GB2330648A - Domestic boiler heated by gas turbine - Google Patents
Domestic boiler heated by gas turbine Download PDFInfo
- Publication number
- GB2330648A GB2330648A GB9722412A GB9722412A GB2330648A GB 2330648 A GB2330648 A GB 2330648A GB 9722412 A GB9722412 A GB 9722412A GB 9722412 A GB9722412 A GB 9722412A GB 2330648 A GB2330648 A GB 2330648A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- boiler
- heat exchanger
- arrangement
- heat
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000010438 heat treatment Methods 0.000 claims abstract description 26
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 8
- 239000003345 natural gas Substances 0.000 claims abstract description 4
- 239000000446 fuel Substances 0.000 claims description 2
- 239000007788 liquid Substances 0.000 claims description 2
- 239000007789 gas Substances 0.000 abstract description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 8
- 238000002485 combustion reaction Methods 0.000 abstract description 2
- 239000000203 mixture Substances 0.000 abstract description 2
- 239000000969 carrier Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000005201 scrubbing Methods 0.000 description 3
- 238000011084 recovery Methods 0.000 description 2
- 238000013022 venting Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
- F24H1/00—Water heaters, e.g. boilers, continuous-flow heaters or water-storage heaters
- F24H1/0027—Water heaters, e.g. boilers, continuous-flow heaters or water-storage heaters using fluid fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/60—Application making use of surplus or waste energy
- F05D2220/64—Application making use of surplus or waste energy for domestic central heating or production of electricity
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Air Supply (AREA)
Abstract
The heat exchanger 200 of a boiler for central heating and domestic hot water is heated by one or more gas turbines 100. When demand for heat is established, an electric motor 300 drives the turbine wheels 130 up to operating speed. Air is drawn in through inlet 102, compressed by vanes on carriers 104, 106 and passed to combustion chamber 120 where it mixes with natural gas supplied through injectors 122. The gas and air mixture is ignited, expands and is forced past turbine wheel 130 towards exit cone 140. A clearance of 5 mm between turbine wheel 130 and housing 124 develops heat rather than thrust. The exit cone 140 develops the flame pattern and guides it into the heat exchanger 200. The heat exchanger 200 comprises three layers of finned tubing bent to form a plurality of parallel sections, and is coupled to a central heating system or hot water supply.
Description
HEATING ARRMNGEMENZ The present invention relates to a heating arrangement and, in the preferred embodiment, to a heating arrangement for a domestic boiler.
In the example of a domestic boiler, having a capacity in the range of about 30,000 to 110,000 BTU, a heat exchanger is arranged over a heat source such as a gas burner in order to heat water passing through the heat exchanger. The heated water is then coupled to heat a hot water supply or a central heating system. Despite elements such as condensing boilers, known heating arrangements are inefficient and allow up to 65 % of the input energy to be unrecovered.
It is an aim of the present invention to provide a compact and efficient heating arrangement.
According to the present invention there is provided a heating arrangement such as for a domestic boiler, comprising a turbine arrangement for heating air passing therethrough.
The turbine arrangement operates on the well known principle developed through the use of turbines in aircraft engines and large scale power generation. However, the aim of the prior art turbine arrangement is to output thrust, whereas the preferred turbine arrangement outputs heat and minimal thrust.
Preferably, the turbine arrangement comprises a turbine fan rotatably mounted within a housing. The clearance between the turbine fan and the housing is usually desired to be as small as possible in order to generate maximum thrust. Conversely, it is preferred that the clearance be relatively large, of the order of 5 mm, in order to provide maximum heat output with sufficient thrust to provide an operational turbine arrangement.
According to a second aspect of the present invention there is provided a boiler comprising a heat exchanger for transferring heat energy between a gas and a liquid, and a turbine arrangement for generating heated gas directed at said heat exchanger.
Preferably, the turbine arrangement runs on a dry fuel, preferably natural gas.
According to a further embodiment of the present invention there is provided a heat exchanger having a plurality of layers arranged substantially co-planar.
Preferably, each layer comprises an elongate tube bent to form a plurality of parallel sections, and preferably the sections of each adjacent layer are offset with respect to each other. Further, the heat exchanger preferably comprises a plurality of fins for directing air through the heat scrubber. Each fin preferably comprises a planar sheet having parallel ribs formed laterally thereacross and holes therethrough for heat recovery and air scrubbing. Each fin preferably has a deflector arranged at around 45" to the plane thereof, for directing air across the fin. Ideally, up to around 80 fins are provided across the heat exchanger arranged parallel to the incoming air flow and perpendicular to the heat exchanger layers.
For a better understanding of the invention, and to show how embodiments of the same may be carried into effect, reference will now be made, by way of example, to the accompanying diagrammatic drawings, in which:
Figure 1 is a schematic sectional view of a turbine arrangement;
Figure 2 is a plan view of a preferred heating arrangement;
Figure 3 is an expanded schematic view of a heat exchanger;
Figure 4 is a front view of a fin; and
Figure 5 is a side view of a fin.
Referring firstly to Figure 1, a turbine arrangement is shown as will be familiar to persons skilled in the art, having an inlet 102, a front vane carrier 104 and a rear vane carrier 106 carrying front and rear vanes, respectively, for drawing in cold air and compressing and slowing the air. The compressed air is passed to a combustion chamber 120 having gas injectors and atomisers 122 introducing a combustible fluid preferably natural gas from a mains supply. The gas and air mixture is ignited and expands and thus is forced past turbine wheel 130 toward an exit cone 140.
The turbine wheel has been developed to produce heat rather than thrust by allowing a relatively large tolerance between the turbine and the surrounding housing 124. If the gap is too great, between the tip of the turbine wheel and the housing, then insufficient energy will be passed to the turbine wheel to sustain the turbine cycle.
The shape of the exit cone 140 significantly affects the flame pattern produced from the turbine wheel 130. The exit cone 140 develops the flame pattern and guides it into the heat exchanger.
Referring to Figure 2, two turbine heat generators 100 are shown arranged side by side and directed toward a heat exchanger 200. A electric motor 300 having a centrifugal clutch is coupled to each of the turbine heat generators 100 to drive the turbine wheels up to operating speed of about 28,000 rpm at start up.
Operation of the heating arrangement and boiler system is suitably controlled by a central control means including interlocking sensors and temperature sensors. When demand for heat is established, such as from a central heating arrangement or a domestic hot water arrangement, the electric motor is engaged to run the or each turbine wheel up to operating speed of about 28,000 rpm. Operating speed is achieved after about 4 seconds, and a valve in the gas supply is opened to supply gas at a first predetermined rate to gas injectors 122 of Figure 1. Once a sustained flame is detected such as by a suitably placed thermo-couple, the gas flow is increased to a second preset level. The speed of the turbine is dependent upon the volume of gas provided, and consequently increases in speed up to a maximum speed of around 80,000 rpm. In the preferred embodiment, full working system temperature is achieved within 4 to 5 minutes, and is continually monitored through heating control sensors. As the system attains working temperature, the volume of gas supplied is reduced to a rate between the first and second levels and the speed of the turbine consequently drops. Thus, the output of the heat generator can be easily varied to match demand.
In the preferred embodiment, a maximum desired operating output can be achieved within around 10 seconds from start up with the turbine running at around 85,000 rpm and producing an output of around 1010"C.
The heat exchanger will now be described in more detail with reference to Figures 3, 4 and 5. The heat exchanger 200 is suitably coupled to a central heating system or a hot water supply. The boiler can be set to operate on winter or summer settings according to variations in the incoming water temperature.
The heat exchanger 200 preferably comprises three layers to provide good thermal transfer efficiency. As may be seen in Figure 3, each layer comprises a tube 202, 203, 204 bent to form a plurality of parallel sections.
The middle tube is offset with respect to the top and bottom tubes such that air passing through the heat exchanger must pass around the tube.
Referring now to Figures 4 and 5, a plurality of fins, preferably of the order of eighty fins, are provided across the heat exchanger. Each fin 220 has a plurality of holes 221 therethrough and lateral ribs 222, for good heat recovery. The fins are preferably set with a minimum amount of clearance.
Relatively small gaps are required between the fins due to the relatively high velocity of the heated air exiting the turbine heat generator 100. As the air is moving over the fins at relatively high speed, the arrangement of holes 221, and ribs 222 increase friction to provide an air scrubbing effect which increases efficiency by around 5 to 7%. Each fin is provided with a deflector 223 arranged at around 45" for deflecting air across the fin, and for contributing to the air scrubbing effect.
The boiler and heat exchanger does not require a fan or other external venting source, because the residual velocity of the air exiting the heat exchanger is sufficient to ensure adequate venting. Also, relatively long runs of flue ducting may be installed.
The heating arrangement described herein has a number of advantages in that it is efficient and compact. In the preferred embodiment, a boiler is arranged to fit within the space available in a standard single wall unit of around 300 mm wide by 720 mm high by 280 mm deep. The heating arrangement is efficient with losses only in the region of 43 % . Emissions from the heating arrangement are clean and well within current UK and EU standards.
Referring again to Figure 2, where two heat generators 100 are shown arranged side by side, further units may be provided according to the heat output desired. For example, four generators may be provided giving a total output of around 250,000 BTU. Further improvements in the efficiency of each unit and/or the provision of further units show that the heating arrangement described herein is generally applicable in providing an output up to around 500,000 BTU.
The reader's attention is directed to all papers and documents which are filed concurrently with or previous to this specification in connection with this application and which are open to public inspection with this specification, and the contents of all such papers and documents are incorporated herein by reference.
All of the features disclosed in this specification (including any accompanying claims, abstract and drawings), and/or all of the steps of any method or process so disclosed, may be combined in any combination, except combinations where at least some of such features and/or steps are mutually exclusive.
Each feature disclosed in this specification (including any accompanying claims, abstract and drawings), may be replaced by alternative features serving the same, equivalent or similar purpose, unless expressly stated otherwise. Thus, unless expressly stated otherwise, each feature disclosed is one example only of a generic series of equivalent or similar features.
The invention is not restricted to the details of the foregoing embodiment(s). The invention extends to any novel one, or any novel combination, of the features disclosed in this specification (including any accompanying claims, abstract and drawings), or to any novel one, or any novel combination, of the steps of any method or process so disclosed.
Claims (10)
- CLAIMS 1. A heating arrangement for a domestic boiler, comprising a turbine arrangement for heating air passing therethrough.
- 2. A boiler as claimed in claim 1, wherein said turbine arrangement comprises a turbine fan rotatably mounted within a turbine housing.
- 3. A heating arrangement as claimed in claim 2, wherein a clearance between the turbine fan and the housing is arranged to provide maximum heat output and minimal thrust.
- 4. A heating arrangement as claimed in claim 3, wherein said clearance is of the order of 5mm.
- 5. A boiler comprising a heating arrangement as claimed in any of claims 1 to 4, and a heat exchanger for transferring heat energy from said heated air to a heat exchange liquid.
- 6. A boiler as claimed in claim 5, wherein said heat exchanger is arranged to lie directly in the path of heated air produced by said turbine arrangement.
- 7. A boiler as claimed in claim 6, wherein said turbine arrangement comprises an exit cone for defining a flame pattern of heated air exiting the turbine fan, said exit cone for directing said flame pattern toward said heat exchanger.
- 8. A heating arrangement or boiler as claimed in any preceding claim, wherein said turbine arrangement is powered by a dry fuel including natural gas.
- 9. A heating arrangement substantially as hereinbefore described with reference to Figure 1 of the accompanying drawings.
- 10. A boiler substantially as hereinbefore described with reference to Figures 1 to 5 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9722412A GB2330648A (en) | 1997-10-24 | 1997-10-24 | Domestic boiler heated by gas turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9722412A GB2330648A (en) | 1997-10-24 | 1997-10-24 | Domestic boiler heated by gas turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9722412D0 GB9722412D0 (en) | 1997-12-24 |
GB2330648A true GB2330648A (en) | 1999-04-28 |
Family
ID=10820988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9722412A Withdrawn GB2330648A (en) | 1997-10-24 | 1997-10-24 | Domestic boiler heated by gas turbine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2330648A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1048906A2 (en) * | 1999-04-28 | 2000-11-02 | Robert Pickering | Heat exchanger for a boiler |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1004139A (en) * | 1963-05-16 | 1965-09-08 | Centrax Ltd | Gas turbine power plants |
DE2539828A1 (en) * | 1975-09-08 | 1977-03-17 | Dotzenrath Wolfgang | Central heating system for individual houses - incorporates gas turbine between burner and heat exchanger to increase efficiency |
US4598542A (en) * | 1984-01-07 | 1986-07-08 | Rolls-Royce Limited | Gas turbine power plant |
GB2273340A (en) * | 1992-12-11 | 1994-06-15 | British Gas Plc | Combined heat and power apparatus |
WO1996037735A1 (en) * | 1995-05-26 | 1996-11-28 | Ecopower Technology Oy | Energy supply system for heat-delivering appliances used in private houses or apartments |
EP0799981A2 (en) * | 1996-04-04 | 1997-10-08 | Forschungszentrum Jülich Gmbh | Gas turbine heat and power plant |
-
1997
- 1997-10-24 GB GB9722412A patent/GB2330648A/en not_active Withdrawn
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1004139A (en) * | 1963-05-16 | 1965-09-08 | Centrax Ltd | Gas turbine power plants |
DE2539828A1 (en) * | 1975-09-08 | 1977-03-17 | Dotzenrath Wolfgang | Central heating system for individual houses - incorporates gas turbine between burner and heat exchanger to increase efficiency |
US4598542A (en) * | 1984-01-07 | 1986-07-08 | Rolls-Royce Limited | Gas turbine power plant |
GB2273340A (en) * | 1992-12-11 | 1994-06-15 | British Gas Plc | Combined heat and power apparatus |
WO1996037735A1 (en) * | 1995-05-26 | 1996-11-28 | Ecopower Technology Oy | Energy supply system for heat-delivering appliances used in private houses or apartments |
EP0799981A2 (en) * | 1996-04-04 | 1997-10-08 | Forschungszentrum Jülich Gmbh | Gas turbine heat and power plant |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1048906A2 (en) * | 1999-04-28 | 2000-11-02 | Robert Pickering | Heat exchanger for a boiler |
EP1048906A3 (en) * | 1999-04-28 | 2002-10-02 | Robert Pickering | Heat exchanger for a boiler |
Also Published As
Publication number | Publication date |
---|---|
GB9722412D0 (en) | 1997-12-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |