GLAND CONDENSER SKID SYSTEMS BY SHELL & PLATES TECHNOLOGY

Abstract

The disclosure concerns a gland condenser skid system for thermodynamic machine, namely a steam turbine, the gland condenser skid system comprising a shell and plates heat exchanger as gland condenser (10), said shell and plates heat exchanger being formed of gasket-free welded tube sheets.

Claims

1. A gland condenser skid system comprising a shell and plates heat exchanger as gland condenser, said shell and plates heat exchanger being formed of gasket-free welded tube sheets.

2. The system according to claim 1, wherein a tank is connected downstream said gland condenser.

3. The system according to claim 2, wherein the top of said tank is connected to at least one evacuation system by fans.

4. The system according to claim 2, wherein the top of said tank is connected to at least one evacuation system by steam ejectors.

5. The system according to claim 2, wherein the bottom of said tank is connected to at least one condensate outlet.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0017] A more complete appreciation of the disclosed embodiments of the invention and many of the attended advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:

[0018] FIG. 1 illustrates a perspective view of a gland condenser composed of a shell and plates heat exchanger;

[0019] FIG. 2 illustrates a schematic view of internal flow distribution of a gland condenser composed of a shell and plates heat exchanger;

[0020] FIG. 3A illustrates a schematic view of the hot fluid internal flow distribution of a gland condenser composed of a shell and plates heat exchanger;

[0021] FIG. 3B illustrates a schematic view of the cold fluid internal flow distribution of a gland condenser composed of a shell and plates heat exchanger;

[0022] FIG. 4 illustrates a perspective view of a gland condenser system comprising a shell and plates heat exchanger as gland condenser, and

[0023] FIG. 5 illustrates a schematic view of a piping and instrumentation diagram (P&ID) of a gland condenser system comprising a shell and plates heat exchanger as gland condenser.

DETAILED DESCRIPTION OF EMBODIMENTS

[0024] According to one aspect, the present subject matter is directed to a gland condenser skid system comprising a shell and plates heat exchanger as gland condenser, said shell and plates heat exchanger being formed of fully welded plates.

[0025] According to another aspect, the present subject matter is directed to a gland condenser skid system comprising a gasket-free shell and plates heat exchanger as gland condenser.

[0026] Referring now to the drawing, FIG. 1 shows a perspective view of a gland condenser composed of a shell and plates heat exchanger, indicated as a whole by the reference number 10 and comprising a shell 10, the gland condenser 10 being provided with a first inlet 11 for a flow of air and steam from a steam turbine sealing system, to be cooled, and a second inlet 12 for a flow of a cooling fluid, usually water, to exchange heat with the flow of steam and air to be cooled. The gland condenser 10 is also provided with a first outlet 13 for the flow of cooling fluid and a second outlet 14 for the flow of air and at least partially condensed steam. The flow of air and at least partially condensed steam is then conveyed to an external hot well for final separation. FIG. 1 also shows part of the structure 15 supporting the gland condenser 10.

[0027] FIG. 2A illustrates a schematic view of the internal flow distribution of the gland condenser 10, composed of a shell and plates heat exchanger, comprising a plurality of plates 10, stacked on each other and still separated from each other to form a plate pack provided with a plurality free spaces, each space being comprised between two adjacent plates 10. The space comprised between two adjacent plates 10 alternately define a first flow path connecting the inlet 11 and the outlet 14 of the flow S of air and steam to be cooled and a second flow path connecting the inlet 12 and the outlet 13 of the flow F of cooling fluid. The plates 10 are welded to keep the first flow path and the second flow path separate. Heat is exchanged between the flow S of air and steam to be cooled and the flow F of cooling fluid through the plates 10. The fully welded plate pack is assembled into the shell 10.

[0028] FIG. 3A shows the flow S of air and steam to be cooled, running on one side of a plate 10, while FIG. 3B shows the flow F of cooling fluid, running on the other side of the same plate 10.

[0029] FIG. 4 illustrates a perspective view of a gland condenser system comprising a shell and plates heat exchanger as gland condenser 10 according to the present disclosure, the gland condenser system also comprising a tank 16 for additional separation of condensate from the flow S of air and steam, two motorized evacuation fans 17, or alternatively a steam ejector system, for evacuation of residual air and steam through an outlet 18 and an outlet 19 for evacuation of condensate.

[0030] FIG. 5 illustrates a schematic view of a piping and instrumentation diagram (P&ID) of a gland condenser system comprising a shell and plates heat exchanger as gland condenser according to the present disclosure.

[0031] The gland condenser skid system including a gland condenser based on shell and plates technology involves many advantages over a gland condenser based on shell and tubes technology, including: [0032] more compact and flexible lay-out, the shell and plates heat exchanger allowing a higher efficiency than traditional shell and tubes layout; additionally, depending on specific needs, a proper design can be developed by simple parameters optimization as vessel diameter, length and flow direction; [0033] higher heat transfer rate & efficiency (reduced heat exchanging surface), shell and plates heat exchangers ensuring heat exchanging coefficient up to 8 times higher than equivalent shell and tubes layouts; [0034] lower installation costs, with strong reduction in foot printing, volume and weight; [0035] lower cooling water flow request, as a consequence of a strongly higher heat exchanging coefficient; important saving of cooling water flow is achieved with similar duty; [0036] limited and standardized heat exchange solution, since a higher performance larger standard size application is obtained; [0037] performance reliability & robust design; [0038] low hold-up volume, reliable and cost-effective production in a variety of petrochemical applications; in particular, over shell and tubes technology, cost benefits are comprised in the range of 15-35% depending on materials and size classes; [0039] solid Resistance to fatigue, due to plates layout (i.e. corrugated shape) and geometrical control able to exclude fatigue issue; [0040] ability to work with liquids, gases and two-phase mixtures, including a wide range of aggressive media, implying no limitation with respect to fluid typology and corrosion/erosion effects; [0041] ability to handle pressures up to 100 bar g (1450 psi g) as per PED and ASME, along with temperatures as high as 450 C., due to fully welded solution of tube sheet package with gasket exclusion; [0042] fully welded solution (corrugated tube sheet pack by laser welding) and gasket-free, to solve any leakage issue; [0043] materials applicability from carbon steel, stainless steel to titanium: no limitation for material selection able to cover any cooling water type.

[0044] While aspects of the invention have been described in terms of various specific embodiments, it will be apparent to those of ordinary skill in the art that many modifications, changes, and omissions are possible without departing form the spirt and scope of the claims.