[0001] The invention relates to a heat exchanger structure particularly for nuclear plants.
[0002] It is known that in the design of heat exchangers intended for operation in very
drastic conditions due to high pressures or temperatures being involved, technicians
are called upon to overcome considerable difficulties. Particularly in the case of
nuclear plants, where for example a sodium-air exchanger is provided which operates
at a high temperature, the calculation standards which the designer is forced to follow
are so exacting that, notwithstanding the sophisticated and highly laborious crosschecking
calculations which are carried out, the prior art requires construction techniques
which often show considerable complexity.
[0003] This results mainly from the fact that said standards require that crosschecks be
made in the operating condition bearing in mind the several overlapping loads which,
albeit with a modest degree of likelihood, could occur simultaneously; thus, to the
primary stresses of thermal origin brought about by material deformations as the temperature
increases from ambient temperature to operative temperature, the stresses are to be
added due to seismic phenomena, those deriving from thermal transients, creep stresses,
and others yet, thereby complex and costly constructions are required effective to
resist thereagainst.
[0004] This invention is aimed at providing a heat exchanger structure particularly for
nuclear plants, wherein constructional techniques of great simplicity can be adopted
to reduce costs both through material and labour savings.
[0005] Within the proposed aim, it is an object of the invention to provide a heat exchanger
structure which can bring about a simplification in the crosschecking calculations.
[0006] According to one aspect of the present invention the proposed aim and cited object
are achieved by a heat exchanger structure particularly for nuclear plants, characterized
in that it comprises at least one pair of headers connected by a tube nest, said tube
nest having a cold pre-deformed structure, such as to minimize, in the operating condition
thereof, the primary stresses of thermal origin.
[0007] It will be appreciated that according to one embodiment the said pre-tensioning effecting
cold pre-deformation is opposite to the thermal deformation or stresses caused in
the operative temperature conditions.
[0008] The solution stems from the consideration that the strain pattern or distribution
induced by the primary stresses of thermal origin alone, in the operating condition,
is close to the limit conditions imposed by the cold condition standards, thereby,
by imparting the tube nest with cold pre-stressing so as to substantially induce said
strain pattern, one will achieve in the hot operating condition a minimization of
such primary stresses, thus leaving an ample margin for subsequent verifications which
take into account the seismic phenomena, thermal transients, etc., which in the cold
condition, as is apparent, were not to be accounted for.
[0009] The possibility derives from the foregoing of adopting specially advantageous construction
forms, such as having a cross-section of quadrangular, instead of circular, shape
for the headers, as better specified hereinafter.
[0010] Further features and advantages will be more clearly apparent from the description
of a preferred, though not exclusive, embodiment of the invention, as illustrated
by way of example and not of limitation in the accompanying drawings, where:
Figure 1 is a schematical side elevation view of the invention;
Figure 2 is a sectional view taken in the plane II-II of Figure 1, showing for reference
purposes a single tube of the tube nest;
Figure 3 is a detail view of the mounting of one tube of the tube nest to the header.
[0011] With reference to the above-mentioned views, indicated at 1 and 2 are the two headers
with quadrangular cross-section connected by a tube nest formed by generally yoke-like
or U-like tubes such as 3, with the web portion of the U-shape or centrally thereof
having a substantial extension. The tubes are, as previously mentioned, subjected
to cold pre-stressing, the stress whereof is substantially relieved as the exchanger
is operated at a high temperature, thanks to deformation of the materials. The temperature
of of the cold, pre-stressing may be the room temperature or any other low temperature
suitable to create the desired stress relieving effect in operative conditions.
[0012] An advantageous structural symmetry is achieved by securing the tubes such as 3 with
a retaining action in all directions via the support 3a located substantially in the
middle of the web portion of the U-shape of the tubes and by means of the supports
3b and 3c arranged symmetrically offset with respect to the support 3a on the web
portion of the U-shape, near the elbows thereof and providing retention only perpendicularly
to the plane in which the U-like tubes extend, while allowing axial movement in the
axial direction of the tubes and in a direction parallel to said plane in which the
tubes extend (plane in which Fig. 1 is located) and perpendicular to the tubes themselves.
For the purpose the holes of support 3b have an elongated shape in the last mentioned
direction. Assuming that the exchanger in question transports the hot fluid through
the interior of the headers and tubes of the tube nest which are swept across the
exterior wall by the cold fluid, e.g. ambient air, there may occur two conditions
of operation; a first condition, which we will call isothermal, when no cold fluid
is directed into the exchanger and accordingly the exchanger is at a uniform temperature
throughout, and a second condition, which we will call of power removal, which occurs
when cold fluid is directed into the exchanger interior in the interspace between
the tubes so that the inlet header, which we assume to be the one indicated at 1,
will be at a higher temperature than the cooled tubes 3 and related supports.
[0013] To also achieve minimal primary stresses of thermal origin in the perpendicular direction
to the plane containing the yokes, provision is then made to reduce the longitudinal
drilling pitch 4(or distance between the holes)on the header 1 for connecting the
tubes such as 3 with respect to the drilling pitch 5 on the support 3b, so that the
resulting pre-stressing of the tubes in the cold condition is substantially cancelled,
along with its related stresses, in the power removal conditions of operation thanks
to the greater expansion of the header 1 over the support 3b.
[0014] In the instance of an exchanger wherein it is the cold fluid that flows through the
interior of the headers and tubes swept exteriorly by the hot fluid, it will, of course,
be the pitch 5 which is decreased relatively to the pitch 4.
[0015] One of the main advantages to be derived from the low stress values occurring at
the connection sections of the tube nest tubes to the headers resides in the possibility
of adopting quadrangular cross-section headers, i.eo formed by flat radiused plates,
instead of the usual circular cross-section headers which have a much higher rigidity
than the flat plates, and which must be used of necessity, owing to the high stresses,
on the exchangers fabricated in accordance with the prior art.
[0016] The quadrangular cross-section appreciably facilitates the construction of the header
supports and allows the geometry of the tube nest tubes to be simplified.
[0017] The connecting lugs such as 6 of the headers to the tubes 3 may then be formed by
milling the flat plates such as 1a of the headers, instead of extruding them as is
required in the case of circular cross-section headers.
[0018] For the purpose the starting plate 1a has an initial thickness equal to the sum of
the projecting length of lug 6 and the final thickness of plate 1a and by milling
the excess thickness corresponding to the length of the lug 6 is removed, except for
the portion which will form the lug 6 which thus is an integral part of the plate
1a. This affords savings in the heat treatment which otherwise would be necessary
after the extrusion and the fabrication of the end section of the lugs is possible
with the same thickness as the tubes such as 3, thus enabling said tubes to be welded
directly i.e. in abutment relationship onto the lugs, with attendant elimination of
the intermediate stub pipe which is required where the lugs are obtained by extrusion
for the purpose of providing gradual transition from the tube thickness to that of
the end section of the lug which is much larger; the connection, therefore, reduces
itself to making a single weld, which in addition may be effected in ideal conditions
with the IBW (Internal Bore Welding) method, contrary to what happens in the case
of the circular cross-section header owing to the continued adjustments involved.
[0019] Another feature to be pointed out is that the ample margin left for strength checks
in the operating condition, by virtue of the primary stresses of thermal origin having
been minimized, allows for easier calculations, with appreciable savings in designing
time, which may normally require even a few months.
[0020] The invention just described is susceptible to many modifications and variations,
all of which fall within the scope of the inventive concept; further, all the details
may be replaced with other technically equivalent elements.
[0021] In practicing the invention, the materials used, as well as the shapes and dimensions,
may be any ones contingent on individual requirements.
1. A heat exchanger structure particularly for nuclear plants, characterized in that
it comprises at least one pair of headers (1,2) connected by a tube nest (3),said
tube nest having a coldfpre-deformed structure, such as to minimize, in the operating
condition thereof, the primary stresses of thermal origin.
2. A heat exchanger structure particularly for nuclear plants, characterized in that
it comprises two substantially parallel headers (1,2) of quadrangular cross-section
connected by a tube nest (3) formed by yoke-like tubes with remarkable extension of
the central leg, being cold pre-deformed so as to minimize, in the operating condition,
the primary stresses of thermal origin.
3. An exchanger structure according to one or more of the preceding claims, characterized
in that the yoke-like tubes (3) are retained in all directions by means of supports
(3a) at the substantially middle area, and are retained in the normal direction to
the plane containing the yoke by means of supports (3b,3c) at two areas arranged symmetrically
with respect to the middle area substantially at the end of the central leg.
4o An exchanger structure according to one or more of the preceding claims, characterized
in that the lugs (6) for providing connection between the yoke-like tubes (3) and
headers (1,2), as formed by milling from the plates of said headers (1,2) and integral
therewith,have at the end section thereof a thickness such as to allow direct abutment connection
to said tubes.
5. An exchanger structure according to one or more of the preceding claims, characterized
in that the weldments between the lugs (6) and yoke-like tubes (3) are effected with
the IBW method.
6. An exchanger structure according to one or more of the preceding claims, containing
the hot fluid inside the headers (1,2) and tubes (3), characterized in that the longitudinal
pitch (4) of the connection holes on the inlet header (1) with the yoke-like tubes
(3) is reduced over the pitch (5) of said tubes (3) at the supports (3b).
7. An exchanger structure according to one or more of the preceding claims, containing
the cold fluid inside the headers (1,2) and tubes (3), characterized in that the longitudinal
pitch (4) of the connection holes on the inlet header with the yoke-like tubes (3)
is increased over the pitch (5) of said tubes (3) at the supports (3b,3c).
8. A heat exchanger structure particularly for nuclear plants, according to the preceding
claims, and substantially as herein described and illustrated.