George C Graham | Washing machine having flexible extractor and automatic control |
US2684170A (en) * | 1950-12-11 | 1954-07-20 | Smith Corp A O | Noncorrosive welded tank joint |
US2809762A (en) * | 1953-09-25 | 1957-10-15 | Fairchild Engine & Airplane | Pressure vessel |
US2827195A (en) * | 1954-07-07 | 1958-03-18 | Thomas F Kearns | Container for high pressure fluids |
US2859892A (en) * | 1954-02-09 | 1958-11-11 | Specialties Dev Corp | Spherical container |
US2952378A (en) * | 1956-06-25 | 1960-09-13 | Leonard C Renslow | Capsule or gondola used in high altitude research |
US3166837A (en) * | 1961-08-10 | 1965-01-26 | Metal Specialty Company | Method and apparatus for making domelike hollow metal structure |
US3945236A (en) * | 1974-10-03 | 1976-03-23 | C-R-O Engineering Co., Inc. | Formation of segments for containers and the like |
US4304038A (en) * | 1977-09-26 | 1981-12-08 | Nippon Aluminium Mfg. Co., Ltd. | Method of manufacturing small-sized pressure vessel of sheet metal |
EP0042887A1 (en) * | 1980-06-27 | 1982-01-06 | Tank- en Apparatenbouw DE BLESSE B.V. | Gas tank, particularly a liquid petroleum gas LPG-tank for a vehicle |
US5046638A (en) * | 1990-03-22 | 1991-09-10 | Fluoroware, Inc. | Seamless pressure vessel with recessed indentation |
US20110284562A1 (en) * | 2010-04-29 | 2011-11-24 | Pavel Novak | Pressure container |
US20110315692A1 (en) * | 2009-03-11 | 2011-12-29 | Lennart Svensson | Pressure Vessel For a High Pressure Press |
US10449633B1 (en) * | 2019-03-13 | 2019-10-22 | Dalian University Of Technology | Gas pressure forming method of ellipsoidal shells based on current self-resistance heating |
-
1930
- 1930-01-15 US US421012A patent/US1966241A/en not_active Expired - Lifetime
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE748096C (en) * | 1937-07-21 | 1944-10-26 | Ball stick bottle | |
US2489903A (en) * | 1946-01-21 | 1949-11-29 | Lummus Co | Flash chamber |
US2596233A (en) * | 1946-04-06 | 1952-05-13 | Bell & Gossett Co | Pressure vessel |
US2609964A (en) * | 1947-04-04 | 1952-09-09 | American Pipe & Steel Corp | Recess mounting for valves and fittings for liquefied petroleum gas containers |
US2630942A (en) * | 1948-03-24 | 1953-03-10 | John E Shaffer | Home rechargeable liquid wax insecticide and fire-fighting bomb |
US2637521A (en) * | 1949-03-01 | 1953-05-05 | Elliott Co | Gas turbine rotor and method of welding rotor disks together |
US2657564A (en) * | 1949-03-17 | 1953-11-03 | George C Graham | Washing machine having flexible extractor and automatic control |
US2684170A (en) * | 1950-12-11 | 1954-07-20 | Smith Corp A O | Noncorrosive welded tank joint |
US2809762A (en) * | 1953-09-25 | 1957-10-15 | Fairchild Engine & Airplane | Pressure vessel |
US2859892A (en) * | 1954-02-09 | 1958-11-11 | Specialties Dev Corp | Spherical container |
US2827195A (en) * | 1954-07-07 | 1958-03-18 | Thomas F Kearns | Container for high pressure fluids |
US2952378A (en) * | 1956-06-25 | 1960-09-13 | Leonard C Renslow | Capsule or gondola used in high altitude research |
US3166837A (en) * | 1961-08-10 | 1965-01-26 | Metal Specialty Company | Method and apparatus for making domelike hollow metal structure |
US3945236A (en) * | 1974-10-03 | 1976-03-23 | C-R-O Engineering Co., Inc. | Formation of segments for containers and the like |
US4304038A (en) * | 1977-09-26 | 1981-12-08 | Nippon Aluminium Mfg. Co., Ltd. | Method of manufacturing small-sized pressure vessel of sheet metal |
EP0042887A1 (en) * | 1980-06-27 | 1982-01-06 | Tank- en Apparatenbouw DE BLESSE B.V. | Gas tank, particularly a liquid petroleum gas LPG-tank for a vehicle |
US5046638A (en) * | 1990-03-22 | 1991-09-10 | Fluoroware, Inc. | Seamless pressure vessel with recessed indentation |
US20110315692A1 (en) * | 2009-03-11 | 2011-12-29 | Lennart Svensson | Pressure Vessel For a High Pressure Press |
US8893909B2 (en) * | 2009-03-11 | 2014-11-25 | Avure Technologies Ab | Pressure vessel for a high pressure press |
US20110284562A1 (en) * | 2010-04-29 | 2011-11-24 | Pavel Novak | Pressure container |
US8640910B2 (en) * | 2010-04-29 | 2014-02-04 | Magna Steyr Fahrzeugtechnik Ag & Co Kg | Pressure container |
US10449633B1 (en) * | 2019-03-13 | 2019-10-22 | Dalian University Of Technology | Gas pressure forming method of ellipsoidal shells based on current self-resistance heating |
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