US2344856A - Means for reinforcing hollow containers for gases under pressure - Google Patents
Means for reinforcing hollow containers for gases under pressure Download PDFInfo
- Publication number
- US2344856A US2344856A US449384A US44938442A US2344856A US 2344856 A US2344856 A US 2344856A US 449384 A US449384 A US 449384A US 44938442 A US44938442 A US 44938442A US 2344856 A US2344856 A US 2344856A
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- Prior art keywords
- bands
- receptacle
- band
- indentation
- indented
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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
- F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
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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
- F17C2201/0104—Shape cylindrical
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
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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
- F17C2201/0104—Shape cylindrical
- F17C2201/0123—Shape cylindrical with variable thickness or diameter
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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
- F17C2201/056—Small (<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
- F17C2203/01—Reinforcing or suspension means
- F17C2203/011—Reinforcing means
- F17C2203/012—Reinforcing means on or in the wall, e.g. ribs
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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
- F17C2203/0643—Stainless 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
- 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
- F17C2221/01—Pure fluids
- F17C2221/011—Oxygen
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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
- F17C2221/012—Hydrogen
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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
- F17C2221/014—Nitrogen
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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
- F17C2221/031—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
- 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
- F17C2223/035—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
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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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0186—Applications for fluid transport or storage in the air or in space
- F17C2270/0189—Planes
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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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/32—Hydrogen storage
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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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49863—Assembling or joining with prestressing of part
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49863—Assembling or joining with prestressing of part
- Y10T29/49874—Prestressing rod, filament or strand
Definitions
- This invention relates to the reinforcing of hollow metallic articles and more specifically to means for reinforcing hollow metallic containers for gases under high pressure.
- a bullet piercing the side of the tank causes the metal of the container to shatter causing immediate danger to the personnel from flying particle's.
- Variou arrangements for reinforcing these tanks or containers have been suggested.
- One of these makes use of a plurality of circumferential steel bands contained in grooves extendin completely around the container and crossedover by longitudinal hands. This does not solve the problem,
- this object is attained by providing a first group of metallic bands each being in contact with the outer surface of the container and a second group of bands also in contact with the outer surface of the container over substantially all of the length of each band, the bands of the second group crossing those of the first group at an angle which is preferably a right angle.
- the bands of one of the groups are indented at intervals to under pass the bands of the second of the groups.
- a casing to enclose gases under pressure comprising a metallic cylinder having two end cups fastened thereto, as by butt welding, and two groups of crossed bands for strengthening or reinforcing the casing.
- the bands of the first group are each indented at intervals to nest into indentations at corresponding intervals in the surface of the cylinder.
- the bands of the second group are placed so that they cross the bands of the first group at the indented portions thereof, the indented portions of the cylinder occurring at regular intervals so as to permit this.
- the bands are preferably welded, soldered or annealed together at the crossover points and to the cylinder at other points for added strength.
- each longitudinal band is in contact with the casing throughout the full length of the band and each circumferential band is in contact with the casing throughout its full length except for the places where it crosses the longitudinal bands.
- both of the groups of bands are crossed in a spiral around the cylinder and the bands of one group cross those of the other at the indented portions of the cylinder, the construction being otherwise similar to the preferred arrangement.
- the hemispherical ends are also held to the cylinder in either case by welding the bands to the hemispherical ends.
- the ends may be of other shapes without affecting the scope of the invention.
- the hemispherical ends may be indented or not as desired.
- Fig. 1 is a longitudinal view of a casing member for high Pressure gases reinforced in accord ance.with this invention
- Fig. 2 is an end view of the casing shown in Fig.
- Fig. 3 is a cross-sectional view taken in a plane indicated by the line 33 in Fig. 1;
- Fig. 4 is a cross-sectional view taken in a plane indicated by the line H in Fig. 1;
- Fig. 5 is an enlarged partial cross-sectional view taken in a plane indicated by the line 5-5 in Fi 1-;
- Fig. 6 is an enlarged view, with portions broken Igtwag's, of a portion of the casing and two crossed
- Fig. 1 is a longitudinal view of a specific embodiment of the invention showing, by way of example, a casing member for high pressure gases reinforced in accordance with the invention.
- Fig. 2 is an end view of the casing while Fig. 3 is a cross-sectional view taken in a plane transverse to the longitudinal axis.
- the casing comprises a cylindrical member ll of astrong metal such as 24 gauge stainless steel and two end members l2 and I3, shown, for example, as hemispherical cups, which also may be of steel.
- the cups l2 and l3 are attached to the member II by any suitable means such as by butt-*welding.
- the seams are indicated by the reference characters l9 and 20.
- a plug H is fitted in the end I2 to permit the entrance and egress of gas under pressure.
- bands l5, l8, l1 and I8 Fastened to the cylinder II and the ends I2 I and I3 by any suitable means, such as by welding, are longitudinal bands l5, l8, l1 and I8. While four longitudinal bands have been shown, more or less than this number may be provided, if desired. Bands l and I! may comprise one continuous band passing around the end l3 or may be two bands, each attached to the end I! as well as to the end l2 and the cylindrical portion ll.
- circumferential bands 2!, 22, 23, 24 and 25 are circumferential bands 2!, 22, 23, 24 and 25.
- Fig. 4 which is a cross-sectional view taken in a plane transverse to the longitudinal axis of the tube through theband 23
- each of the circumferential bands is ring shaped, the outer and inner surfaces intersecting the plane of the drawing in perfect circles.
- the inner diameter of the circumferential band 23 is substantially the same as the outer diameter of the cylinder II.
- the circumferential bands can keep their cirpular shape (or elliptical, if the cylinder II has an elliptical cross-section) and at the same time cross the longitudinal bands and still make contact throughout substantially their entire length because of the indentations in the cylinder ll under each of the crossover points of the longitudinal and circumferential bands.
- One such indentation (under the crossov.er" of the bands l1 and 25) is indicated by the reference character 26 in Figs. 5 and 6.
- Fig. 5 is an enlarged partial cross-sectional view taken through the longitudinal band l1 and the longitudinal axis of the cylinder l I while Fig.
- FIG. 6 is a fragmentary view, with portions broken away, of a portion of the wall of the cylinder I l and adjacent the crossover of the bands I! and 25.
- the indentation 213 (and the others like it) is only slightly larger than an area which has for its dimensions the width of a longitudinal band and the width of a circumferential band.
- the depth of the indentation 26 is substantially the same as the thickness of one of the longi tudinal bands.
- the longitudinal and circumferential bands cross each other at right angles.
- the longitudinal bands, at the portions thereof over the indentations in the wall of the cylinder II are also indented to nest into these indentations.
- the circumferential-bands thus pass over the indentations in the longitudinal bands and still maintain their circular shape and contact 'the wall of the cylinder H.
- the wall of the cylinder H may be indented as it is being made, or later, by forging or rolling or by shaping with a punch press.
- the iongitudinal bands are indented by any suitable forming means, such as by a press, and fastened in place by spot or gas welding, for example.
- the circumferential bands are formed by welding together the ends or by forging or by any other suitable means and spot or gas welded or sweated around the cylinder.
- the circumferential and longitudinal bands are preferably spot welded to each other at all cross-overs.
- casings strength is greatly reinforced because the closed circumferential bands hold the longitudinal bands in place, snug against the surface of the cylinder.
- both groups of bands may spiral around the casing, one group having indentations which nest into indentations in the cylinder wall and the other group crossing the first group over these indentations.
- the angle of intersection may then be a right angle of any other convenient angle.
- the bands may be woven over and then under other bands, in a basket weave manner, although such construction is diflicult with steel bands of an appreciable thickness.
- a hollow metal receptacle having an indentation in the outside surface thereof, a metallic band fastened to the outside of said receptacle in such a manner that it passes over said indentation, said band being indented throughout its width in the portion thereof over said indentation, and a second metallic band fastened to the outside of said receptacle in such a manner that it crosses the indented portion of said first-mentioned band, the dimension of said indentation longitudinally of said first band being substantially equal to the transverse dimension of the second band, and the surface of the receptacle surrounding the indentation being relatively smooth.
- a hollow metal receptacle having an indentation i the outside surface thereof, a metallic band fastened to the outside of said receptacle in such a manner that it passes over said indentation, said band being indented throughout its width in the portion thereof over said indentation, a second metallic band fastened to the outside of said receptacle in such a manner that it crosses the indented portion of said first-mentioned band, and means, for
- the dimension of said indentation longitudinally of said first band being substantially equal to the transverse dimension of the second band, and the surface of the receptacle surrounding the indentation being relatively smooth.
- a hollow metal receptacle for gases at high pressure a large portion at least of which is cylindrical, a first group of bands each fastened to the outside of said receptacle, and a second group of bands arranged to cross the bands of the first group, said receptacle having an indentation in the outside surface thereof under each of said crossings and each of the bands of the first group having an indentation throughout its width extending into the corresponding indentation in said receptacle, whereby each of said bands is in contact with the surface of said receptacle throughout substantially all its length, the dimension of each indentation longitudinally of .each band in the first group being substantially equal to the transverse dimension of the band in the second group at that point, and the surface of the receptacle surrounding the identation being relatively smooth.
- a hollow metal receptacle for gases under high pressure a large portion at I least of which is cylindrical, a plurality of longitudinal bands eachfastened to the outside of said receptacle, and a plurality of circumferential bands around said cylinder and crossing said longitudinal bands at substantially right angles, said receptacle having an indentation therein under each of said crossings and each of said longitudinal bands having an indentation at said crossing interfitting the longitudinal band in the corresponding indentation in said receptacle,
- each of said bands is in contact with the surface of said receptacle throughout substantially all its length.
- a hollow metal receptacle I for gases under high pressure a large portion at least of which is cylindrical, a plurality of indented bands each fastened to the outside of said receptacle, and a plurality of other bands around said cylinder and crossing said indented bands, said receptacle having an indentation therein under each of said crossings and each of said indented bands having an indentation throughout its width extending into the corresponding indentation in said receptacle, whereby each of said bands is in contact with the surface of said receptacle throughout substantially all its length.
- each of the indentations in said receptacle being of substantially the same depth as the thickness of an indented band and the dimension of each indentation longitudinally of each of said indented bands being substantially equal to the tranverse dimension of said other band at that point, and the surface of the receptacle surrounding the indentation being relatively smooth.
- each indented band to each of the dther hands it crosses, the dimension of each indentation longitudinally of each of said indented bands being substantially equal to the transverse dimension of said other band at that point, and the surface of the receptacle surrounding the indentation being relatively smooth.
- a hollow metal receptacle for gases under high pressure comprising a smooth surface cylindrical portion having a plurality of groups of aligned indentations therein, and two end portions welded to said cylindrical portion to form a gas tight container, a plurality of indented bands each of which is in contact with the surface of and is fastened to said cylindrical and end portions, each band being so positioned that it passes over a group of said indentations and is also indented so that it nests into each of the indentations in the aligned group, the indentations in each group being aligned with the indentations in the other groups.
- a hollow metal receptacle for gases under high pressure a large portion at least of which is cylindrical, a plurality of bands each fastened to the outside of said receptacle, and another band spiralled around said receptacle and crossing each of said first-mentioned bands, said receptacle having an indentation therein under each.
- each of said bands is in contact with the surfaceof said receptacle throughout substantially all its length, the dimension of each of said indentations longitudinally of said firstmentioned bands being substantially equal to the transverse dimension of the band spiralled around said receptacle and the surface of the; receptacle surrounding the indentations therein
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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
March 21, 1944. EARLE 2,344,856
MEANS FOR REINFORCING HOLLOW CONTAINERS FOR GASES UNDER PRESSURE Filed July 2, 1942 /7- I v I /8 2/ 3 LO- 22 I7 23 7 L I L 26 a z? 25 M /24 a 9 /25 /7 2O g I /20 l3 M/l E/VTOR l3 GL. C. EARLE A T TORNE V Patented Mar. 21, 1944 UNITED STATES PATENT OFFICE MEANS FOR nanwoacmo HOLLOW CON- ramsas roa GASES UNDER rasssuac Guyon L. C. Earle, Forest Hills, N. Y. Application July 2, 1942, Serial No. 449,384
9 Claims.
This invention relates to the reinforcing of hollow metallic articles and more specifically to means for reinforcing hollow metallic containers for gases under high pressure.
It has been common for years to move gases, such as compressed air, oxygen, hydrogen, and nitrogen, from place to place in hollow metal containers. These gases are customarily placed at a high pressure, frequently reaching several hundred pounds per square inch, thus requiring that the walls be of one of the heavy metals and very strong. It has been found that many situations arise where it is advisable to make the containers of lighter material and still retain even more strength in the containing means for gases under pressure than that usually provided in containers for ordinary commercial use. A specific example of one such situation is the case of a light weight container which may be subjected to the fire of bullets and other projectiles, such as an oxygen tank for a warplane. A bullet piercing the side of the tank causes the metal of the container to shatter causing immediate danger to the personnel from flying particle's.- Variou arrangements for reinforcing these tanks or containers have been suggested. One of these makes use of a plurality of circumferential steel bands contained in grooves extendin completely around the container and crossedover by longitudinal hands. This does not solve the problem,
however, as there is a weakness around the grooves which encourages tearing. While other reinforcing means have been tried none of them has been completely satisfactory.
It is accordingly the principal object of the present invention to provide novel means for reinforcing hollow metallic articles and particularly for reinforcing metallic containers for high pressure gases.
In accordance with the present invention, this object is attained by providing a first group of metallic bands each being in contact with the outer surface of the container and a second group of bands also in contact with the outer surface of the container over substantially all of the length of each band, the bands of the second group crossing those of the first group at an angle which is preferably a right angle. The bands of one of the groups are indented at intervals to under pass the bands of the second of the groups.
In a specific embodiment of the invention,
shown by way of example to illustrate the principles of novelty thereof, there is provided a casing to enclose gases under pressure comprising a metallic cylinder having two end cups fastened thereto, as by butt welding, and two groups of crossed bands for strengthening or reinforcing the casing. The bands of the first group are each indented at intervals to nest into indentations at corresponding intervals in the surface of the cylinder. The bands of the second group are placed so that they cross the bands of the first group at the indented portions thereof, the indented portions of the cylinder occurring at regular intervals so as to permit this. The bands are preferably welded, soldered or annealed together at the crossover points and to the cylinder at other points for added strength. The bands, or some of them, are also preferably welded to the ends. In a form of the invention where the indented bands are longitudinal and the crossover" bands are circumferential, each longitudinal band is in contact with the casing throughout the full length of the band and each circumferential band is in contact with the casing throughout its full length except for the places where it crosses the longitudinal bands. Thus any tear whichstarts in the casing soon reaches a band and is halted.
In a modification, both of the groups of bands are crossed in a spiral around the cylinder and the bands of one group cross those of the other at the indented portions of the cylinder, the construction being otherwise similar to the preferred arrangement.
The hemispherical ends are also held to the cylinder in either case by welding the bands to the hemispherical ends. Of course the ends may be of other shapes without affecting the scope of the invention. The hemispherical ends may be indented or not as desired.
The invention will be more readily understood by referring to the following description taken in connection with the accompanying drawing forming a part thereof, in which:
Fig. 1 is a longitudinal view of a casing member for high Pressure gases reinforced in accord ance.with this invention;
Fig. 2 is an end view of the casing shown in Fig.
Fig. 3 is a cross-sectional view taken in a plane indicated by the line 33 in Fig. 1;
Fig. 4 is a cross-sectional view taken in a plane indicated by the line H in Fig. 1;
Fig. 5 is an enlarged partial cross-sectional view taken in a plane indicated by the line 5-5 in Fi 1-; and
Fig. 6 is an enlarged view, with portions broken Igtwag's, of a portion of the casing and two crossed Referring more particularly to the drawing, Fig. 1 is a longitudinal view of a specific embodiment of the invention showing, by way of example, a casing member for high pressure gases reinforced in accordance with the invention. Fig. 2 is an end view of the casing while Fig. 3 is a cross-sectional view taken in a plane transverse to the longitudinal axis. The casing comprises a cylindrical member ll of astrong metal such as 24 gauge stainless steel and two end members l2 and I3, shown, for example, as hemispherical cups, which also may be of steel. The cups l2 and l3 are attached to the member II by any suitable means such as by butt-*welding. The seams are indicated by the reference characters l9 and 20. A plug H is fitted in the end I2 to permit the entrance and egress of gas under pressure.
Fastened to the cylinder II and the ends I2 I and I3 by any suitable means, such as by welding, are longitudinal bands l5, l8, l1 and I8. While four longitudinal bands have been shown, more or less than this number may be provided, if desired. Bands l and I! may comprise one continuous band passing around the end l3 or may be two bands, each attached to the end I! as well as to the end l2 and the cylindrical portion ll.
Around the circumference of the cylinder II at convenient points are circumferential bands 2!, 22, 23, 24 and 25. As shown in Fig. 4, which is a cross-sectional view taken in a plane transverse to the longitudinal axis of the tube through theband 23, each of the circumferential bands is ring shaped, the outer and inner surfaces intersecting the plane of the drawing in perfect circles. The inner diameter of the circumferential band 23 is substantially the same as the outer diameter of the cylinder II.
In accordance with the present invention, the circumferential bands can keep their cirpular shape (or elliptical, if the cylinder II has an elliptical cross-section) and at the same time cross the longitudinal bands and still make contact throughout substantially their entire length because of the indentations in the cylinder ll under each of the crossover points of the longitudinal and circumferential bands. One such indentation (under the crossov.er" of the bands l1 and 25) is indicated by the reference character 26 in Figs. 5 and 6. Fig. 5 is an enlarged partial cross-sectional view taken through the longitudinal band l1 and the longitudinal axis of the cylinder l I while Fig. 6 is a fragmentary view, with portions broken away, of a portion of the wall of the cylinder I l and adjacent the crossover of the bands I! and 25. As shown in these two figures, the indentation 213 (and the others like it) is only slightly larger than an area which has for its dimensions the width of a longitudinal band and the width of a circumferential band. The depth of the indentation 26 is substantially the same as the thickness of one of the longi tudinal bands. As shown in Figs. 1 and 6, the longitudinal and circumferential bands cross each other at right angles. The longitudinal bands, at the portions thereof over the indentations in the wall of the cylinder II are also indented to nest into these indentations. The circumferential-bands thus pass over the indentations in the longitudinal bands and still maintain their circular shape and contact 'the wall of the cylinder H.
The wall of the cylinder H may be indented as it is being made, or later, by forging or rolling or by shaping with a punch press. The iongitudinal bands are indented by any suitable forming means, such as by a press, and fastened in place by spot or gas welding, for example. The circumferential bands are formed by welding together the ends or by forging or by any other suitable means and spot or gas welded or sweated around the cylinder. The circumferential and longitudinal bands are preferably spot welded to each other at all cross-overs. The
casings strength is greatly reinforced because the closed circumferential bands hold the longitudinal bands in place, snug against the surface of the cylinder.
In the arrangement of the present invention, great strength is imparted to the casing by having all bands contact its surface throughout substantially their entire lengths. No ridges, such as would be produced by one set of bands overlapping the other, are present in the present structure, thus preventing the disadvantages inherent in such a ridged arrangement, which disadvantages are effective increase in diameter of the structure caused by elevation of certain of the bands and separation of these bands from the casing with its consequent disadvantages.
In a modified arrangement, both groups of bands may spiral around the casing, one group having indentations which nest into indentations in the cylinder wall and the other group crossing the first group over these indentations. The angle of intersection may then be a right angle of any other convenient angle. In another modification, the bands may be woven over and then under other bands, in a basket weave manner, although such construction is diflicult with steel bands of an appreciable thickness.
Various other modifications are possible in the embodiments described above without departing from the spirit and scope of the invention, as indicated by the appended claims.
What is claimed is:
1. In combination, a hollow metal receptacle having an indentation in the outside surface thereof, a metallic band fastened to the outside of said receptacle in such a manner that it passes over said indentation, said band being indented throughout its width in the portion thereof over said indentation, and a second metallic band fastened to the outside of said receptacle in such a manner that it crosses the indented portion of said first-mentioned band, the dimension of said indentation longitudinally of said first band being substantially equal to the transverse dimension of the second band, and the surface of the receptacle surrounding the indentation being relatively smooth.
2. In combination, a hollow metal receptacle having an indentation i the outside surface thereof, a metallic band fastened to the outside of said receptacle in such a manner that it passes over said indentation, said band being indented throughout its width in the portion thereof over said indentation, a second metallic band fastened to the outside of said receptacle in such a manner that it crosses the indented portion of said first-mentioned band, and means, for
fastening said first band to said second band at said crossing, the dimension of said indentation longitudinally of said first band being substantially equal to the transverse dimension of the second band, and the surface of the receptacle surrounding the indentation being relatively smooth.
3. In combination, a hollow metal receptacle for gases at high pressure, a large portion at least of which is cylindrical, a first group of bands each fastened to the outside of said receptacle, and a second group of bands arranged to cross the bands of the first group, said receptacle having an indentation in the outside surface thereof under each of said crossings and each of the bands of the first group having an indentation throughout its width extending into the corresponding indentation in said receptacle, whereby each of said bands is in contact with the surface of said receptacle throughout substantially all its length, the dimension of each indentation longitudinally of .each band in the first group being substantially equal to the transverse dimension of the band in the second group at that point, and the surface of the receptacle surrounding the identation being relatively smooth.
4. In combination, a hollow metal receptacle for gases under high pressure, a large portion at I least of which is cylindrical, a plurality of longitudinal bands eachfastened to the outside of said receptacle, and a plurality of circumferential bands around said cylinder and crossing said longitudinal bands at substantially right angles, said receptacle having an indentation therein under each of said crossings and each of said longitudinal bands having an indentation at said crossing interfitting the longitudinal band in the corresponding indentation in said receptacle,
whereby each of said bands is in contact with the surface of said receptacle throughout substantially all its length.
5. In combination, a hollow metal receptacle for gases under high pressure, a large portion .at
least of which is cylindrical, a plurality of indented bands each fastened to the outside of said receptacle, and a plurality of other bands around said cylinder and crossing said indented bands, said receptacle having an indentation therein under each of said crossings and each of said indented bands having an indentation at said crossing interfitting the longitudinal band in the corresponding indentation in said receptacle, whereby all of said bands are in contact with the surface of said receptacle throughout substantially all their length, each of the indentations in said receptacle being only slightly larger than an area equal to the width of the adjacent indented band times the width of the said other band crossing it.
6. In combination, a hollow metal receptacle I for gases under high pressure, a large portion at least of which is cylindrical, a plurality of indented bands each fastened to the outside of said receptacle, and a plurality of other bands around said cylinder and crossing said indented bands, said receptacle having an indentation therein under each of said crossings and each of said indented bands having an indentation throughout its width extending into the corresponding indentation in said receptacle, whereby each of said bands is in contact with the surface of said receptacle throughout substantially all its length.
each of the indentations in said receptacle being of substantially the same depth as the thickness of an indented band and the dimension of each indentation longitudinally of each of said indented bands being substantially equal to the tranverse dimension of said other band at that point, and the surface of the receptacle surrounding the indentation being relatively smooth.
receptacle throughout substantially all its length,
and means for fastening each indented band to each of the dther hands it crosses, the dimension of each indentation longitudinally of each of said indented bands being substantially equal to the transverse dimension of said other band at that point, and the surface of the receptacle surrounding the indentation being relatively smooth.
8. In combination, a hollow metal receptacle for gases under high pressure comprising a smooth surface cylindrical portion having a plurality of groups of aligned indentations therein, and two end portions welded to said cylindrical portion to form a gas tight container, a plurality of indented bands each of which is in contact with the surface of and is fastened to said cylindrical and end portions, each band being so positioned that it passes over a group of said indentations and is also indented so that it nests into each of the indentations in the aligned group, the indentations in each group being aligned with the indentations in the other groups. and a plurality of crossing bands around said cylindrical portion and over said indented bands at the indentations thereof, each of said crossing bands being in contact with the surface of said cylindrical portion for its entire length except for the portions thereof immediately over the indentations in said cylinder crossed by said 9. In combination, a hollow metal receptacle for gases under high pressure, a large portion at least of which is cylindrical, a plurality of bands each fastened to the outside of said receptacle, and another band spiralled around said receptacle and crossing each of said first-mentioned bands, said receptacle having an indentation therein under each. of said crossings and each of said first-mentioned bands having an indentation throughout its width at said crossing interfitting the first-mentioned band in the corresponding indentation in said receptacle. whereby each of said bands is in contact with the surfaceof said receptacle throughout substantially all its length, the dimension of each of said indentations longitudinally of said firstmentioned bands being substantially equal to the transverse dimension of the band spiralled around said receptacle and the surface of the; receptacle surrounding the indentations therein
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US449384A US2344856A (en) | 1942-07-02 | 1942-07-02 | Means for reinforcing hollow containers for gases under pressure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US449384A US2344856A (en) | 1942-07-02 | 1942-07-02 | Means for reinforcing hollow containers for gases under pressure |
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US2344856A true US2344856A (en) | 1944-03-21 |
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US449384A Expired - Lifetime US2344856A (en) | 1942-07-02 | 1942-07-02 | Means for reinforcing hollow containers for gases under pressure |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2426630A (en) * | 1943-09-27 | 1947-09-02 | Specialties Dev Corp | High-pressure gaseous oxygen package |
US2684170A (en) * | 1950-12-11 | 1954-07-20 | Smith Corp A O | Noncorrosive welded tank joint |
US3123243A (en) * | 1964-03-03 | Sectionalized motor case construction | ||
US3970208A (en) * | 1973-12-28 | 1976-07-20 | National Forge Company | Protective shield for pressure vessels |
US5433332A (en) * | 1991-04-12 | 1995-07-18 | Sira S.P.A. | Container for roving |
US9618160B2 (en) | 2009-02-06 | 2017-04-11 | Hexagon Technology As | Pressure vessel longitudinal vents |
US10088110B2 (en) | 2016-05-17 | 2018-10-02 | Hexagon Technology As | Pressure vessel liner venting via nanotextured surface |
US10544901B2 (en) | 2016-04-06 | 2020-01-28 | Hexagon Technology As | Pressure vessel vented boss with sintered metal plug |
US10627048B2 (en) | 2015-12-16 | 2020-04-21 | Hexagon Technology, As | Pressure vessel dome vents |
AU2021229217B1 (en) * | 2021-04-22 | 2021-12-16 | Mark Stewart Dimmock | Hydrogen transportation and storage system |
US20230035247A1 (en) * | 2021-07-27 | 2023-02-02 | Airbus Operations S.L.U. | Hydrogen tank for aircraft |
US12092266B2 (en) * | 2019-12-02 | 2024-09-17 | Plug Power Inc. | Support structure for cryogenic transport trailer |
-
1942
- 1942-07-02 US US449384A patent/US2344856A/en not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3123243A (en) * | 1964-03-03 | Sectionalized motor case construction | ||
US2426630A (en) * | 1943-09-27 | 1947-09-02 | Specialties Dev Corp | High-pressure gaseous oxygen package |
US2684170A (en) * | 1950-12-11 | 1954-07-20 | Smith Corp A O | Noncorrosive welded tank joint |
US3970208A (en) * | 1973-12-28 | 1976-07-20 | National Forge Company | Protective shield for pressure vessels |
US5433332A (en) * | 1991-04-12 | 1995-07-18 | Sira S.P.A. | Container for roving |
US9618160B2 (en) | 2009-02-06 | 2017-04-11 | Hexagon Technology As | Pressure vessel longitudinal vents |
US11073240B2 (en) * | 2015-12-16 | 2021-07-27 | Hexagon Technology As | Pressure vessel dome vents |
US10627048B2 (en) | 2015-12-16 | 2020-04-21 | Hexagon Technology, As | Pressure vessel dome vents |
US10544901B2 (en) | 2016-04-06 | 2020-01-28 | Hexagon Technology As | Pressure vessel vented boss with sintered metal plug |
US10088110B2 (en) | 2016-05-17 | 2018-10-02 | Hexagon Technology As | Pressure vessel liner venting via nanotextured surface |
US12092266B2 (en) * | 2019-12-02 | 2024-09-17 | Plug Power Inc. | Support structure for cryogenic transport trailer |
AU2021229217B1 (en) * | 2021-04-22 | 2021-12-16 | Mark Stewart Dimmock | Hydrogen transportation and storage system |
US20230035247A1 (en) * | 2021-07-27 | 2023-02-02 | Airbus Operations S.L.U. | Hydrogen tank for aircraft |
US12135111B2 (en) * | 2021-07-27 | 2024-11-05 | Airbus Operations S.L.U. | Hydrogen tank for aircraft |
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