Patent Grant
9140449
This application is the US National Stage of International Application No. PCT/EP2009/051432 filed Feb. 9, 2009, and claims the benefit thereof. The International Application claims the benefits of European Patent Application No. 08002769.1 EP filed Feb. 14, 2008. All of the applications are incorporated by reference herein in their entirety.
The present invention relates to a burner element and a burner which are equipped with a corrosion-resistant insert.
Internally, particular parts of a burner typically come into contact with fuel. The chemical reaction of sulfur compounds (H2S) contained in the fuel with the base metal of the burner may cause iron sulfide scale to form inside the burner. The base metal of the burner is typically steel, e.g. 16Mo3 steel. The iron sulfide scale forming inside the burner may flake off and in some cases cause plugging of the holes through which the fuel is injected into a combustion chamber. The holes through which the fuel is injected into the combustion chamber are typically 1.5 mm in diameter. Plugging of said holes results in uneven combustion, thereby considerably worsening in particular the emission values of the burner in question. The availability of the burner affected or more specifically the associated combustion chamber is impaired in this case.
The problem of possible plugging of the holes as a result of flaking iron sulfide scale has hitherto been solved either by cleaning the burner or installing a new burner. However, cleaning is very time-consuming. In such cases, therefore, a complete set of new burners generally has to be installed which is very expensive. Although the problems described only occur on machines which are operated with pre-heating, these machines are being increasingly used. High additional costs resulting from the possible formation of iron sulfide scale are therefore to be expected.
In addition, the formation of in particular iron sulfide scale can be reduced by using corrosion-resistant materials such as IN617. However, these materials are much more expensive than the 16Mo3 steel used hitherto.
An object of the invention is to provide an advantageous burner element. Another object of the present invention is to provide an advantageous burner.
The objects are achieved by a burner element and a burner as claimed in the independent claims. The dependent claims contain further advantageous embodiments of the invention.
The burner element according to the invention comprises a surface which potentially comes into contact with a fuel. The burner element also comprises a base metal and a corrosion-resistant material, the surface potentially coming into contact with a fuel being made of said corrosion-resistant material. This prevents the formation of deposits, in particular of iron sulfide scale, on the surface potentially coming into contact with a fuel, thus ensuring compliance with emission limit values. It also enables the costs of cleaning or installing a new burner to be saved.
The base metal can be e.g. steel, in particular 16Mo3 steel. The corrosion-resistant material can be e.g. IN617. As it is only the surface potentially coming into contact with a fuel that is made of the corrosion-resistant and expensive material IN617, considerable cost savings can be made compared to a burner element made entirely from a corrosion-resistant material such as IN617.
The burner element according to the invention is implemented, for example, as a burner carrier flange. Furthermore, the burner carrier flange according to the invention comprises a base body comprising the base metal and an insert comprising the corrosion-resistant material.
In addition, the insert can comprise an outer surface and at least one opening. The base body can have an opening with an inner surface. In this case the insert can be disposed in the opening of the base body such that the inner surface of the opening of the base body is tightly connected to the outer surface of the insert. The insert can be e.g. welded into the base body.
In addition, the opening of the base body can be disposed eccentrically in the base body with respect to a central axis of the base body. Also the opening of the insert can be disposed eccentrically in the insert with respect to a central axis of the insert. The opening of the base body and/or the opening of the insert can have e.g. a circular cross section.
Using the burner carrier flange according to the invention, the fuel used can flow through the opening of the insert. As the insert is made of corrosion-resistant material, the fuel does not come into contact with the base metal, thereby preventing scale formation.
The burner according to the invention comprises an inventive burner element as described above. Said burner can be, for example, a pilot burner. The pilot burner can comprise, for example, nozzle holes one millimeter in diameter. The burner according to the invention basically has the same advantages as the described burner element according to the invention. With the aid of the present invention, the formation of deposits, in particular of iron sulfide scale, inside a burner can be inexpensively and effectively prevented. In addition, the present invention improves the emission values of the burner.
Further properties, features and advantages of the present invention will now be described in greater detail on the basis of an exemplary embodiment and with reference to the accompanying drawings in which:
An exemplary embodiment of the present invention will now be explained in greater detail with reference to
The graph shows the CO emission values for the burner in question over a period of time, subdivided into four sections I, II, III, IV. After a longer operating section I with extremely low emission values, the latter increased continuously in the second section II, but were mainly below 10 mg/m3. In the subsequent time section III, the CO emission values increased more strongly than in section II and were mainly between 10 and 30 mg/m3. In the fourth time section IV, CO emission values mainly between 40 and 80 mg/m3 were measured.
The measurement shown in
The design of a burner such as can be used e.g. as part of a gas turbine will now be explained in greater detail with reference to
The burner 1 comprises a housing 4. Inside said housing 4, a fuel oil return line 5 is disposed along the central axis 2. Disposed concentrically around said fuel oil return line 5 is a fuel oil feed line 6 which likewise runs along the central axis 2. There can also be a plurality of fuel oil feed lines 6 disposed concentrically around the fuel oil return line 5. On the side facing away from the combustion chamber 3, the fuel oil feed line 6 is connected to a connecting pipe 7 which can be connected to a fuel oil supply. The flow direction of the fuel oil is indicated by the arrows 8 and 9. The fuel oil can initially flow through the connecting pipe 7 into the fuel oil feed line 6. The fuel oil can flow through said fuel oil feed line 6 parallel to the central axis 2 in the direction of the combustion chamber 3 and be injected into said combustion chamber 3. Excess fuel oil can flow away from the combustion chamber 3 through the fuel oil return line 5 in a direction parallel to the central axis 2 as indicated by the arrow 9.
Along the central axis 2, one or more water lines 17 are disposed radially with respect to the central axis 2 outside the fuel oil return line 5 and the fuel oil feed line 6. The water line or lines 17 are connected to a water feed 16 on the side of the burner 1 facing away from the combustion chamber 3.
Fuel gas diffusion lines 10, 110 are disposed concentrically around the fuel oil return line 5, the fuel oil feed line 6 and the water lines 17. The fuel gas can be forwarded in the fuel gas diffusion lines 10, 110 to fuel nozzles 11. The fuel nozzles 11 are likewise disposed concentrically around the central axis 2 and enable the fuel to be injected into the combustion chamber 3.
Disposed radially with respect to the central axis 2 outside the fuel gas diffusion lines 10, 110 is a fuel gas pre-mixing supply line 12 through which the fuel gas can be fed to further fuel nozzles 13 via an annular distributor 18 disposed annularly around the central axis 2. The fuel can be injected into the combustion chamber 3 through the fuel nozzles 13. The flow direction of the fuel/air mixture in the combustion chamber 3 is indicated by arrows 14.
Reference character 30 indicates the position of the burner carrier flange. In particular the distribution of the fuel gas to the fuel gas diffusion lines 110 takes place in the burner carrier flange 30. The fuel gas diffusion lines 110 are implemented as pipes leading to the combustion chamber 3.
The inner surfaces of the burner carrier flange 30 are in direct contact with the fuel gas flowing through them. Because of the chemical reaction of sulfur compounds contained in the fuel gas with the base metal of these components, iron sulfide scale may form on the inner surfaces of the burner carrier flange 30. This scale can flake off, resulting in partial plugging of the fuel nozzles 11, 13.
The inner surface 32 of the opening 31 contains a groove 33 running along the circumference of the opening 31 and through which the fuel gas is conveyed to the fuel gas diffusion lines 110. The burner carrier flange 30 also contains a flow duct 36 which runs perpendicular to the central axis 35 and is fluidically connected to the groove 33. The flow duct 36 is also connected to an opening 34 which is disposed radially outside the opening 31 with respect to the central axis 35. Fuel gas can be fed into the groove 33 through the opening 34. The opening 34 has a central axis 37 which runs parallel to the central axis 35 of the burner carrier flange 30. The opening 34 has a smaller diameter than the opening 31.
The opening 31 also has an inner surface 32 which typically comes into contact with a fuel. This can be in particular the surface of the groove 33. Deposits such as iron sulfide scale can form on said inner surface 32 as the result of contact with the fuel.
The base body 21 has a circular cross section with a central axis 29. It also comprises a through-going opening 26 which is disposed eccentrically with respect to the central axis 29. The opening 26 has a drop-shaped cross section. The inner surface of the opening 26 is denoted by the reference character 24.
The insert 22 comprises an outer surface 25 which is designed such that the insert 22 can be inserted in the opening 26 of the base body 21 such that the inner surface 24 of the base body 21 is tightly connected to the outer surface 25 of the insert 22.
The insert 22 also comprises a through-going opening 23 which has a circular cross section and is disposed eccentrically with respect to the central axis 29. The inner surface of the opening 23 potentially coming into contact with a fuel is denoted by the reference character 28. The insert 22 also comprises an opening 27 which has the same characteristics as the opening 34 of the conventional burner carrier flange 30 described in connection with
The variant shown in
Inside the insert 22, the opening 23, which again has a circular cross section, is disposed eccentrically with respect to the central axis 41 of the insert 22. The other elements indicated in
Another variant of the inventive burner flange 50 is shown schematically in
By splitting the inventive burner carrier flange 20, 40, 50 into two in the form, of a base body 21 and an insert 22 which consist of different materials, the problem of scale formation can be inexpensively solved. In particular, the part of the burner carrier flange 20, 40, 50 potentially coming into contact with a fuel and therefore at risk of such scaling is made of a corrosion-resistant material such as IN617, and the remaining part, i.e. the base body 21, is made of an inexpensive material such as 16Mo3 steel.
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|---|---|---|---|
| 08002769 | Feb 2008 | EP | regional |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/EP2009/051432 | 2/9/2009 | WO | 00 | 1/7/2011 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2009/101043 | 8/20/2009 | WO | A |
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