US2792965A - Pressure vessel construction - Google Patents
Pressure vessel construction Download PDFInfo
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- US2792965A US2792965A US470410A US47041054A US2792965A US 2792965 A US2792965 A US 2792965A US 470410 A US470410 A US 470410A US 47041054 A US47041054 A US 47041054A US 2792965 A US2792965 A US 2792965A
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- pressure vessel
- skirt
- vessel
- high temperature
- construction
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J3/00—Processes of utilising sub-atmospheric or super-atmospheric pressure to effect chemical or physical change of matter; Apparatus therefor
- B01J3/04—Pressure vessels, e.g. autoclaves
Definitions
- This invention relates to a pressure vessel construction having a laminated support skirt.
- Pressure vessels of circular cross section are often supported by a cylindrically shaped skirt support on a xed foundation.
- a longitudinal temperature gradient In such a construction there may exist large -dilerences between the temperature of the shell and of the foundation, thus subjecting the skirt to a longitudinal temperature gradient.
- Such temperature conditions will cause the higher temperature portions of the skirt to expand to a diameter proportional to the thermal coeiiicient of expansion of the metal, and this diameter is different at all of the longitudinal positions of the skirt.
- This induces longitudinal bending stresses into the metal of the skirt. If the mechanical integrity of the skirt is to be maintained under any given conditions of longitudinal temperature gradient, these bending stresses must be at ⁇ a safe value, and such value must be well within the elastic limit of the metal.
- the skirt is usually required to sustain the dead weight loading of the pressure vessel, the dynamic or shock loading of the vessel and the piping reactions transmitted to it through the vessel.
- the skirts are required to sustain very high temperature gradients, shock loads, and piping reactions and the problem of obtaining a proper skirt design is compounded when there is added the usual condition that the vessel and its support means must occupy a minimum volume.
- the conventional skirt design wherein the skirt is made of a single thick plate, becomes inadequate because the bending stresses are prohibitively high.
- the present invention solves this problem by providing a cylindrically shaped skirt support made of a number of thin shells placed concentrically and coextensively one within another so as to present a laminated structure. For 'any given temperature conditions this structure is subject to much lower bending stresses than a solid plate of the same thickness. It is well known in the field of mechanics that for any given length of a member subjected to longitudinal temperature gradient, that a thin member will develop less bending stress than a thicker member. However, such thin sections will not carry as large a compressive load as thick members.
- the present invention involves a number of thin members placed to gether in a laminated structure yand thus acting in conjunction to :carry the required compressive load with the result that the composite structure develops less bending stress than a single plate of the same dimensions.
- a high temperature pressure vessel construction facilitating its support with a minimum of thermally created stresses.
- Fig. 1 is a partial sectional elevation of a pressure vessel supported by a laminated skirt in accordance with the invention
- Fig. 2 is a plan section on line 2 2 of Fig. 1;
- Fig. 3 is a partial section of the lamina weld
- Fig. 4 is a partial section of an alternate attachment of the skirt toa foundation.
- a high temperature and high pressure vessel 10 having a closed end 11 is supported by a cylindrically shaped skirt 12 which rests on a foundation 14.
- the lower end of the skirt 12 is fixed to the foundation 14 by a number of circumferentially spaced angle irons 16..
- the skirt 12 comprises the thin'lamina plates 18, 20 and 22.
- the inner plate 18 is formed from a rectangular plate into a circular shell and its edges joined by the longitudinal weld 24.
- the second plate 20, is similarly formed into a circular shell and snugly fitted around plate 18 with its longitudinal ends joined by a weld 26.
- the outside plate 22 is formed into a circular shell and snugly tted around plate 20 and its edges joined by the longitudinal weld 28.
- Each of 'the longitudinal welds are made as in Figure 3 where the edges of the plate 22 ⁇ are shaped to receive a backing strip 29. This c0nstruction precludes any of the plates from being joined by the welds.
- the skirt is then attached to the pressure vessel 10 by a large weld 30 which unites all of the plates 18, 20 and 22 to the pressure vessel.
- Fig. 4 is an alternate construction to that of Fig. l for attaching the lower edge of the skirt 12 to a founda tion 14A by a common weld joining the plates 18A, 20A and 22A. Such a construction would be used in cases where the pressure vessel 10 would have a large overturning moment.
- the lamination plates are assembled in such a way that they act in conjunction for supporting the vessel but are free to individually and independently distort in bending. It is important that in the assembly of the laminations that they not be preshunk into place or that they not be joined at any point except at the ends of the skirt. They should be simply in surface to surface contact so as to give mutual support to each other to withstand the compressive loading.
- the present invention provides a support for a pressure vessel which is of the shortest longitudinal length for any given set of load and temperature conditions.
- a high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal cross section and a metallic laminated cylindrically shaped skirt having its larninations integrally secured to the pressure vessel and to each other by a common securement in heat transfer relationship and extending beyond one end of said vessel for the support thereof.
- a high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal cross section and a metallic laminated cylindrically shaped skirt secured to the pressure vessel in heat transfer relationship and extending beyond one end of said vessel for the support thereof, said skirt formed by a plurality ofconcentric' metal laminac arrangedin surface to surface contact and joined to each other only at their end portions and free for relative rnovement'interrnediate their ends.
- a high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal Y cross section and a metallic laminated cylindrically Ashaped skirt secured to the pressure vessel in heat transfer rela tionship 'and' extending beyond one end of said vessel for the support thereof, said skirt formed'by a plurality of concentric Vcoextensive metaly laminae arranged' in surface to surface contact andjoined to each other only at their end portions vandrfree for relative movement intermediate their ends.
- a high temperature pressure vessel construction comprising-a vertically elongated'pressure vesselsubject to a high temperature -and having a -circular horizontal cross ⁇ section and a 'metallic laminated cylindrically ShapedslCirt'secured-to'thepressure vessel in heat transfer relationship Vand'extencling*beyond one end kof said ⁇ vessel for 'thesupport'thereoh said skirt formed Vby a plurality of concentric metal laminae arranged in surface to sur-V fa-cefcontactand joined to each other only'at their end portions, said laniinae being joined to each other and to said 'vessel by a-comrnon Weld at one edge ofsaid skirt.
- a high temperature ⁇ pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having acircular horizontal cross section and a metallic laminated cylindrically shaped ⁇ skirty secured to the pressure vessel in heat transfer relationship and extending beyond one end of said vessel for the support thereof, said skirt formed by a plurality of concentric metal laininae arranged in surface to surface contact and joined to each other only at their end portions, said laminae Being-joined to each other and to the lower portion of said vessel by a common Weld at one edge of said'ski'rt.
- a high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal cross section and a metallic laminated cylindrically shaped skirt secured to the pressure vessel in heat transfer relationship .and extending beyond one end of said vessel for the support thereof, said. shirt formed by a plurality of concentric metal larninae arranged in surface to surface contact and joined to each otheronly at their yend portions, said'laniinae being joined to each other .and to the lower portion of said vessel and said foundation structure by common Vweld's at opposite edges of said skirt.
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- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
May 21, 1957 E. E. scHoEssow PRESSURE VESSEL CONSTRUCTION Filed Nov. 22, 1954 2 INVENTO R fr] 'oassow ATTORNEY FIG.2
United States Patent'O PRESSURE VESSEL CONSTRUCTION Earl E. Schoessow, Barberton,
Babcock & Wilcox Company, corporation of New Jersey Ohio, assignor to The New York, N. Y., a
This invention relates to a pressure vessel construction having a laminated support skirt.
Pressure vessels of circular cross section are often supported by a cylindrically shaped skirt support on a xed foundation. In such a construction there may exist large -dilerences between the temperature of the shell and of the foundation, thus subjecting the skirt to a longitudinal temperature gradient. Such temperature conditions will cause the higher temperature portions of the skirt to expand to a diameter proportional to the thermal coeiiicient of expansion of the metal, and this diameter is different at all of the longitudinal positions of the skirt. This induces longitudinal bending stresses into the metal of the skirt. If the mechanical integrity of the skirt is to be maintained under any given conditions of longitudinal temperature gradient, these bending stresses must be at `a safe value, and such value must be well within the elastic limit of the metal. The skirt is usually required to sustain the dead weight loading of the pressure vessel, the dynamic or shock loading of the vessel and the piping reactions transmitted to it through the vessel. In many of the advanced engineering applications in use by industry today, the skirts are required to sustain very high temperature gradients, shock loads, and piping reactions and the problem of obtaining a proper skirt design is compounded when there is added the usual condition that the vessel and its support means must occupy a minimum volume. In this case the conventional skirt design, wherein the skirt is made of a single thick plate, becomes inadequate because the bending stresses are prohibitively high.
The present invention solves this problem by providing a cylindrically shaped skirt support made of a number of thin shells placed concentrically and coextensively one within another so as to present a laminated structure. For 'any given temperature conditions this structure is subject to much lower bending stresses than a solid plate of the same thickness. It is well known in the field of mechanics that for any given length of a member subjected to longitudinal temperature gradient, that a thin member will develop less bending stress than a thicker member. However, such thin sections will not carry as large a compressive load as thick members. The present invention involves a number of thin members placed to gether in a laminated structure yand thus acting in conjunction to :carry the required compressive load with the result that the composite structure develops less bending stress than a single plate of the same dimensions. Thus there is provided a high temperature pressure vessel construction facilitating its support with a minimum of thermally created stresses.
The various features of novelty which characterize the invention are pointed out with particularity in the claims annexed to and forming a part of this specification. For a better understanding of the invention, its operating advantages and speciiic objects attained by its use, reference should be had to the accompanying drawings and descrip- 2,792,965 Patented May 21, 1957 ICC tive matter in which there is illustrated and described preferred embodiments ofthe invention.
In the drawings:
Fig. 1 is a partial sectional elevation of a pressure vessel supported by a laminated skirt in accordance with the invention;
Fig. 2 is a plan section on line 2 2 of Fig. 1;
Fig. 3 is a partial section of the lamina weld; and
Fig. 4 is a partial section of an alternate attachment of the skirt toa foundation.
A high temperature and high pressure vessel 10 having a closed end 11 is supported by a cylindrically shaped skirt 12 which rests on a foundation 14. The lower end of the skirt 12 is fixed to the foundation 14 by a number of circumferentially spaced angle irons 16..
The skirt 12 comprises the thin'lamina plates 18, 20 and 22. The inner plate 18 is formed from a rectangular plate into a circular shell and its edges joined by the longitudinal weld 24. The second plate 20, is similarly formed into a circular shell and snugly fitted around plate 18 with its longitudinal ends joined by a weld 26. Similarly the outside plate 22 is formed into a circular shell and snugly tted around plate 20 and its edges joined by the longitudinal weld 28. Each of 'the longitudinal welds are made as in Figure 3 where the edges of the plate 22 `are shaped to receive a backing strip 29. This c0nstruction precludes any of the plates from being joined by the welds. The skirt is then attached to the pressure vessel 10 by a large weld 30 which unites all of the plates 18, 20 and 22 to the pressure vessel.
Fig. 4 is an alternate construction to that of Fig. l for attaching the lower edge of the skirt 12 to a founda tion 14A by a common weld joining the plates 18A, 20A and 22A. Such a construction would be used in cases where the pressure vessel 10 would have a large overturning moment.
The lamination plates are assembled in such a way that they act in conjunction for supporting the vessel but are free to individually and independently distort in bending. It is important that in the assembly of the laminations that they not be preshunk into place or that they not be joined at any point except at the ends of the skirt. They should be simply in surface to surface contact so as to give mutual support to each other to withstand the compressive loading.
The present invention provides a support for a pressure vessel which is of the shortest longitudinal length for any given set of load and temperature conditions.
While in accordance with the provisions of the statutes, I have illustrated and described herein a speciic form of the invention now known to me, those skilled in the art will understand that changes may be made in the form ot' the apparatus disclosed without departing from the spirit of the invention covered by my claims, and that certain features of the invention may sometimes be used to advantage without a corresponding use of the other features.
I claim:
1. A high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal cross section and a metallic laminated cylindrically shaped skirt having its larninations integrally secured to the pressure vessel and to each other by a common securement in heat transfer relationship and extending beyond one end of said vessel for the support thereof.
2. A high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal cross section and a metallic laminated cylindrically shaped skirt secured to the pressure vessel in heat transfer relationship and extending beyond one end of said vessel for the support thereof, said skirt formed by a plurality ofconcentric' metal laminac arrangedin surface to surface contact and joined to each other only at their end portions and free for relative rnovement'interrnediate their ends.
3. A high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal Y cross section anda metallic laminated cylindrically Ashaped skirt secured to the pressure vessel in heat transfer rela tionship 'and' extending beyond one end of said vessel for the support thereof, said skirt formed'by a plurality of concentric Vcoextensive metaly laminae arranged' in surface to surface contact andjoined to each other only at their end portions vandrfree for relative movement intermediate their ends.
4. A high temperature pressure vessel construction comprising-a vertically elongated'pressure vesselsubject to a high temperature -and having a -circular horizontal cross` section and a 'metallic laminated cylindrically ShapedslCirt'secured-to'thepressure vessel in heat transfer relationship Vand'extencling*beyond one end kof said `vessel for 'thesupport'thereoh said skirt formed Vby a plurality of concentric metal laminae arranged in surface to sur-V fa-cefcontactand joined to each other only'at their end portions, said laniinae being joined to each other and to said 'vessel by a-comrnon Weld at one edge ofsaid skirt.
5; A high temperature `pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having acircular horizontal cross section and a metallic laminated cylindrically shaped `skirty secured to the pressure vessel in heat transfer relationship and extending beyond one end of said vessel for the support thereof, said skirt formed by a plurality of concentric metal laininae arranged in surface to surface contact and joined to each other only at their end portions, said laminae Being-joined to each other and to the lower portion of said vessel by a common Weld at one edge of said'ski'rt.
6. A high temperature pressure vessel construction comprising a vertically elongated pressure vessel subject to a high temperature and having a circular horizontal cross section and a metallic laminated cylindrically shaped skirt secured to the pressure vessel in heat transfer relationship .and extending beyond one end of said vessel for the support thereof, said. shirt formed by a plurality of concentric metal larninae arranged in surface to surface contact and joined to each otheronly at their yend portions, said'laniinae being joined to each other .and to the lower portion of said vessel and said foundation structure by common Vweld's at opposite edges of said skirt.
References Cited in the ille of -lthis patent UNITED STATES PATENTS 55,791, VanV Duzer .June 19, .1866 95,324 Cochran Sept. 28, 1869 1,921,247 Walker Aug. 8, 193,3 2,057,347 Reed Oct. 131936 2,404,777 Gaines July 30, 1946
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US470410A US2792965A (en) | 1954-11-22 | 1954-11-22 | Pressure vessel construction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US470410A US2792965A (en) | 1954-11-22 | 1954-11-22 | Pressure vessel construction |
Publications (1)
Publication Number | Publication Date |
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US2792965A true US2792965A (en) | 1957-05-21 |
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Application Number | Title | Priority Date | Filing Date |
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US470410A Expired - Lifetime US2792965A (en) | 1954-11-22 | 1954-11-22 | Pressure vessel construction |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2967352A (en) * | 1955-06-22 | 1961-01-10 | Kellogg M W Co | Method of welding a skirt to a cylindrical vessel |
US2993617A (en) * | 1959-06-01 | 1961-07-25 | Rheem Mfg Co | Lined tank and method of making |
US3143238A (en) * | 1962-03-13 | 1964-08-04 | Firestone Tire & Rubber Co | Single walled metal containers |
US3497101A (en) * | 1967-01-31 | 1970-02-24 | Hideo Sagara | Multi-layer container |
JPS5033325B1 (en) * | 1970-05-30 | 1975-10-29 | ||
JPS5036045B1 (en) * | 1970-04-27 | 1975-11-20 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US55791A (en) * | 1866-06-19 | Improvement in milk-cans | ||
US95324A (en) * | 1869-09-28 | Improvement in mile-can | ||
US1921247A (en) * | 1932-05-11 | 1933-08-08 | Solar Sturges Mfg Co | Milk can and method of making same |
US2057347A (en) * | 1934-03-24 | 1936-10-13 | Smith Corp A O | Beer barrel |
US2404777A (en) * | 1942-01-29 | 1946-07-30 | Republic Industries | Container and closure therefor |
-
1954
- 1954-11-22 US US470410A patent/US2792965A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US55791A (en) * | 1866-06-19 | Improvement in milk-cans | ||
US95324A (en) * | 1869-09-28 | Improvement in mile-can | ||
US1921247A (en) * | 1932-05-11 | 1933-08-08 | Solar Sturges Mfg Co | Milk can and method of making same |
US2057347A (en) * | 1934-03-24 | 1936-10-13 | Smith Corp A O | Beer barrel |
US2404777A (en) * | 1942-01-29 | 1946-07-30 | Republic Industries | Container and closure therefor |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2967352A (en) * | 1955-06-22 | 1961-01-10 | Kellogg M W Co | Method of welding a skirt to a cylindrical vessel |
US2993617A (en) * | 1959-06-01 | 1961-07-25 | Rheem Mfg Co | Lined tank and method of making |
US3143238A (en) * | 1962-03-13 | 1964-08-04 | Firestone Tire & Rubber Co | Single walled metal containers |
US3497101A (en) * | 1967-01-31 | 1970-02-24 | Hideo Sagara | Multi-layer container |
JPS5036045B1 (en) * | 1970-04-27 | 1975-11-20 | ||
JPS5033325B1 (en) * | 1970-05-30 | 1975-10-29 |
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