The present invention relates to steam turbines, and in particular to steam turbines designed to facilitate later modification for operation with power plant incorporating carbon capture facilities.
Recently, there has been a growing consensus that global warming and resultant climatic change are serious threats to future socioeconomic stability. This has prompted interest in carbon capture and storage—so-called “carbon sequestration”—as a way of continuing to use fossil fuels without releasing carbon dioxide into the atmosphere. Unfortunately, carbon capture and sequestration technologies are not yet fully developed. Furthermore, designing power plants to capture the carbon they produce is likely to reduce their efficiency substantially. Consequently, most fossil-fuelled power-plants are still being built without provision for future carbon capture. It is therefore likely that governments will make regulations and/or provide incentives so that plants are designed for ease of retrofitting with carbon-capture equipment; i.e., they will be designed so that they are “carbon-capture ready”.
Hitherto, steam turbines for power plants have normally been built to operate for their entire life on a particular thermodynamic cycle, as shown in German patent no. DE 628 830 C. However, depending on the carbon capture measures adopted, retrofitting of power plants with carbon capture equipment will necessitate modification of their steam turbines. An object of the present invention is therefore to provide steam turbines that are readily modifiable after design and manufacture to accommodate, at minimum expense, the demands of carbon-capture equipment added to the power generation plant at a later date.
A steam turbine is provided that is configured to facilitate post-modification for operation in a carbon capture mode as part of a power plant incorporating carbon-capture facilities. The turbine includes a turbine rotor, a turbine casing and a plurality of turbine stages. In an original configuration of the turbine, the turbine rotor and turbine casing are each longer, by respective lengths, than is necessary to accommodate the plurality of turbine stages. The lengths are sufficient to accommodate at least one further turbine stage at an exit of the turbine during the post-modification, such that after modification, the turbine will operate with an increased expansion ratio and an increased volumetric flow rate at its exit.
The disclosure also deals with a power plant that is configured to facilitate post-modification for operation in a carbon capture mode as part of a power plant incorporating carbon-capture facilities. The power plant includes a steam turbine that has a turbine rotor, a turbine casing and a plurality of turbine stages. In an original configuration of the turbine, the turbine rotor and turbine casing are each longer, by respective lengths, than is necessary to accommodate the plurality of turbine stages. The lengths are sufficient to accommodate at least one further turbine stage at an exit of the turbine during the post-modification, such that after modification, the turbine will operate with an increased expansion ratio and an increased volumetric flow rate at its exit. The steam turbine is an intermediate pressure steam turbine operable to receive steam from a high pressure steam turbine and deliver steam to a low pressure steam turbine at a first volumetric flow rate.
The disclosure further deals with a carbon-capture-ready power plant that includes a boiler and a steam turbine having a plurality of stages. To facilitate post-construction modification of the power plant to incorporate a carbon capture process that requires process steam, the steam turbine is longer than is necessary to accommodate the plurality of turbine stages by an extra length sufficient to accommodate at least one further turbine stage at the exit of the turbine during the post-construction modification. After modification, the turbine is operable with an increased expansion ratio and an increased volumetric flow rate at its exit, thereby allowing steam to be bled from the turbine exit to supply the required process steam.
Exemplary embodiments of the invention will now be described, with reference to the accompanying drawings, in which:
According to the present disclosure, a carbon-capture-ready power plant includes a boiler and a steam turbine comprising a plurality of stages, wherein to facilitate post-construction modification of the power plant to incorporate a carbon capture process that requires process steam, the steam turbine is longer than is necessary to accommodate the plurality of turbine stages by an extra length sufficient to accommodate at least one further turbine stage at the exit of the turbine during the post-construction modification, such that after modification, the turbine is operable with an increased expansion ratio and an increased volumetric flow rate at its exit, thereby allowing steam to be bled from the turbine exit to supply the required process steam.
Preferably, the extra length is sufficient to accommodate at least two further turbine stages at the exit of the turbine. The extra length may be at least partially pre-adapted to accommodate the extra stage(s).
It is envisaged that the steam turbine should be an intermediate pressure steam turbine operable to receive steam from a high pressure steam turbine and deliver steam to a low pressure steam turbine at a first volumetric flow rate. After modification, the intermediate pressure steam turbine will be operable to deliver process steam at a second volumetric flow rate while delivering steam to the low pressure steam turbine at the first volumetric flow rate.
The present disclosure further embraces a steam turbine constructed to facilitate later modification for operation in a carbon capture mode as part of a power plant incorporating carbon-capture facilities, the turbine comprising:
a turbine rotor;
a turbine casing; and
a plurality of turbine stages;
wherein in an initial as-manufactured condition of the turbine, the turbine rotor and turbine casing are each longer—by respective lengths r and c—than is necessary to accommodate the plurality of turbine stages, the lengths r and c being sufficient to accommodate at least one further turbine stage at the exit of the turbine during the later modification, such that after modification, the turbine will operate with an increased expansion ratio and an increased volumetric flow rate at its exit.
Preferably, the extra lengths r and c are sufficient to accommodate at least two further turbine stages at the exit of the turbine. At the time of manufacture of the turbine, the extra lengths r and c of the turbine rotor and the turbine casing, respectively, may be adapted to accommodate the extra stage(s), or such adaptation may occur during the later modification of the turbine for carbon capture. It would of course be possible only partially to adapt the turbine rotor and the turbine casing at the time of manufacture and to complete the adaptation during later modification of the turbine.
Adaptation to accommodate the extra stage(s) may comprise features machined in the extra length r of the turbine rotor and/or the extra length c of the turbine casing to accommodate complementary features in the further turbine stage(s). In this case, a fairing should be provided on the turbine rotor and/or the turbine casing to avoid turbulence in the flow through the turbine due to the presence of unused features in the extra lengths of the turbine rotor and/or the turbine casing.
It should be understood that in a turbine according to the present invention, the prospective accommodation of extra turbine stages at some point in the future will necessitate appropriate dimensioning of other turbomachinery components during initial design and manufacture. Hence, the flow areas of the turbine casing and the turbine exit duct(s) must be designed to accommodate the largest volumetric flow rates that they will encounter after modification for carbon capture.
Each turbine stage in an axial flow turbine will comprise a fixed or stator blade and moving or rotor blade. The present invention is equally applicable to the disc and diaphragm type of turbine (so-called “impulse” turbines) and to the reaction type of turbine. In a reaction type of turbine, the static blades have outer portions fixed in the turbine casing and inner portions that sealingly confront the turbine rotor, the moving blades having root portions mounted in a drum-type turbine rotor and radially outer ends that sealingly confront the turbine casing. In a disc and diaphragm type of machine, inner and outer rings kinematically support the fixed blades, the outer rings being mounted in the turbine casing.
Briefly described, a preferred embodiment of the invention comprises a steam turbine for a carbon-capture ready fossil fuel power plant. The turbine includes an intermediate pressure (IP) turbine manufactured to operate with a particular expansion ratio and supply a low pressure turbine with a particular volumetric flow rate of steam. The IP turbine is manufactured with extra lengths in its rotor and casing to enable the later addition of extra turbine stages effective to increase the turbine's expansion ratio and volumetric flow rate at its exit without increasing its overall as-manufactured length. After addition of the extra stages, the resulting additional volumetric flow of process steam can be bled off from the exit of the IP turbine to service a post-combustion carbon-capture process, without affecting the ability of the IP turbine to supply the low pressure turbine with the original volumetric flow rate of steam.
Referring now to
IP turbine 10 comprises, inter alia, a turbine rotor 12, a turbine casing 14 and a number of turbine blade stages 16. In this particular case there are nine turbine stages 16, but of course there could be more or less stages according to the design requirements.
Each IP turbine stage 16 comprises a fixed blade 18 and moving blade 20. In the present example, the turbine is constructed as a disc and diaphragm type of turbine (often called an impulse type of turbine) and hence the fixed blades 18 are kinematically supported by inner and outer rings 22, 24, respectively, each outer ring 24 being mounted in an annular recess 25 in the turbine casing 14 and each inner ring 22 occupying an annular chamber 27 between successive disc rim or “head” portions 26 of the rotor 12 (divisions between individual discs are not shown, since the discs have been welded together during the rotor manufacturing process so that the rotor is a single unit). The radially inner surfaces of the inner rings 22 sealingly confront portions of the outer rotor surface that lie between the disc head portions 26. As well known in the industry, labyrinth seals, brush seals, or the like (not shown), may be provided to seal the gaps between the inner rings 22 and the rotor surface. Regarding the moving blades 20, in this particular design they have root portions 28 that are fixed to the disc rim portions 26 of the rotor 12 by a pinned root arrangement, as is also well known. The tips of the moving blades 20 are provided with shroud or cover portions 30, whose outer surfaces sealingly confront corresponding lands 32 on the turbine casing 14. Again, labyrinth seals, brush seals, or the like (not shown), may be provided to seal the gaps between the shrouds 30 and the lands 32.
As will be evident from
As can be seen from
Additional characteristics of the turbine of
In an alternative embodiment (not shown), adaptation of the rotor and casing necessary to accommodate the extra stages is deferred until modification for carbon capture becomes necessary. Hence, in this alternative embodiment, the extra lengths r and c would appear plain, being machined down only to the rotor outer profile and the casing inner profile, respectively. To avoid completely the need for separate inner and outer diffuser rings acting as fairings, it would be possible to machine the extra lengths r and c of the rotor and stator so that the rotor's outer profile and the casing's inner profile comprise the necessary diffusing profiles of the turbine exit.
Whereas the above description with reference to
Referring back to
It should be understood that provision for the addition of two turbine stages in
Although
Several advantages are achievable by the present invention:
The present invention has been described above purely by way of example, and modifications can be made within the scope of the invention as claimed. The invention also consists in any individual features described or implicit herein or shown or implicit in the drawings or any combination of any such features or any generalisation of any such features or combination, which extends to equivalents thereof. Thus, the breadth and scope of the present invention should not be limited by any of the above-described exemplary embodiments. Each feature disclosed in the specification, including the claims and drawings, may be replaced by alternative features serving the same, equivalent or similar purposes, unless expressly stated otherwise.
Unless the context clearly requires otherwise, throughout the description and the claims, the words “comprise”, “comprising”, and the like, are to be construed in an inclusive as opposed to an exclusive or exhaustive sense; that is to say, in the sense of “including, but not limited to”.
Number | Date | Country | Kind |
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0616832.2 | Aug 2006 | GB | national |
This application is a continuation of International Application No. PCT/EP2007/058772 filed Aug. 23, 2007, which claims priority to Great Britain Application No. 0616832.2 filed Aug. 25, 2006, the contents of both of which are incorporated by reference as if fully set forth.
Number | Name | Date | Kind |
---|---|---|---|
4221114 | Wilde et al. | Sep 1980 | A |
6783321 | Lathrop et al. | Aug 2004 | B2 |
6865893 | Koganezawa et al. | Mar 2005 | B2 |
20030192516 | Brunemann et al. | Oct 2003 | A1 |
20050069411 | Bast et al. | Mar 2005 | A1 |
20050118025 | Hiegemann et al. | Jun 2005 | A1 |
Number | Date | Country |
---|---|---|
628830 | Apr 1936 | DE |
1038838 | Sep 1958 | DE |
1055809 | Nov 2000 | EP |
1055879 | Nov 2000 | EP |
1116779 | Jun 1968 | GB |
1258099 | Dec 1971 | GB |
1362799 | Aug 1974 | GB |
79228 | Jun 1949 | NL |
WO 03060292 | Jul 2003 | WO |
Number | Date | Country | |
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20090175722 A1 | Jul 2009 | US |
Number | Date | Country | |
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Parent | PCT/EP2007/058772 | Aug 2007 | US |
Child | 12391455 | US |