Heat exchanger tube support structure

Information

  • Patent Grant
  • 6498827
  • Patent Number
    6,498,827
  • Date Filed
    Monday, November 1, 1999
    25 years ago
  • Date Issued
    Tuesday, December 24, 2002
    22 years ago
Abstract
A support plate for retaining tube array spacing within a heat exchanger tube and shell structure. The support plate having a plurality of individual tube receiving apertures formed therein. Each apertures has at least three inwardly protruding members and bights are formed therebetween when the tube associated therewith is lodged in place to establish secondary fluid flow through the support plate. The inwardly protruding members terminate in flat lands that restrain but do not all contact the outer surface of the respective tube. These flat lands minimize fretting wear and eliminate potential gouging of the outer wall of the tube. The plate wall forming each aperture has an hourglass configuration which, inter alia, reduces pressure drop, turbulence and local deposition of magnetite and other particulates on the support plates.
Description




FIELD AND BACKGROUND OF THE INVENTION




The invention relates generally to heat exchanger construction and more particularly to support plates for retaining tube array spacing within the heat exchanger.




DESCRIPTION OF THE PRIOR ART




The pressurized water vapor generators or heat exchangers, associated with nuclear power stations and which transfer the reactor-produced heat from the primary coolant to the secondary coolant that drives the plant turbines may be as long as 75 feet and have an outside diameter of about 12 feet. Within one of these heat exchangers, straight tubes through which the primary coolant flows may be no more than ⅝ inch in outside diameter, but have an effective length of as long as 52 feet between the tube-end mountings and the imposing faces of the tube sheets. Typically, there may be a bundle of more than 15,000 tubes in one of these heat exchangers. It is clear that there is a need to provide structural support for these tubes in the span between the tube sheet faces to ensure tube separation, adequate rigidity, and the like.




The tube support problem has led to the development of a drilled support plate structure of the type described in U.S. Pat. No. 4,120,350. This support system consists of an array of flat plates that is arranged in the heat exchanger with the planes of the individual plates lined transverse to the longitudinal axes of the tubes in the bundle. Holes or apertures are drilled and broached in each of the flat support plates to accommodate the tubes. Each aperture has at least three inwardly protruding members that restrain but do not all engage or contact the outer surface of the respective tube. Bights that are intermediate of these inwardly protruding members are formed in the individual support plate apertures when the tube associated therewith is lodged in place to establish secondary fluid flow through the plate. The inwardly protruding members terminate in arcs that define a circle of a diameter that is only slightly greater than the outside diameter of the associated tube. The broached support plates are made of SA-212 Gr.B, a carbon material, and may include tube free lanes with unblocked broached holes which detrimentally allow low steam quality secondary fluid flow to pass through the unblocked holes.




It has been found, after long periods of operation, that deposits consisting primarily of magnetite are formed at the tube support plates. These deposits block the bights formed between protruding members and thus cause undesirable increases in pressure drop which will in turn result in an increase in the secondary water level in the downcomer. If corrective actions are not taken, the rising water level could potentially flood the steam bleed ports and the main feed water nozzles and result in a malfunction of the steam bleeding and the main feed water systems.




Corrective actions such as power derating, chemical cleaning or water slap are costly. Moreover, the removal of deposits by chemical cleaning or water slap could damage the support plates.




Accordingly, there is a need for a tube support plate which minimizes pressure drop and deposit blockage while providing adequate structural strength.




BRIEF SUMMARY OF THE INVENTION




The problems associated with the prior art tube support plates are largely overcome by the present invention which resorts to a stronger more corrosive resistant plate material such as stainless steel and by forming hourglass shaped tube holes in the support plates which minimize pressure drop by reducing local turbulence and are less likely to cause the deposition of magnetite and other particles on the surface of the support plates.




In view of the foregoing it will be seen that one aspect of the invention is to manufacture the tube support plates out of a stronger more corrosion resistant material such as stainless steel.




Another aspect of this invention is to have the protruding members of the broached holes terminate in flat lands.




A further aspect of the present invention is to provide hourglass shaped broached holes in the tube support plates.




These and other aspects of the present invention will be more fully understood after a review of the following description of the preferred embodiment along with the accompanying drawings.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a vertical elevation view in full section of a once-through vapor generator embodying the principles of the invention;





FIG. 2

is a plan view of a portion of a prior art support plate;





FIG. 3

is a plan view of one of the broached holes in the prior art support plate shown in

FIG. 2

with a tube inserted therethrough;





FIG. 4

is a detail view of a portion of the tube abutting one of the protruding members of the prior art broached hole shown in

FIG. 3

;





FIG. 5

is a plan view of a portion of a support plate and tube assembly that embodies principles of the invention for use with a heat exchanger of the type shown in

FIG. 1

;





FIG. 6

is a plan view of one of the broached holes in the support plate shown in

FIG. 5

with a tube inserted therethrough;





FIG. 7

is a detail view of a portion of the tube abutting one of the protruding members of the broached hole shown in

FIG. 6

;





FIG. 8

is a plan view of one of the broached holes in the support plate shown in

FIG. 5

with the tube removed; and





FIG. 9

is a cross-sectional view taken along lines A—A of

FIG. 8

showing the hourglass feature of the present invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




The present invention is described in connection with a once-through steam generator for a nuclear power plant, although these principles are generally applicable to shell and tube heat exchangers in any number of diverse fields of activities. Thus, as shown in

FIG. 1

for the purpose of illustration, a once-through steam generator unit


10


comprising a vertically elongated cylindrical pressure vessel or shell


11


closed at its opposite ends by an upper head member


12


and a lower head member


13


.




The upper head includes an upper tube sheet


14


, a primary coolant inlet


15


, a manway


16


and a handhole


17


. The manway


16


and the handhole


17


are used for inspection and repair during times when the vapor generator unit


10


is not in operation. The lower head


13


includes drain


18


, a coolant outlet


20


, a handhole


21


, a manway


22


and a lower tube sheet


23


.




The vapor generator


10


is supported on a conical or cylindrical skirt


24


which engages the outer surface of the lower head


13


in order to support the vapor generator unit


10


above structural flooring


25


.




As hereinbefore mentioned, the overall length of a typical vapor generator unit of the sort under consideration is about 75 feet between the flooring


25


and the upper extreme end of the primary coolant inlet


15


. The overall diameter of the unit


10


moreover, is in excess of 12 feet.




Within the pressure vessel


11


, a lower cylindrical tube shroud wrapper or baffle


26


encloses a bundle of heat exchanger tubes


27


, a portion of which is shown illustratively in FIG.


1


. In a vapor generator unit of the type under consideration moreover, the number of tubes enclosed within the baffle


26


is in excess of 15,000, each of the tubes having an outside diameter of ⅝ inch. It has been found that Alloy 690 is a preferred tube material for use in vapor generators of the type described. The individual tubes in the bundle


27


each are anchored in respective holes formed in the upper and lower tube sheets


14


and


23


through belling, expanding or seal welding the tube ends within the tubesheets.




The lower baffle or wrapper


26


is aligned within the pressure vessel


11


by means of pins (not shown). The lower baffle


26


is secured by bolts (not shown) to the lower tubesheet


23


or by welding to lugs (not shown) projecting from the lower end of the pressure vessel


11


. The lower edge of the baffle


26


has a group of rectangular water ports


30


or, alternatively, a single full circumferential opening (not shown) to accommodate the inlet feedwater flow to the riser chamber


19


. The upper end of the baffle


26


also establishes fluid communication between the riser chamber


19


within the baffle


26


and annular downcomer space


31


that is formed between the outer surface of the lower baffle


26


and the inner surface of the cylindrical pressure vessel


11


through a gap or steam bleed port


32


.




A support rod system


28


is secured at the uppermost support plate


45


B, and consists of threaded segments spanning between the lower tubesheet


23


and the lowest support plate


45


A and thereafter between all support plates


45


up to the uppermost support plate


45


B.




A hollow toroid shaped secondary coolant feedwater inlet header


34


circumscribes the outer surface of the pressure vessel


11


. The header


34


is in fluid communication with the annular downcomer space


31




35


through an array of radially disposed feedwater inlet nozzles


35


. As shown by the direction of the

FIG. 1

arrows, feedwater flows from the header


34


into the vapor generating unit


10


by way of the nozzles


35


and


36


. The feedwater is discharged from the nozzles downwardly through the annular downcomer


31


and through the water ports


30


into the riser chamber


19


. Within the riser chamber


19


, the secondary coolant feedwater flows upwardly within the baffle


26


in a direction that is counter to the downward flow of the primary coolant within the tubes


27


. An annular plate


37


, welded between the inner surface of the pressure vessel


11


and the outer surface of the bottom edge of an upper cylindrical baffle or wrapper


33


insures that feedwater entering the downcomer


31


will flow downwardly toward the water ports


30


in the direction indicated by the arrows. The secondary fluid absorbs heat from the primary fluid through the tubes in the bundle


27


and rises to steam within the chamber


19


that is defined by the baffles


26


and


33


.




The upper baffle


33


, also aligned with the pressure vessel


11


by means of alignment pins (not shown), is fixed in an appropriate position because it is welded to the pressure vessel


11


through the plate


37


, immediately below steam outlet nozzles


40


. The upper baffle


33


, furthermore, enshrouds about one third of the tube bundle


27


.




An auxiliary feedwater header


41


is in fluid communication with the upper portion of the tube bundle


27


through one or more nozzles


42


that penetrate the pressure vessel


11


and the upper baffle


33


. This auxiliary feedwater system is used, for example, to fill the vapor generator


10


in the unlikely event that there is an interruption in the feedwater flow from the header


34


. As hereinbefore mentioned, the feedwater, or secondary coolant that flows upwardly through the tube bank


27


in the direction shown by the arrows rises into steam. In the illustrative embodiment, moreover, this steam is superheated before it reaches the top edge of the upper baffle


33


. This superheated steam flows in the direction shown by the arrow, over the top of the baffle


33


and downwardly through an annular outlet passageway


43


that is formed between the outer surface of the upper cylindrical baffle


33


and the inner surface of the pressure vessel


11


. The steam in the passageway


43


leaves the vapor generating unit


10


through steam outlet nozzles


40


which are in communication with the passageway


43


. In this foregoing manner, the secondary coolant is raised from the feed water inlet temperature through to a superheated steam temperature at the outlet nozzles


40


. The annular plate


37


prevents the steam from mixing with the incoming feedwater in the downcomer


31


. The primary coolant, in giving up this heat to the secondary coolant, flows from a nuclear reactor (not shown) to the primary coolant inlet


15


in the upper head


12


, through individual tubes in the heat exchanger tube bundle


27


, into the lower head


13


and is discharged through the outlet


20


to complete a loop back to the nuclear reactor which generates the heat from which useful work is ultimately extracted.




Referring now to

FIG. 2

, there is shown a plan view of a portion of a prior art support plate


45


characterized by holes or apertures


46


, each of which has at least three inwardly protruding members


47


that restrain but do not all engage or contact the outer surface of the tube


48


extending through the hole


46


. Bights


49


that are intermediate of these inwardly protruding members


47


are formed in the individual support plate holes


46


when the associated tube


48


is lodged in place to establish fluid passage through the plate


45


. The inwardly protruding members


47


terminate in arcs or arcuate lands


51


that define a circle of a diameter that is only slightly greater than the outside diameter of the associated tube


48


.




Turning now to prior art

FIG. 3

, there is shown a plan view of one of the broached holes


46


and a portion of the surrounding support plate


45


of

FIG. 2

with a tube


48


inserted through the broached hole


46


. A detail of

FIG. 3

is shown at

FIG. 4

which depicts a problem encountered with this prior art broached hole


46


whereby the sharp edges


50


formed along the vertical sides of the arcuate land


51


of the inwardly protruding member


47


can potentially gouge the outer wall of tube


48


thereby resulting in a faster increase in the depth rate at which through-wall tube wear occurs for a given volume loss. This prior art support plate


45


also allows for a small annular space between the arcuate land


51


and the outer wall of tube


48


and, due to the associated flow restrictions, results in rapidly accumulating detrimental deposits for at least some of the support plates


52


.




Referring now to

FIG. 5

, there is shown a plan view of a portion of support plate


52


characterized by holes or apertures


53


, each of which has at least three inwardly protruding members


54


that restrain but do not all engage or contact the outer surface of the tube


55


extending through the hole


53


. Bights


56


that are intermediate of these inwardly protruding members


54


are formed in the individual support plate holes


53


when the associated tube


55


is lodged in place to establish fluid passage through the plate


52


. In accordance with the present invention, the inwardly protruding members


54


terminate in flat lands


57


.




Turning now to

FIG. 6

, there is shown a plan view of one of the broached holes


53


of

FIG. 5 and a

portion of the surrounding support plate


52


. A tube


55


extends through the broached hole


53


. A detail of

FIG. 6

is shown at

FIG. 7

where the flat land


57


of the inwardly protruding member


54


provides sufficient tube contact length to lower contact stress thereby minimizing fretting-wear of the tube


55


. The flat land configuration also eliminates the potential gouging of the outer wall of tube


55


thus decreasing the depth rate at which through-wall wear occurs for a given volume loss. Moreover, the space between the flat land


57


and the outer wall of tube


55


is increased to reduce deposition accumulation.




Referring to

FIG. 8

, there is shown a plan view of one of the broached holes


53


of

FIG. 5 and a

portion of the surrounding support plate


52


. As shown in FIG.


8


and in

FIG. 9

which is a cross-sectional view taken along lines A—A of

FIG. 8

, the inner wall


58


forming the protruding member


54


in the support plate


52


has an hourglass configuration comprised of a tube contact section


59


with beveled end sections


60


. In a tube support plate of the type under consideration, the thickness of the broached plate is 1.5 inches, the length of the tube contact section


59


is 0.75 inches, and the chamfer angle of the beveled end section


60


is 11 degrees.




The beveled end sections


60


of the broached holes


53


improve the local fluid flow patterns and reduce the deposition of magnetite and other particles on the support plate


52


due to a decrease in hydraulic shock losses. Computational fluid dynamic modelling of the flow paths through an hourglassed broached hole


53


and experimental testing have confirmed that the gradual contraction and expansion of the fluid flow therethrough effectively reduces pressure drop which contributes to the greater margin for system pressure drop increases. Furthermore, as a result of a reduction in the hydraulic loss coefficient, the hourglassed configured broached holes


53


contribute to greater margins for water level problems such as water level instability and high water levels resulting from high pressure drops. The hourglass configuration reduces fluid turbulence in the area of contact between tube


55


and the protruding member


54


of support plate


52


thereby reducing local deposition of magnetite and other particles on the support plate


52


. The hourglass configuration also allows for greater rotational motions between tubes


55


and the protruding members


54


before experiencing binding due to a moment couple from opposing forces at the top and bottom edges of the tube support plate


52


.




According to the present invention, the tube support plate


52


is made of stainless SA-240 410S material with a specified high yield of 50 ksi or above and ultimate tensile strength (UTS) of 80 ksi or above.




The following chart shows the superiority of the SA-240 410S stainless steel material of the present invention when compared to the SA-212 Gr.B carbon steel used to make the prior art tube support plates


47


.


















Material Specification




Chemical




Yield (ksi)




UTS (ksi)











SA-212 GrB




C-Si




38 ksi (min)




70 ksi (min)






SA-240 410S




13 Cr




50 ksi (min)




80 ksi (min)














From the foregoing it is thus seen that the tube support plates


52


made with SA-240 410S stainless material provide (1) improved corrosion resitance; (2) higher strength; and (3) improved compatibility to minimize fretting wear with the tubes


55


which are made of Alloy 690 material.




While a specific embodiment of the invention has been shown and described in detail to illustrate the application of the principles of the invention, it will be understood that the invention may be embodied otherwise without departing from such principles.



Claims
  • 1. In a heat exchanger tube and shell structure, a generally flat support plate having a plurality of individual tube receiving apertures formed therein, at least three members integral with the plate defining each of the apertures, the integral members protruding inwardly toward the center of the respective aperture and forming bights between at least adiacent pairs of the members in order to provide a predetermined flow area when the tube that is individual to the respective aperture is lodged in place, the flow area having an inlet and an outlet, the members having beveled and sections at the inlet and the outlet, the inwardmost end of each of the integral members forming a flat land, said protruding integral member flat lands restraining but not all contacting the outer surface of the individual tube that is to be received within the respective aperture.
  • 2. A heat exchanger tube and shell structure according to claim 1 wherein each of the apertures has an hourglass configuration.
  • 3. A heat exchanger tube and shell structure according to claim 1 wherein the beveled end sections have a chamfer angle of about 11 degrees.
  • 4. A heat exchanger tube and shell structure according to claim 1 wherein the inwardmost end of each of the integral members includes a tube contact section formed between the beveled end sections.
  • 5. A heat exchanger tube and shell structure according to claim 4 wherein the tube contact section is about 0.75 inches in length.
  • 6. A heat exchanger tube and shell structure according to claim 1 wherein the plate is formed from SA-240 410S stainless steel material.
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Number Name Date Kind
4120350 Norton Oct 1978 A
4204305 Norton May 1980 A
4220199 Romanos Sep 1980 A
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4576228 Glatthorn Mar 1986 A
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4690206 Bein Sep 1987 A
4709756 Wilson et al. Dec 1987 A
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4902468 Veronesi et al. Feb 1990 A
4933138 Mouesca et al. Jun 1990 A
5072786 Wachter Dec 1991 A
5092280 Franklin et al. Mar 1992 A
5178822 Buford, III et al. Jan 1993 A
Foreign Referenced Citations (2)
Number Date Country
3008455 Sep 1981 DE
0296018 Dec 1988 EP