U.S. patent number 3,762,448 [Application Number 05/080,511] was granted by the patent office on 1973-10-02 for thick walled pressure vessel.
This patent grant is currently assigned to Struthers Scientific and International Corporation. Invention is credited to John Donohue.
United States Patent |
3,762,448 |
Donohue |
October 2, 1973 |
**Please see images for:
( Certificate of Correction ) ** |
THICK WALLED PRESSURE VESSEL
Abstract
A thick walled pressure vessel having a tubular wall is
prestressed by bending to resist extreme external pressures, the
bending being applied by the external pressure being resisted. The
tubular or cylindrical wall contains internal axial cuts which
divide the wall into axial sectors with faying surfaces
therebetween so that the application of external pressure decreases
the curvature of the sectors to prestress them.
Inventors: |
Donohue; John (Howell, NY) |
Assignee: |
Struthers Scientific and
International Corporation (New York, NY)
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Family
ID: |
26238113 |
Appl.
No.: |
05/080,511 |
Filed: |
October 13, 1970 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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691090 |
Nov 22, 1967 |
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Foreign Application Priority Data
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Nov 24, 1966 [GB] |
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52,653/66 |
Jan 20, 1967 [GB] |
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3,178/67 |
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Current U.S.
Class: |
138/171;
220/DIG.29; 228/235.1; 29/446; 220/581; 228/141.1 |
Current CPC
Class: |
B21D
51/24 (20130101); F17C 1/00 (20130101); Y10S
220/29 (20130101); Y10T 29/49863 (20150115); F17C
2201/0104 (20130101); F17C 2209/221 (20130101); F17C
2203/0636 (20130101) |
Current International
Class: |
B21D
51/16 (20060101); F17C 1/00 (20060101); B21D
51/24 (20060101); B23p 011/02 () |
Field of
Search: |
;113/12S
;29/477.7,477,477.3,475,497.5,446 ;138/171 ;220/3,DIG.29 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Klinksiek; Henry T.
Parent Case Text
CROSS REFERENCES TO RELATED APPLICATIONS
This application is a division of patent application Ser. No.
691,090 filed Nov. 22, 1967, now abandoned.
Claims
I claim:
1. In a thick walled pressure vessel, a tubular wall for resisting
high external pressure, said wall containing internal axial cuts
dividing the wall into axial sectors with faying surfaces
therebetween, the faying surfaces being sealed at their outer edges
at the outer surface of said wall, said sectors elastically bending
to decrease their curvature under external pressure to prestress
said sectors and thereby said wall of said pressure vessel.
2. The combination according to claim 1 wherein said faying
surfaces are closed under external pressure.
3. The combination according to claim 1 wherein said tubular wall
is cylindrical, and wherein said axial sectors when unprestressed
have curvatures totalling more than 360.degree. and are elastically
bent by external pressure to close said faying surfaces and have
curvatures then totalling substantially 360.degree..
4. In the process of forming a thick walled pressure vessel having
a curved metal closing wall of an integral layer of material
wherein the closing wall has axial sectors joined and sealed at
their outer edges;
abutting the metal closing wall axial sectors leaving open faying
surfaces therebetween,
and bending the closing wall to decrease its curvature to resist
higher external pressures by applying ecternal pressure to close
the faying surfaces.
Description
BACKGROUND OF THE INVENTION
It is well known that when a normally unstressed thick-walled
cylinder is subjected to high pressure on either the outside or the
inside, the circumferential stress at the inside of the wall is
greater than that at the outside by the amount of the pressure
applied. It is, therefore, common in producing such cylinders that
are to be subject to a pressure that is a significant fraction of
the allowable stress, to trap into the wall a beneficial prestress
which will be more or less cancel out the difference in stress
between the outside and inside and thereby allow a higher average
stress. This has been done by shrinking one or more cylinders
together, winding with wire or tape under tension, applying
controlled pressure so that a portion of the wall is stressed
beyond its yield point, and by controlled quenching from the
metal's plastic temperature. This disclosure describes a novel
method of using bending to produce the desired results, and points
out that its use has advantages not only in internally pressurized
vessels, but even more particularly in externally pressurized
vessels, where the first two methods cannot be used and the third
is often impractical.
SUMMARY OF THE INVENTION
With regard to external pressure, where the desired prestress is
circumferential tension at the inner wall and compression at the
outer, with a consequent radial tension in the wall, winding is
obviously impractical and concentric cylinders will have initial
clearance, making them highly susceptible to buckling. With the
bending method, however, all final stresses are compressive; and it
can be shown that, by suitably calculating the planes of the faying
surfaces, the prestresses can be applied simultaneously with the
pressure. In fact, the paradoxical but sound conclusion can be
reached that a vessel, lightly but suitably sealed, composed of two
semi-cylindrical halves, can be stronger than a continuous
cylindrical vessel of the same dimensions.
BRIEF DESCRIPTION OF THE DRAWING
FIGS. 1 and 2 are diagrams showing the internal and external radii
of a thick walled pressure vessel with radial, circumferential, and
axial stresses graphed as a function of cylinder wall
thickness;
FIGS. 3, 4, 6 and 9 are end views of two sectors of a cylinder
having internal faying surfaces so that the cylinder will be
prestressed by bending as it is subjected to external pressure,
FIGS. 3, 4, 6 and 9 showing the effect of progressively increasing
external pressure on the cylinder; and
FIGS. 5, 7 and 8 show stress and pressure forces acting on a half
of each of the sectors of FIGS. 4, 6 and 9 respectively.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
To evaluate the desired prestress in a thick walled cylinder
subjected to outside or inside pressure, a choice must be made from
several theories of tube failure: maximum stress, strain energy,
maximum shear, etc. In the case of the closed tubular vessel under
external pressure only, there are no tensile stresses involved.
Failure must occur at the inner surface as this is the only free
surface. Also, since the stresses involved are compression in both
axial and circumferential directions, and failure by direct
compression is inconceivable, failure must be by shear. For the
most efficient condition, the shear stress should be equal in all
directions, or the axial and the circumferential compression at the
inner surface should be equal, giving a resultant shearing stress
equal to one-half the compressive stress and at 45.degree. to any
radius.
The formulae for stresses in a thick cylinder are ##SPC1##
where
s.sub.c = circumferential stress
s.sub.r = radial stress
s.sub.a = axial stress for the case of a vessel closed at the
ends
p = pressure
r = radius
and subscripts i and o denote "inside" and "outside," respectively.
Pressure and compressive stress are considered positive and tensile
stress negative.
Further
Internal Pressure External Pressure s.sub.a = -p.sub.i
[r.sub.i.sup.2 /(r.sub.o.sup.2 -r.sub.i.sup.2)] = p.sub.o
[r.sub.o.sup.2 /(r.sub.o.sup.2 -r.sub.i.sup.2)] s.sub.ci = -p.sub.i
[(r.sub.o.sup.2 +r.sub.i.sup.2)/(r.sub.o.sup.2 -r.sub.i.sup.2)] =
2p.sub.o [r.sub.o.sup.2 /(r.sub.o.sup.2 -r.sub.i.sup.2)] s.sub.co =
-2p.sub.i [r.sub.i.sup.2 /(r.sub.o.sup.2 -r.sub.i.sup.2)] = p.sub.o
[(r.sub.o.sup.2 =r.sub.i.sup.2)/(r.sub.o .sup.2 -r.sub.i.sup.2)]
p.sub.o = 0; s.sub.Ri = -p.sub.i p.sub.i =0; s.sub.Ro = p.sub.o
s.sub.Ro = 0 s.sub.Ri = 0
For stresses due to the bending of a curved beam, we will not use
the approximation of Winkler, but the more accurate formula of
Guest (see Case, J., "Strength of Materials," Longmans, Green, and
Co., 1925; sec.285 ff., for Winkler, and sec. 309 for Guest). A
slight modification of Guest's formulae give: ##SPC2##
and, in particular, ##SPC3##
where,
s.sub.R = radial stress due to bending
s.sub.p = circumferential stress due to bending
D = an arbitrary constant
For the case of external pressure on a vessel with closed ends, we
will set up a prestress s.sub.pi by bending such that
s.sub.ci +s.sub.pi =s.sub.a or s.sub.pi = -p.sub.o
(r.sub.o.sup.2)/(r.sub.o.sup.2 -r.sub.i.sup.2)
The equations above for bending stresses in a curved beam may be
solved for D and the compensating stresses which may be obtained by
bending may be calculated. As shown in FIG. 1, a section through a
cylinder has been drawn with an internal radius r.sub.i and an
external radius r.sub.o so that r.sub.o /r.sub.i =2. Superimposed
on the horizontal radius T of the cylinder is a graph with a
horizontal axis OT and a positive vertical axis OP and a negative
vertical axis O-P.
In FIG. 1, line 20 is a graph of the uncompensated circumferential
stress in terms of a given outside pressure p.sub.o plotted on axis
OP against cylinder wall thickness plotted on axis OT. Line 24 is a
similar graph of the circumferential prestress set up in the
cylinder wall by bending to decrease its curvature. Line 21 is a
graph of the combined circumferential stresses which result in the
cylinder when prestressed by bending and subjected to an outside
pressure p.sub.o. Line 21 indicates that a cylinder prestressed by
bending may have an inside circumferential stress of about one half
that of an unprestressed cylinder. While the outside stress of a
prestressed cylinder is shown to be almost 2.5p.sub.o, there is no
place for the metal to flow. It is to be noted that even axial flow
will be resisted by the axial stress indicated by the graph line
26.
Line 23 is a graph of the radial prestress produced by bending.
Line 22 is a graph of the radial stress produced by an external
pressure of p.sub.o. Line 25 is a graph of the combined radial
stresses in a prestressed cylinder subjected to an external
pressure p.sub.o. It is interesting to note that the radial stress
produced by bending and neglected by the Winkler theory is of
benefit in reducing the radial stress near r.sub.i is a prestressed
cylinder. This reduction of radial stress reduces the tendency for
shear failure by radially inward flow.
If, however, it is desired to maintain a constant compressive
stress across the tube wall, as called for by the maximum stress
theory of failure, such a stress would be
s.sub.k = p.sub.o (r.sub.o)/(r.sub.o -r.sub.i) =s.sub.ci
+s.sub.pi
or
s.sub.pi = -p.sub.o (r.sub.o)/(r.sub.o -r.sub.i)
This again may be solved for D and the stresses calculated.
FIG. 2 shows a cylinder and a graph similar to that shown in FIG.
1. Line 20 again graphs the circumferential stress resulting from
an outside pressure p.sub.o. Line 27 graphs the circumferential
stress in the cylinder resulting from bending so that the combined
circumferential stresses in the cylinder will be approximately
constant through its thickness when subjected to an external
pressure p.sub.o. Line 28 is a graph of the combined
circumferential stresses in the cylinder which may thus be
prestressed to approximate a constant compressive stress across its
wall when subjected to an external pressure p.sub.o.
To analyze longitudinal joints in a cylinder under hydrostatic
external pressure, let us consider such a cylinder of indefinite
length with prestress due only to bending. The stress pattern will
be the same over any radial section because the bending moment
across any such section is constant and independent of the central
angle. The external pressure is constant, directed toward the
center, and independent of the central angle. There is, therefore,
no shear on any radial plane. Under full design pressure, there
will be only compression on such a radial plane.
Therefore, if it is imagined making a diametral cut while
maintaining the external pressure, there will be no change in shape
or stress distribution, since such a change would have to be due to
tension (separation of cut surfaces), shear (sliding of one cut
surface on the other), or a change of shape of the mating surfaces
without separation, which could only be caused by isolated
irregularities in the stress pattern. While such may exist, they
will be equally superimposed on the stressed and unstressed state
and may, for this discussion, be neglected. With release of the
external pressure, the two halves will separate along the cut, and
the prestress due to bending will be released so that the halves
will be free of stress. As the prestress was produced by a bending
moment tending to open up the halves to .pi. radians or
180.degree.. the halves in the unstressed position will have a
slightly greater angular measure, say .pi. + E.
Since the angle at which I make the diametral cut makes no
difference, a second diametral cut at an angle to the first should
have not more effect, except that on release of pressure I will
have four unstressed sectors. Any adjacent pair will then have a
total angular measure of .pi. + E. Also, when unstressed, adjacent
pairs must fit tightly together, because any separation would
indicate a stressed condition before the cut, contrary to the
original hypothesis. The plane cuts originally made under pressure,
therefore, remain plane in the released condition, and
conversely.
FIGS. 3-9 show two sectors or halves 61 and 62 of a cylindrical
shell 60 joined at 63. The outer wall of each sector curves 5
percent more than 180.degree. as shown in the Drawing. This would
be in the order of 0.5 percent for a steel shell 60. FIG. 3 shows
the shell 60 with no external pressure on it. FIG. 6 shows the
effect of sufficient external pressure to reduce the excess angle E
to one-half the original.
FIG. 5 shows the stresses and forces on on half the upper section.
The downward component of the pressure p is resisted by an upward
force F=pr.sub.o more or less concentrated at the outer corner 63.
While the horizontal component of the pressure plus the excess
moment of the vertical force M=Fr.sub.o is resisted by an
unsymmetrical pattern of stresses across the vertical cross section
which range from a fairly high compression at the outside to a low
tension on the inside. In FIG. 6, the external pressure has
increased to a value sufficient to close the mating surfaces
completely. At this external pressure, the stress at the inside
radius is zero around the circumference. Since there is zero
stress, there must be zero strain, and the inside circumference is
the same as in the unstressed state. However, as the total angular
measure has decreased 5 percent, the inside radius has increased 5
percent. Now, neglecting radial strains, which are slight, the wall
thickness has not changed. Therefore, while the outer radius has
increased by the same amount, it has only increased by
three-fourths as great a percent. Thus, since the decrease in
angular measurement is the same throughout, there is a shortening
or compressive strain of the outer circumference of 11/4 percent.
FIG. 7 shows the stress and pressure pattern for this condition. It
can be shown that the outer stress will be equal to the maximum
design pressure and that the pressure to produce this stress will
be (r.sub.o -r.sub.i)/2r.sub.o times this design pressure.
FIG. 9 shows the cylinder 60 under the maximum design pressure
which has produced a uniform maximum design stress across the wall
in accordance with the formulae hereinbefore given. It should be
noted that between FIGS. 6 and 9, r.sub.i has been compressed to
its original value, causing a circumferential strain of 5 percent.
r.sub.o has also returned to its original value, causing an
additional strain of 33/4 percent which, added to the strain
already present in FIG. 7 makes the external strain equal to the
internal.
Thus, it may be seen that longitudinal sectors of a pressure vessel
joined only at their outer points of contact to provide a seal may
be able to resist greater external pressures than a solid
cylindrical pressure vessel of the same wall thickness. If desired,
the faying surfaces of the sectors of such a pressure vessel may be
forced together by suitable bending and then welded to prestress
the vessel to resist greater external pressures. However, in most
applications such as deep diving marine exploration devices, the
bending and the prestress may be applied by the external pressure
which is to be resisted.
While it is possible to apply the concepts of this invention to a
spherical pressure vessel by making cuts in a thick walled sphere
to divide the sphere into sectors with bases corresponding to
regular polygons, the cuts would be made while the sphere was
subjected to pressure. On release of the pressure, the sectors,
being concave cones, could not fit perfectly tightly without
distortion.
However, solid unprestressed spherical ends may be used on a
cylindrical vessel with the same inside and outside radii as the
stresses in the unprestressed ends of a spherical ended cylindrical
vessel will generally be well under the stresses in the prestressed
cylindrical portion. While this invention has been applied to
cylindrical pressure vessels, it could equally well be applied to
vessels with oval or other axial enclosing walls.
* * * * *