阅读说明：本技术 具有流动构造体的煤喷嘴 (Coal nozzle with flow structure ) 是由 迈克尔·萨帕纳罗 威廉·P·贝利 杰森·杰瑞米·韦尔古姆 约瑟夫·霍尔斯道姆 于 2018-07-26 设计创作，主要内容包括：本发明涉及一种粉状固体燃料喷嘴(10),特别是煤喷嘴,包括用于接纳煤/空气混合物的料流(16)的入口开口(12)以及用于将该料流(16)排放到燃烧器中的出口开口(14)。入口开口(12)和出口开口(14)通过流动部分(18)以流体方式连接,并且流动部分(18)的流动横截面(20)沿煤/空气混合物的料流(16)的流动方向(22)变化。流动部分(18)包括流动构造体(24),该流动构造体具有优先地全局的最小流动横截面(26)。流动构造体(24)以流体方式定位在该入口开口(12)和该出口开口(14)之间,并且该流动部分(18)具有流动横截面(20),该流动横截面特别是连续地从该流动构造体(24)到该出口开口(14)增大。(The invention relates to a pulverized solid fuel nozzle (10), in particular a coal nozzle, comprising an inlet opening (12) for receiving a stream (16) of a coal/air mixture and an outlet opening (14) for discharging the stream (16) into a burner. The inlet opening (12) and the outlet opening (14) are fluidically connected by a flow section (18), and the flow cross section (20) of the flow section (18) varies in the flow direction (22) of the stream (16) of the coal/air mixture. The flow portion (18) comprises a flow structure (24) having a preferably global minimum flow cross section (26). A flow arrangement (24) is positioned in a fluid manner between the inlet opening (12) and the outlet opening (14), and the flow portion (18) has a flow cross section (20) which increases in particular continuously from the flow arrangement (24) to the outlet opening (14).)

1. Pulverized solid fuel nozzle (10), in particular a coal nozzle, comprising an inlet opening (12) for receiving a stream (16) of a coal/air mixture and an outlet opening (14) for discharging the stream (16) into a burner, wherein the inlet opening (12) and the outlet opening (14) are fluidly connected by a flow section (18), wherein a flow cross-section (20) of the flow section (18) varies in a flow direction (22) of the stream (16) of the coal/air mixture, and wherein the flow section (18) comprises a flow configuration (24) having a preferably global minimum flow cross-section (26), characterized in that the flow configuration (24) is fluidly positioned between the inlet opening (12) and the outlet opening (14), and in that the flow section (18) has a flow cross section (20) which increases, in particular continuously, from the flow arrangement (24) to the outlet opening (14).

2. Nozzle (10) according to claim 1, characterized in that the flow section (18) comprises a first expansion section (28) and a second expansion section (30) fluidly positioned between the flow construct (24) and the outlet opening (14), wherein the rate of change of the flow cross section (20) of the first expansion section (28) is higher than the rate of change of the flow cross section of the second expansion section (30).

3. Nozzle (10) according to claim 1 or 2, characterized in that the first expansion section is arranged before the second expansion section (30) in the flow direction (22), preferably wherein the first expansion section (28) adjoins the second expansion section (30).

4. Nozzle (10) according to one of the preceding claims, characterized in that the flow cross section (20) of the first expansion section (28) and/or the second expansion section (30) increases in proportion to the square of the respective extension in the flow direction (22) of the first expansion section (28) and/or the second expansion section (30).

5. Nozzle (10) according to one of the preceding claims, characterized in that the cross-sectional area of the flow cross-section (20) of the flow portion (18) has a circular shape at least locally, preferably along its entire length.

6. Nozzle (10) according to one of the preceding claims, characterized in that an igniter (68) is positioned in the flow portion (18) of the nozzle (10), preferentially between the flow construct (24) and the outlet opening (14).

7. Nozzle (10) according to one of the preceding claims, characterized in that the wall (38) of the flow section (18) of the nozzle (10) between the flow structure (24) and the outlet opening (14) is coated at least locally, preferentially along its entire extension in the flow direction (22), with a coating (70) comprising a catalyst (72) adapted to catalyze the reaction of coal with oxygen.

8. Nozzle (10) according to one of the preceding claims, characterized in that the nozzle (10) comprises a cooling device (32), wherein the cooling device (32) is preferentially arranged in the flow direction (22) at least also between the flow construct (24) and the outlet opening (14).

9. Nozzle (10) according to the preceding claim, characterized in that the cooling device (32) comprises a fluid, in particular a liquid, coolant jacket (34), preferably wherein the coolant jacket (34) surrounds the wall of the flow section (18), at least also between the flow arrangement (24) and the outlet opening (14), and/or wherein the coolant jacket (34) surrounds the wall (38) of the flow section (18), before and after the flow arrangement (24), and/or wherein the coolant jacket (34) extends in flow direction (22) from before the flow arrangement (24) to close to the outlet opening (14).

10. Nozzle (10) according to one of the two preceding claims, characterized in that the nozzle (10) comprises at least one coolant supply line (42) having an inlet (44) close to the inlet opening (12) of the nozzle (10) and an outlet (46) into the coolant jacket (34), wherein the outlet (46) is preferably positioned in the vicinity of the outlet opening (14) of the nozzle (10).

11. Nozzle (10) according to one of the two preceding claims, characterized in that the coolant jacket (34) comprises a thermal expansion compensation joint (50) for compensating for different thermal expansions of different sections of the nozzle (10) due to an uneven temperature distribution along the nozzle (10) during operation.

12. Nozzle (10) according to the preceding claim, characterized in that the thermal expansion compensation joint (50) comprises a bellows (52).

13. Nozzle (10) according to one of the preceding claims, characterized in that the nozzle (10) comprises a pivoting mechanism (74) which allows the outlet opening (14) to pivot relative to the inlet opening (12).

14. Nozzle (10) according to one of the preceding claims, characterized in that the nozzle (10) comprises a cylindrical section (54) and a converging conical section (56) following the cylindrical section (54) in flow direction (22), and a first diverging conical section (58) following the converging conical section (56) in flow direction (22), and a second diverging conical section (60) following the first diverging conical section (58) in flow direction (22), wherein the first diverging conical section (58) has a first divergence angle (62) which is higher than a second divergence angle (64) of the second diverging conical section (60).

15. Nozzle (10) according to one of the preceding claims, characterized in that the flow portion (18) is located at least between the flow arrangement (24) and the outlet opening (14), preferably along its entire length, without an insert.

Background

The present invention relates to pulverized solid fuel nozzles, in particular coal nozzles, which can be applied in burners for burning pulverized coal, wherein the nozzles are designed in such a way that the formation of nitrogen oxides during the combustion process is minimized.

Disclosure of Invention

It is an object of the present invention to provide a pulverized solid fuel nozzle, in particular a coal nozzle, which allows clean combustion of pulverized coal, in particular low NOx combustion of coal. Another object is that the nozzle is simple in construction and has a high service life.

This object is achieved with a pulverized solid fuel nozzle, in particular a coal nozzle, according to claim 1.

The pulverized solid fuel nozzle, particularly a coal nozzle, according to the present invention is a nozzle for solid fuel injection, comprising an inlet opening for receiving a stream of a coal/air mixture and an outlet opening for discharging said stream into a burner, wherein the inlet opening and the outlet opening are fluidically connected by a flow section, wherein the flow cross section of the flow section varies in the flow direction of the coal/air mixture, and wherein the flow portion comprises a flow construct having a preferentially global minimum flow cross-section, characterized in that a flow arrangement is positioned in a fluid manner between the inlet opening and the outlet opening, and in that the flow portion has a flow cross-section which increases from the flow arrangement to the outlet opening. Optionally, the flow portion has a flow cross-section which continuously increases for at least 50% of the extension of the flow portion between the flow structure and the outlet opening, in particular for at least 60% of the extension of the flow portion between the flow structure and the outlet opening, in particular for at least 80% of the extension of the flow portion between the flow structure and the outlet opening. Optionally, the portion of the flow portion having a continuously increasing flow cross section is an uninterrupted portion of the flow portion. Optionally, the flow section has a flow cross-section that increases continuously over the entire extension of the flow section between the flow arrangement and the outlet opening.

A mixture of pulverized coal and air is blown into the inlet opening of the nozzle and then flows in the flow direction along the flow section. When the stream of coal/air mixture reaches the flow structure, the gas stream is at its maximum flow velocity. When the stream of coal/air mixture has passed through the flow structure, its flow velocity decreases due to the increase in the flow cross section. This reduction in flow velocity allows the flame to propagate into the nozzle. Thus, during operation of the nozzle, a flame front is located within the nozzle, which provides favorable combustion conditions for the volatile substances in the fuel. Coal can ignite in a fuel-rich environment, and volatile matter in the fuel can be burned off, so that chemicals can be produced that reduce NOx produced via the later stages of combustion.

Optionally, the flow section comprises a first expanded section and a second expanded section fluidly positioned between the flow construct and the outlet opening, wherein the first expanded section has a higher rate of change of flow cross-section than the second expanded section. The described embodiment with two expanded sections provides preferred flow characteristics such that the flame front is located within the nozzle, but does not propagate beyond the flow structure.

Optionally, the first expanded portion is arranged before the second expanded portion in the flow direction, preferably wherein the first expanded portion abuts the second expanded portion. By this arrangement, a rapid reduction of the flow velocity of the stream of coal/air mixture to the passing flow configuration is achieved.

Optionally, the flow cross-section of the first expanded portion and/or the second expanded portion increases in proportion to the square of the respective extension in the flow direction of the first expanded portion and/or the second expanded portion. This is achieved, for example, if the respective expansion section has a circular cross section and the diameter of the cross section increases linearly with the extent in the flow direction. The increase in the flow cross section leads to advantageous flow characteristics in the nozzle.

Optionally, the flow cross-section of the flow portion has a circular shape at least locally, preferably along its entire length. By this shape the nozzle can be easily manufactured, while the circular shape of the cross-section is advantageous for the flow characteristics, in particular the increase of the flow cross-section in combination with the circular shape of the cross-section requires flow characteristics that are advantageous for improving the propagation of the flame into the nozzle.

Optionally, the igniter is located in the flow portion of the nozzle, preferentially between the flow construct and the outlet opening. In this way, the stream of coal/air mixture can be directly ignited in the new model, and the operation and all the flow characteristics of the nozzle are such that the flame front is located within the nozzle.

Optionally, the wall of the flow portion of the nozzle between the flow structure and the outlet opening is coated at least partially, preferably along its entire extension in the flow direction, with a coating comprising a catalyst suitable for catalyzing the reaction of coal with oxygen. Thereby enhancing the combustion of the coal and promoting the location of the flame front within the nozzle.

Optionally, the nozzle comprises a cooling device, wherein the cooling device is preferentially arranged in the flow direction at least also between the flow arrangement and the outlet opening. By heating of this material, the nozzle can be kept at a lower temperature and the service life of the nozzle is increased. The location of the flame front within the nozzle results in a higher degree of heating of the nozzle assembly compared to operation of the nozzle in which the flame front is located outside the nozzle, so that the implementation of the above-described cooling means is particularly advantageously combined with the location of the flame front within the nozzle. Such cooling means may be cooling fins or channels through which a cooling medium is supplied to the area of the nozzle intended to be cooled. Optionally, there may be gas blown around the nozzle to effect cooling from outside the nozzle.

Optionally, the cooling device comprises a fluid, in particular a liquid, coolant jacket, preferably wherein the coolant jacket surrounds the wall of the flow section, at least also between the flow configuration and the outlet opening, and/or wherein the coolant jacket surrounds the wall of the flow section, before and after the flow configuration, and/or wherein the coolant jacket extends in the flow direction from before the flow configuration to the outlet opening. Such a coolant jacket allows surrounding the component to be cooled with a fluid coolant. Preferably, the coolant jacket is designed to contain a liquid coolant. The use of a liquid coolant provides the benefit of a high cooling rate due to the generally high specific heat capacity of the liquid. Such a liquid coolant may be water that provides the benefits of low cost, universal availability, and high specific heat capacity.

Optionally, the coolant jacket has a coolant flow direction opposite to the flow direction of the stream of the coal/air mixture. Hereby is achieved that the coolant and its coldest state are in contact with the hottest part of the nozzle, so that an advantageous heat transfer rate is obtained.

Optionally, the nozzle comprises at least one coolant tube having an inlet proximate to the inlet opening of the nozzle and an outlet into the coolant jacket, wherein the outlet is preferably located proximate to the outlet opening of the nozzle. Thereby, coolant can be introduced into the coolant tube close to the inlet opening, wherein the temperature is within reasonable boundaries during operation of the nozzle, and then the coolant is conveyed via the coolant tube to the outlet opening, wherein intensive cooling of the nozzle is beneficial.

Optionally, the coolant jacket comprises a thermal expansion compensation joint for compensating for different thermal expansions of different sections of the nozzle due to non-uniform temperature distribution along the nozzle during operation. When viewed from the inlet opening to the outlet opening of the nozzle during operation of the nozzle, there may be a strong temperature gradient such that the nozzle is deformed unevenly along its extent. The thermal expansion compensation joint is configured such that it can accommodate varying rates of thermal expansion of various portions of the nozzle, which facilitates the useful life of the nozzle, particularly the coolant jacket.

Optionally, the thermal expansion compensation joint comprises a bellows. In this way, the thermal expansion compensation joint can be manufactured in a straightforward and cost-effective manner, so that cooling based on liquid coolant can be realized in the nozzle with limited expenditure. Furthermore, such bellows provide a high degree of flexibility and thus can accommodate large differences in thermal expansion of different components.

Optionally, the nozzle comprises a pivoting mechanism that allows the outlet opening to pivot relative to the inlet opening. Through the direction of flow of such a coal/air mixture or under ignition conditions, the flame exiting the nozzle may be directly desired, while the attachment of the nozzle may be stationary.

Optionally, the nozzle comprises a cylindrical section, and a converging conical section following the cylindrical section in the flow direction, and a first diverging conical section following the converging conical section in the flow direction, and a second diverging conical section following the first diverging conical section in the flow direction, wherein the first diverging conical section has a higher divergence angle than the second diverging conical section. Optionally, two (preferably all) of the above sections of the nozzle abut a respective previous section. This results in an easily implementable design of the nozzle. Such nozzles can be manufactured using readily available components and are therefore inexpensive to construct and highly durable.

Optionally, the flow section is at least between the flow construct and the outlet opening, preferably along its entire length, without an insert. This allows an advantageous flow distribution in the nozzle. By non-insert is meant a flow portion or a portion thereof where there are no inserts in the cross-section of the flow portion that would cause a significant abrupt change in the cross-sectional area of the flow portion.

Drawings

FIG. 1: a perspective view of a nozzle according to the present invention;

FIG. 2: a side view of the nozzle of FIG. 1; and is

FIG. 3: the cross-sectional view of the nozzle of figures 1 and 2,

FIG. 4: an alternative embodiment of the nozzle in the view of FIG. 3;

FIG. 5: an alternative embodiment of the nozzle in the view of FIG. 3; and is

FIG. 6: an alternative embodiment of the nozzle in the view of fig. 3.

Detailed Description

Fig. 1 shows a perspective view of a nozzle 10 for solid fuel injection according to the present invention. The nozzle 10 includes an inlet opening 12 and an outlet opening 14.

The inlet opening 12 is for receiving a stream 16 of a coal/air mixture indicated symbolically via an arrow. The outlet opening 14 is used for discharging the stream 16 into a not shown burner.

The inlet opening 12 and the outlet opening 14 are fluidly connected by a flow portion 18, as shown in fig. 3. The flow cross section 20 of the flow section 18 varies in the flow direction 22 of the stream 16 of the coal/air mixture. The flow section 18 comprises a flow structure 24 which, in the embodiment of the figures, has a global minimum flow cross-section 26, i.e. the flow cross-section 20 has its minimum at the minimum flow cross-section 26. The flow arrangement 24 is fluidly positioned between the inlet opening 12 and the outlet opening 14, i.e. the stream 16 of the coal/air mixture first passes through the inlet opening 12, then through the flow arrangement 24, then through the outlet opening 14. The flow cross section 20 of the flow portion 18 increases from the flow structure 24 to the outlet opening 14. In the present embodiment, the flow cross section 20 of the flow section 18 continuously increases over the entire extension of the flow section 18 from the flow arrangement 24 to the outlet opening 14.

The flow portion 18 includes a first expanded portion 28 and a second expanded portion 30 fluidly positioned between the flow formation 24 and the outlet opening 14. The rate of change of the flow cross-section 20 of the first expanded portion 28 is higher than the rate of change of the flow cross-section 20 of the second expanded portion 30. The first expansion section 28 is arranged before the second expansion section 30 in the flow direction and is adjoined later.

The flow cross-section 20 of the first and second expanded portions 28, 30 increases in the flow direction 22 in proportion to the square of the respective extension, because the cross-sectional area of the flow cross-section 20 in each of the expanded portions 28, 30 is circular and the diameter of the circular cross-sectional area increases in proportion to the extension in the flow direction 22.

The nozzle 10 comprises a cooling device 32 which in the present embodiment is realized as a coolant jacket 34. The cooling device 32, i.e. the coolant jacket 34, is also arranged at least between the flow structure 24 and the outlet opening 14 in the flow direction. More specifically, the coolant jacket extends from before the flow construct 24 along the extension of the nozzle 10 until proximate the outlet opening 14.

The coolant jacket 34 is configured to contain a liquid coolant 36 indicated symbolically via arrows. The coolant jacket 34 surrounds a wall 38 of the flow portion 18. The coolant jacket 34 extends in this surrounding manner in the flow direction 22 from before the flow structure 24 to the vicinity of the outlet opening 14.

The coolant jacket 34 is configured such that the coolant flow direction 40 within the coolant jacket 34 is opposite the flow direction 22 of the stream 16 of the coal/air mixture.

The nozzle 10 includes several coolant supply lines 42 in the form of tubes. The coolant supply lines 42 each have an inlet 44 near the inlet opening 12 of the nozzle 10 and an outlet 46 into the coolant jacket 34, with the outlet 46 being located near the outlet opening 14 of the nozzle 10. The coolant 36 exits the coolant jacket 34 coolant outlet line 48. In the present embodiment, the coolant jacket 34 is adapted and arranged to function with water as the coolant 36. The use of other liquids as the coolant 36 is possible and within the scope of the present invention.

The coolant jacket 34 includes a thermal expansion compensation joint 50 that is used to compensate for the different thermal expansions of the different sections of the nozzle 10 due to the non-uniform temperature distribution along the nozzle 10 during operation.

The thermal expansion compensation joint 50 in turn comprises a bellows 52.

The nozzle in the current embodiment includes a cylindrical section 54, and a converging conical section 56 aft of the cylindrical section 54 in the flow direction 22, and a first diverging conical section 58 aft of the converging conical section 56 in the flow direction 22, and a second diverging conical section 60 aft of the first diverging conical section 58 in the flow direction 22, wherein the first diverging conical section 58 has a first divergence angle 62 that is higher than a second divergence angle 64 of the second diverging conical section 60.

In the present embodiment, the flow portion 18 is plug-less. By non-insert is meant a flow portion 18 or a portion thereof in which there are no inserts in the cross-section of the flow portion 18 that would cause a significant abrupt change in the cross-sectional area of the flow portion 18. As can be seen in fig. 3, there is a thermal element 66 that extends into the flow section 18. However, the size of the thermal elements 66 is so small that they do not cause a significant abrupt change in the cross-sectional area of the flow section 18. They are therefore not considered to constitute inserts within the meaning of the present invention. However, a static or dynamic mixer arranged in the flow section 18 will be considered to constitute an insert within the meaning of the present invention.

Fig. 4 shows an embodiment of a construction similar to the embodiment of fig. 1 to 3. In the embodiment of fig. 4, the nozzle 10 additionally includes an igniter 68 (shown schematically) located in the flow portion 18 of the nozzle 10. More specifically, in this embodiment, the igniter 68 is located between the flow construct 24 and the outlet opening 14.

Fig. 5 shows an embodiment of a construction similar to the embodiment of fig. 1-3. In the embodiment of fig. 5, the wall 38 of the flow portion 18 of the nozzle 10 between the flow construct 24 and the outlet opening 14 is coated with a coating 70 (shown schematically) comprising a catalyst 72 suitable for catalyzing the reaction of coal with oxygen.

Fig. 6 shows an embodiment of a construction similar to the embodiment of fig. 1-3. In the embodiment of fig. 6, the nozzle includes a pivot mechanism 74 (shown schematically) that allows the outlet opening 14 to pivot relative to the inlet opening 12.

It is apparent that it is within the scope of the present invention to combine the igniter 68 with the coating 70 and/or the pivot mechanism 74, or to combine the coating 70 with the pivot mechanism 74.

In operation of the above embodiment, a stream 16 of a coal/air mixture is blown into the inlet opening 12 and then propagates through the flow structure 24 along the nozzle 10 and subsequently reduces its flow velocity. Either the stream 16 of coal/air mixture is ignited by the igniter 68 and the flame front is already located in the nozzle 10 as a result of this ignition and remains there as a result of the reduction in flow velocity behind the flow structure 24, or the stream 16 of coal/air mixture is ignited outside the nozzle 10, i.e. after it has passed through the outlet opening 14. In the latter case, due to the reduced flow velocity behind the flow structure 24, a flame front propagates into the nozzle 10 and is maintained between the flow structure 24 and the outlet opening 14 during operation of the nozzle 10.

Because the flame front is located within the nozzle 10, combustion of the coal or other solid fuel begins in a fuel rich environment. This combustion in a fuel rich environment produces chemicals that are transported with the stream 16 of already combusted coal/air mixture and reduces the formation of NOx during combustion occurring outside the nozzle 10. This results in a total of significantly reduced NOx formation during combustion of stream 16 of the coal/air mixture.

Secondary air may be blown along the exterior of the nozzle 10 and may enhance the combustion process.

The coating 70 containing the catalyst 72, if present, facilitates the location of the flame front within the nozzle 10 as it reduces the amount of energy required to initiate the reaction between the coal and oxygen (i.e., the burning of the coal).

List of reference numerals

10 nozzle

12 inlet opening

14 outlet opening

16 coal/air mixture stream

18 flow section

20 flow cross section

22 direction of flow

24 flow structure

26 minimum flow cross section

28 first expansion section

30 second expansion section

32 cooling device

34 coolant jacket

36 liquid coolant

38 wall of the flow section

40 direction of coolant flow

42 coolant supply line

44 inlet

46 outlet

48 coolant outlet line

50 thermal expansion compensation joint

52 corrugated pipe

54 cylindrical section

56 converging conical section

58 first diverging conical section

60 second diverging conical section

62 first divergence angle

64 second divergence angle

66 thermal element

68 igniter

70 coating layer

72 catalyst

74 pivoting mechanism