Gland condenser skid system with shell and plate technology

Abstract

The present disclosure relates to a gland condenser skid system for a thermodynamic machine, i.e., a steam turbine, comprising a shell and plate heat exchanger as a gland condenser (10), the shell and plate heat exchanger being formed of welded tube plates without gaskets.

Description

[Technical Field]

[0001] The present disclosure relates to a gland condenser skid system including a gland condenser based on so-called shell and plate technology. The embodiments disclosed herein relate specifically to improved thermodynamic machines, such as steam turbines and / or engine generators, or mechanical drive stations, in which a shell and plate heat exchanger is configured to function as a gland condenser. [Background technology]

[0002] Gland condenser skid systems are used to condense steam originating from steam turbine sealing systems, particularly steam leaking past the first section of the seal on the steam turbine shaft. Specifically, when the turbine exhausts into the vacuum system, seal steam must be injected into the seal to prevent the low-pressure end of the turbine from being drawn into the atmosphere. This seal steam from the low-pressure end, and the normal leakage from the high-pressure end, tends to leak and blow out toward the bearing housing. To reduce the likelihood of this leakage causing water accumulation in the lubrication oil system, gland condenser skid systems are used to draw a very slight vacuum (typically 1 or 2 in. Hg) on ​​the outer portion of the shaft seal. Typically, the gland condenser shell side pressure is 0.96 bara.

[0003] The gland condenser skid system includes a compact heat exchanger for condensing the steam and an exhaust for extracting the non-condensable fraction of the steam stream. Additionally, the gland condenser skid system also includes silencers, piping, filters, valves, instrumentation, and structural support.

[0004] The heat exchanger used to condense the steam coming from the steam turbine sealing system, also known as a gland condenser, is usually a water-cooled shell-and-tube heat exchanger, with cooling water flowing through the tubes and steam flowing over the tubes (through the shell), with an outlet at the bottom of the shell where the condensate collects.

[0005] The use of shell-and-tube heat exchangers as gland condensers is also required by API Standard 612, which is the reference specification for the oil and gas (petroleum, petrochemical, and natural gas) market sector for steam turbines and their auxiliary equipment. Its effectiveness and application are recognized worldwide, and its applicability in oil and gas technology can be used as a direct insurance standard for end users. According to API 612, the standard solution for a condenser has a steel shell with a nominal wall thickness of 1.25 mm (0.050 in.) or more and a diameter of at least 15.88 mm (0.625 in.), brass or cupronickel tubes, and a fixed tubesheet with water on the tube side. Alternative material choices are possible depending on the type of cooling water applied. Summary of the Invention [Problem to be solved by the invention]

[0006] However, despite the high reliability of gland condensers configured as shell and tube heat exchangers, this solution also has a number of drawbacks: a) High footprint, large volume, weight and cost. b) Low heat exchange capacity. c) Restrictions on equipment use due to excessive design levels. d) In case of tube bundle damage, it is not feasible to plug the tubes due to the condenser layout (TEMA BEM solution) considering the tube sheets welded to the channels and the channel dimensions not being sufficient for proper utilization. e) Increased component complexity due to the presence of tube bundles. f) High installation and maintenance costs.

[0007] Shell and plate heat exchangers are not used as gland condensers, as this solution does not guarantee against any contamination that may occur in the cooling fluid by sealing the steam turbine oil. In fact, shell and plate heat exchangers do not offer a welded tube sheet system, but rather the package is joined by a plate gasket solution, which is prone to leaks. The main interface of the shell and plate heat exchanger is connected to the high temperature and high pressure case.

[0008] According to the invention, it is proposed to use a shell and plate heat exchanger as a gland condenser in the oil and gas sector, for which purpose the shell and plate heat exchanger is provided with a welded plate package in order to avoid any possible leakage and contamination.

[0009] Thus, in one aspect, the subject matter disclosed herein relates to a shell and plate heat exchanger as a gland condenser, the shell and plate heat exchanger comprising a tube sheet package excluding gaskets (FIGS. 2-3).

[0010] Furthermore, in another aspect, the subject matter disclosed herein relates to new technological solutions with clear benefits in size, weight and cost, maintaining similar safety conditions and with higher thermal efficiency. [Brief explanation of the drawings]

[0011] The disclosed embodiments of this invention and many of the attendant advantages thereof will become more fully appreciated as the same becomes better understood by reading the following detailed description when taken in conjunction with the accompanying drawings, in which: [Figure 1] FIG. 1 shows a perspective view of a gland condenser consisting of a shell and plate heat exchanger. [Figure 2] Figure 2 shows a schematic diagram of the internal flow distribution of a gland condenser consisting of a shell and plate heat exchanger. [Figure 3A]FIG. 3A shows a schematic diagram of the internal flow distribution of the high-temperature fluid in a gland condenser consisting of a shell and plate heat exchanger. [Figure 3B] FIG. 3B shows a schematic diagram of the internal flow distribution of the cryogenic fluid in a gland condenser consisting of a shell and plate heat exchanger. [Figure 4] FIG. 4 shows a perspective view of a gland condenser system with a shell and plate heat exchanger as the gland condenser. [Figure 5] Figure 5 shows a schematic diagram of the piping and instrumentation diagram (P&ID) of a gland condenser system with a shell and plate heat exchanger as the gland condenser. DETAILED DESCRIPTION OF THE INVENTION

[0012] According to one aspect, the present subject matter relates to a gland condenser skid system that includes a shell and plate heat exchanger formed of fully welded plates as the gland condenser.

[0013] According to another aspect, the present subject matter relates to a gland condenser skid system that includes a gasket-less shell and plate heat exchanger as the gland condenser.

[0014] Referring now to the drawings, FIG. 1 shows a perspective view of a gland condenser, generally designated by reference numeral 10, consisting of a shell and plate heat exchanger with a shell 10'. The gland condenser 10 is provided with a first inlet 11 for air and steam flows from a steam turbine sealing system to be cooled and a second inlet 12 for a cooling fluid flow, typically water, for exchanging heat with the steam and air flows to be cooled. The gland condenser 10 also has a first outlet 13 for the cooling fluid flow and a second outlet 14 for the air and at least partially condensed steam flow. The air and at least partially condensed steam flows are then conveyed to an external hot water reservoir for final separation. FIG. 1 also shows a portion of a structure 15 supporting the gland condenser 10.

[0015] FIG. 2A shows a schematic diagram of the internal flow distribution of a gland condenser 10, which is composed of a shell and plate heat exchanger with multiple plates 10″ stacked together to form a plate group with multiple free spaces, but separated from each other. Each space is contained between two adjacent plates 10″. The spaces contained between two adjacent plates 10″ alternately define a first flow path connecting an inlet 11 and an outlet 14 for the flow of air and steam S to be cooled and a second flow path connecting an inlet 12 and an outlet 13 for the flow of cooling fluid F. The plates 10″ are welded to keep the first and second flow paths separate. Heat is exchanged between the flow of air and steam S to be cooled and the flow of cooling fluid F passing through the plates 10″. The fully welded plates are assembled into a shell 10′.

[0016] FIG. 3A shows a flow S of air and steam to be cooled flowing on one side of a plate 10'', and FIG. 3B shows a flow F of cooling fluid flowing on the other side of the same plate 10''.

[0017] 4 shows a perspective view of a gland condenser system comprising a shell and plate heat exchanger as a gland condenser 10 according to the present disclosure. The gland condenser system also comprises a tank 16 for further separating the condensate from the air and steam flow S, and two electrically driven exhaust fans 17 for exhausting the residual air and steam through outlets 18 and 19 for exhausting the condensate, or alternatively a steam ejector system.

[0018] FIG. 5 shows a schematic diagram of a piping and instrumentation diagram (P&ID) of a gland condenser system with a shell and plate heat exchanger as the gland condenser according to the present disclosure.

[0019] Gland condenser skid systems, including gland condensers based on shell and plate technology, entail many advantages over gland condensers based on shell and tube technology, including: -More compact and flexible layout. Shell and plate heat exchangers allow for higher efficiency than traditional shell and tube layouts. Furthermore, depending on specific demands, suitable designs can be developed by optimizing simple parameters such as vessel diameter, length, and flow direction. -Higher heat transfer rate and efficiency (reduced heat exchange surface). Shell and plate heat exchangers guarantee a heat exchange coefficient up to 8 times higher than comparable shell and tube layouts. - Significantly reduced footprint, volume and weight, resulting in lower installation costs. -Lower cooling water flow requirements as a result of the very high heat exchange coefficient. Significant savings in cooling water flow are achieved for the same work. -Limited and standardized heat exchange solutions, resulting in higher performance and larger standard size applications. -Performance reliability and robust design. -Reliable, cost-effective production with low hold-up volumes in a variety of petrochemical applications, especially for shell and tube technology, with cost benefits ranging from 15-35% depending on material and size classification. - Strong fatigue resistance due to plate layout (i.e. corrugated shape) and geometric control which can eliminate fatigue issues. -Ability to handle liquids, gases and two-phase mixtures, including a wide range of aggressive media, which means there are no limitations regarding fluid type and corrosive / erosive effects. -Ability to handle pressures up to 100 bar g (1450 psi g) according to PED and ASME, along with temperatures as high as 450°C, due to a solution that completely welds the tubesheet package excluding gaskets. - Fully welded solution (laser welded corrugated tube sheets) and no gaskets to solve any leakage problems. -Material applicability from carbon steel, stainless steel to titanium. No restrictions on material selection, covering any type of cooling water.

[0020] While aspects of the present invention have been described in terms of various specific embodiments, it will be apparent to those skilled in the art that many modifications, changes, and omissions may be made without departing from the spirit and scope of the claims.

Claims

1. A gland condenser (10) is provided with a shell and plate heat exchanger formed of welded tube plates without gaskets, The gland condenser (10) has a plurality of plates arranged substantially parallel to one another within the tubular shell and transverse to the axis of the shell, The plurality of plates are configured to alternately form, between adjacent plates, at least one space for a cooling fluid to pass in a first direction and at least one space for a fluid to be cooled, including air and steam, to pass in a second direction intersecting the first direction; the cooled fluid inlet (11) and outlet (14) are oriented perpendicular to the axis of the shell, and at least one space for the cooled fluid to pass through defines a first flow path fluidically connecting the cooled fluid inlet (11) and the cooled fluid outlet (14); the cooling fluid inlet (12) and outlet (13) are provided at axially opposite ends of the shell, and at least one space for the cooling fluid to pass through defines a second flow path fluidly connecting the cooling fluid inlet (12) and the cooling fluid outlet (13); the plurality of plates are welded to separate the first flow path and the second flow path; A gland condenser skid system, comprising: two or more cooling fluid inlets (12); and a corresponding cooling fluid outlet (13) for each cooling fluid inlet (12) disposed downward along the axis of each inlet (12).

2. The system of claim 1, further comprising a tank (16) connected downstream of the gland condenser (10).

3. 3. The system according to claim 2, wherein the upper part of the tank (16) is connected to at least one exhaust system by a fan (17).

4. 3. The system of claim 2, wherein the top of the tank (16) is connected to at least one exhaust system by a vapor exhauster.

5. The bottom of the tank (16) is connected to at least one condensate outlet (19). A system according to any one of claims 2 to 4.

6. 6. The system according to claim 1, wherein the plurality of plates are planar in shape such that at least one space for the cooling fluid to pass through and at least one space for the cooled fluid to pass through extend in a plane.

7. 7. The system of claim 1, wherein the plurality of plates are configured to form a plurality of pairs of spaces for the cooling fluid to pass through and spaces for the cooled fluid to pass through adjacent to the spaces for the cooling fluid to pass through.

8. 8. The system of claim 1, further comprising at least one flow passage extending through the plurality of plates and configured to fluidly connect the cooling fluid inlet (12), the cooling fluid outlet (13) and at least one space for the cooling fluid to pass through.

9. 9. The system according to claim 1, wherein at least one space for the passage of the cooled fluid is configured so that the cooled fluid is supplied and discharged through the periphery of the corresponding plate.

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