US20140045128A1

US20140045128A1 - Combustion apparatus

Info

Publication number: US20140045128A1
Application number: US13/714,521
Authority: US
Inventors: Dae-hoon Lee; Kwan-Tae Kim; Young Hoon Song; Jae Ok Lee; Min Hur; Woo Seok Kang
Original assignee: Korea Institute of Machinery and Materials KIMM
Current assignee: Korea Institute of Machinery and Materials KIMM
Priority date: 2012-08-07
Filing date: 2012-12-14
Publication date: 2014-02-13
Also published as: KR101284290B1; JP5435381B2; ES2830039T3; CN103574600A; CN103574600B; EP2696140B1; JP2014035182A; EP2696140A3; EP2696140A2

Abstract

There is provided a combustion apparatus for reducing generation of NOx by securing more time for mixing fuel and air and uniformly mixing fuel and air.

The combustion apparatus includes: a modifying part configured in the center to modify supplied hydrocarbon-based fuel and air and discharge high temperature modified gas including hydrogen to an outlet; and a supply part configured at an outer side of the outlet to jet fuel and air to one side of the modified gas discharged from the modifying part to form a flame at a position spaced apart by a pre-set distance from the outlet.

Description

CROSS-REFERENCE TO RELATED APPLICATION

This application claims priority to and the benefit of Korean Patent Application No. 10-2012-0086479 filed in the Korean Intellectual Property Office on Aug. 7, 2012, the entire contents of which are incorporated herein by reference.

BACKGROUND OF THE INVENTION

(a) Field of the Invention
The present invention relates to a combustion apparatus for reducing generation of NOx by forming flame at a position distant from an outlet by jetting a gas including high temperature hydrogen generated by modifying hydrocarbon fuel.
(b) Description of the Related Art
A general combustion apparatus is configured to make supplied fuel and air meet in the interior or exterior to form a diffusion flame. Here, a generation rate of NOx (or generation of NOx) may differ according to a mixture degree and a mixture speed of fuel and air.
In order to reduce generation of NOx, a combustion apparatus for jetting air or fuel by multiple stages or performing fuel-rich combustion and lean combustion by several stages has been developed. However, multi-staged combustion lengthens flame and makes a structure of a combustion apparatus complicated.
In an effort to solve the problem, a combustion apparatus capable of reducing generation of NOx by mixing fuel and air rapidly has been developed. In this case, the combustion apparatus requires an ignitor (i.e., a lighter or a firer) for igniting flame, and a pilot flame for settling and stabilizing in a combustion apparatus should be formed in an outlet of the combustion apparatus. Namely, without the pilot flame, flame is blown out from the outlet of the combustion apparatus.
The above information disclosed in this Background section is only for enhancement of understanding of the background of the invention and therefore it may contain information that does not form the prior art that is already known in this country to a person of ordinary skill in the art.

SUMMARY OF THE INVENTION

The present invention has been made in an effort to provide a combustion apparatus having advantages of reducing generation of NOx by securing more time for mixing fuel and air and uniformly mixing fuel and air.
The present invention has also been made in an effort to provide a combustion apparatus having advantages of forming a flame at a position distant from an outlet, without being blown out, by modifying fuel and supplying a modified gas including hydrogen from the center of the outlet.
An exemplary embodiment of the present invention provides a combustion apparatus including: a modifying part configured in the center to modify supplied hydrocarbon-based fuel and air and discharge high temperature modified gas including hydrogen to an outlet; and a supply part configured at an outer side of the outlet to jet fuel and air to one side of the modified gas discharged from the modifying part to form a flame at a position spaced apart by a pre-set distance from the outlet.
An equivalence ratio of hydrocarbon-based fuel in the mixture of fuel and air supplied to the modifying part may range from a stoichiometric ratio of partial oxidation to a stoichiometric ratio of combustion.
The modifying part may include a first housing electrically earthed; and an electrode separately installed in the center within the first housing and receiving a voltage applied thereto.
The first housing may include: a discharge region forming a discharge gap with the electrode therebetween to allow fuel and air to react under a partial oxidation condition; and an expanded region expanded from the discharge region to stabilize gas discharged after being reacted in the discharge region.
The supply part may be formed to jet fuel and air to an outer side of the modified gas discharged from the modifying part.
The supply part may include a second housing separately disposed on an outer circumference of the first housing and a third housing separately disposed on an outer circumference of the second housing, and may further include a fuel passage formed between the first housing and the second housing and an air passage formed between the second housing and the third housing.
The air passage may be connected to the discharge region across the fuel passage by a passage connection member connecting the second housing and the first housing.
The second housing may have a side wall formed at one side of the fuel passage, and the first housing may be connected to the side wall through a method such as screw-connection, welding, or the like.
The first housing may further include a coupling portion protruded toward the side wall of the second housing, the fuel passage may include an inflow side formed at the center of one side of the first housing and a supply side connected to the outer circumference of the first housing, and the coupling portion may include a through hole connecting the inflow side and the supply side.
An end portion of the first housing includes a flange formed to be protruded to an outer side in a diameter direction of the second housing such that a space is formed with an end portion of the second housing in a length direction of the second housing in the opposite side of the side wall of the second housing, and the space set between the flange and the end portion of the second housing may allow the supply side of the fuel passage to open to the outside in the diameter direction of the second housing.
The end portion of the second housing and an end portion of the third housing may be disposed in the same line in the diameter direction.
The first housing may include an inner member forming an air nozzle jetting air toward the electrode, and an outer member coupled to an outer circumference of the inner member and accommodating air to be jetted through the air nozzle upon receiving it.
A plurality of air nozzles may be disposed to be spaced apart from each other in a circumferential direction in the inner member, and may have an angle sloped with respect to a diameter direction of the inner member.
The supply part may be formed to jet fuel and air in a direction parallel to the direction in which the modified gas is discharged from an outer side of the modified gas discharged from the modifying part.
The supply part may include a second housing separately disposed on an outer circumference of the first housing and a third housing separately disposed on an outer circumference of the second housing, and may further include a fuel passage formed between the first housing and the second housing and an air passage formed between the second housing and the third housing, and an end portion of the first housing may include a flange disposed at an inner side of an end portion of the second housing and protruded inwardly in a diameter direction of the first housing.
The end portion of the first housing and the end portion of the second housing may be formed to be parallel to each other, and a first swirler may be installed between the end portion of the first housing and the end portion of the second housing and a second swirler may be installed between the end portion of the second housing and the end portion of the third housing.
According to embodiments of the present invention, the modifying part modifies fuel to discharge a modified gas including hydrogen and supplies fuel and air to an outer side of an outlet to the supply part, and thus, a flame can be stably formed at a position spaced apart by a pre-set distance from the outlet.
Thus, a time for mixing fuel supplied from the supply part and air can be further secured by a time corresponding to the distance between the outlet of the combustion apparatus and the flame. Since the mixture time is lengthened, fuel and air can be more uniformly mixed, and thus, generation of NOx can be reduced.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a partial sectional perspective view of a combustion apparatus according to a first embodiment of the present invention.

FIG. 2 is a sectional view of the combustion apparatus illustrated in FIG. 1.

FIG. 3 is a sectional view taken along line III-Iii in FIG. 2.

FIG. 4 is a photograph showing a state of a flame when fuel is burnt by the combustion apparatus of FIG. 1.

FIG. 5 is a photograph showing a state of a flame when fuel is burnt by the related art combustion apparatus.

FIG. 6 is a sectional view of a combustion apparatus according to a second embodiment of the present invention.

DETAILED DESCRIPTION OF THE EMBODIMENTS

Hereinafter, the present invention will be described more fully hereinafter with reference to the accompanying drawings, in which exemplary embodiments of the invention are shown. As those skilled in the art would realize, the described embodiments may be modified in various different ways, all without departing from the spirit or scope of the present invention. The drawings and description are to be regarded as illustrative in nature and not restrictive. Like reference numerals designate like elements throughout the specification.
FIG. 1 is a partial sectional perspective view of a combustion apparatus according to a first embodiment of the present invention. FIG. 2 is a sectional view of the combustion apparatus illustrated in FIG. 1. FIG. 3 is a sectional view taken along line III-Iii in FIG. 2.
Referring to FIGS. 1 to 3, a combustion apparatus 1 according to a first embodiment of the present invention includes a modifying part 100 for modifying hydrocarbon-based fuel into a high temperature modified gas including hydrogen and a supply part 200 jetting fuel and air to an outlet 101 of the combustion apparatus 1. Hydrogen included in the modified gas has fast combustion speed and fast diffusion speed. Thus, the high temperature modified gas and hydrogen supplied from the modifying part 100 form a flame F at a position distant from the outlet 101 of the combustion apparatus 1 and prevents the flame F from being blown off. Namely, the modified gas and hydrogen may stabilize the flame F at a position distant from the outlet 101 of the combustion apparatus 1.
To this end, the modifying part 100 is provided in the center of the combustion apparatus 1 and configured to make supplied fuel react according to a partial oxidation condition to modify it into a gas including high temperature hydrogen and discharge the hydrogen and the modified gas to the outlet 101.
The modified gas discharged from the modifying part 100 is jetted to a front side (the flame F) from the outlet 101 to push the flame F based on the combustion of the fuel supplied from the supply part 200 and air to stably maintain the flame F at a position distant from the outlet 101 by a pre-set distance L.
In the present embodiment, the modifying part 100 is integrally provided in the combustion apparatus 1, so it can stably supply hydrogen toward the air and fuel supplied from the supply part 200 to the outlet 101. Thus, the modifying part 100 can supply hydrogen by a simple configuration, and thus, namely, an additional device for supplying hydrogen is not required.
The supply part 200 is provided at an outer side of the outlet 101 and configured to jet fuel and air to an outer side of the discharged modified gas to form the flame F. The supply part 200 according to the present embodiment is formed to have a structure for accommodating the modifying part 100. The fuel and air supplied from the supply part 200 is pushed by a pre-set distance L from the outlet 101 by the modified gas supplied from the modifying part 100.
However, due to fast combustion and spreading speed of the high temperature modified gas and hydrogen supplied from the modifying part 100, the fuel and air supplied from the supply part 200 are burnt at a position distant from the outlet 101 by the distance L, rather than being blown off, thus stably maintaining the flame F.
The distance L set between the outlet 101 and the flame F secures a longer period of time for mixing fuel and air supplied from the supply part 200. Thus, the fuel and air in a state of having left the outlet 101 may be further uniformly mixed while proceeding by the distance L.
In this manner, the combustion apparatus 1 according to the present embodiment can drastically generation of NOx by using the fast combustion and spreading performance of the high temperature modified gas and hydrogen generated in the modifying part 100 when fuel is burnt.
When a mixture ratio of the fuel and air in the modifying part 100 is excessively rich, a partial oxidation reaction does not take place and hydrogen is not generated. Conversely, when the mixture ratio of the fuel and air in the modifying part 100 is overly close to a combustion ratio, the flame is maintained only within the modifying part 100 and hydrogen is not generated.
When hydrogen is not generated in the modifying part 100, flame formed according to combustion of fuel and air supplied to the supply part 200 is blown out in the outlet 101 of the combustion apparatus 1. Thus, a mixture of fuel and air is required to have an appropriate equivalence ratio.
For example, since a stoichiometric ratio of partial oxidation in a hydrocarbon-based fuel is 0.5 and a stoichiometric ratio of combustion is 2.0. Thus, in case of LNG having methane as a main ingredient in a mixture of fuel and air in the modifying part 100, O₂/C ratio may range from 0.7 to 1.9.
The combustion apparatus 1 will be described in detail. The modifying part 100 includes a first housing 10 supplying air and electrically earthed, and an electrode E separately installed at the center within the housing 10 to supply fuel and receiving a voltage HV applied thereto.
When the voltage HV is applied to the electrode E, plasma discharge occurs in the fuel and air mixed between the electrode E and the first housing 10. In this case, the fuel is partially oxidized to form a high temperature modified gaseous state including hydrogen.
The first housing 10 includes a discharge region 111 and an expanded region 112 set according to a direction in which a gas modified as fuel and air are introduced is discharged. The discharge region 111 has a discharge gap G formed between the first housing 10 and the electrode E, and plasma discharge occurs in the discharge gap G to allow supplied fuel and air to react under a partial oxidation condition so as to be modified.
The expanded region 112 is formed to be expanded greater than a diameter of the discharge region 111 at one side of the discharge region 111, and stabilizes gas discharged after being reacted under the partial oxidation condition and discharges the stabilized gas. Namely, the modified gas reacted under the partial oxidation condition is re-circulated in the large space of the expanded region 112 so as to be stabilized.
The supply part 200 includes a second housing 20 separately disposed on an outer circumference of the first housing 10 and a third housing 30 separately disposed on an outer circumference of the second housing 20. In this case, the first housing 10 is accommodated in the second housing, and the second housing 20 is accommodated in the third housing 30 by stages. For example, the first, second, and third housings 10, 20, and 30 may form a concentric circular structure.
A fuel passage P1 is formed between the first housing 10 and the second housing 20, and an air passage P2 is formed between the second housing 20 and the third housing 30. The fuel passage P1 and the air passage P2 supply fuel and air supplied to one side thereof to the modifying part 100 and the supply part 200.
For example, the air passage P2 is connected to the discharge region 111 of the modifying part 100 across the fuel passage P1 by a passage connection member 22 connected to the first housing 10 by passing through the second housing 20. The air passage P2 supplies air to the discharge region 111. Also, the air passage P2 supplies air between end portions E2 and E3 of the second and third housings 20 and 30 of the supply part 200.
For example, the second housing 20 includes a side wall 21 formed at one side of the fuel passage P1, and the first housing 10 may be connected to the side wall 21 of the second housing 20 through various methods such as screw connection, welding, or the like. For the screw connection, the first housing 10 further includes a coupling portion 11 protruded toward the side wall 21 of the second housing 20. Namely, a male screw of the coupling portion 11 is screw-connected to a female screw of the side wall 21.
Here, the fuel passage P1 set between the first and second housings 10 and 20 includes an inflow side P11 formed in the center at one side of the first housing 10 and a supply side P12 connected to an outer circumference of the first housing 10.
The coupling portion 11 of the first housing 10 includes a through hole 12 connecting the inflow side P11 and the supply side P12 of the fuel passage P1. As soon as air introduced to the inflow side P11 is supplied to the discharge region 111, it is supplied to the supply side P12 through the through hole 12 of the coupling portion 11.
In the opposite side of the side wall 21 of the second housing 20, the first housing 10, the first housing 10 includes a flange 13 formed on an end portion E1 set in one side of the second housing 20 in a length direction (in a horizontal direction in FIG. 2).
The flange 13 is formed to be protruded to the outside in a diameter direction of the second housing 20 and forms a space C with the end portion E2 of the second housing 20. The space C allow the supply side P12 of the fuel passage P1 to be open toward the outer side in a diameter direction of the second housing 20, so that supplied fuel can be supplied toward the outer side of the second housing 20.
Here, the end portion E2 of the second housing 20 and the end portion E3 of the third housing 30 are disposed in the same straight line in the diameter direction, allowing air supplied through the air passage P2 to be mixed with fuel supplied between the both end portions E2 and E3.
Namely, fuel supplied through the fuel passage P1 is supplied to the end of the air passage P2 through the space C so as to be mixed with air supplied through the air passage P2, and discharged to a front side of the outlet 101 in the combustion apparatus 1 to form the flame F.
The size of the space C may be adjusted according to a range in which the coupling portion 11 of the first housing 10 is fastened to the side wall 21 of the second housing 20. A mixture ratio of air and fuel may be set by controlling supply of fuel through the fuel passage P1 with respect to supply of air through the air passage P2 according to a size of the space C.
Also, the first housing 10 includes an inner member 14 and an outer member 15 coupled to partially overlap with each other in a length direction. The inner member 14 includes an air nozzle 16 jetting air toward the electrode E of the discharge region 111.
A plurality of air nozzles 16 are disposed to be spaced apart from the inner member 14 in a circumferential direction, and have an angle (θ) sloped with respect to a diameter direction of the inner member 14 (See FIG. 3). Thus, air supplied to the air nozzle 16 is supplied while being rotated in the circumferential direction between the electrode E and the first housing 10 and in the gap G.
The outer member 15 includes a chamber 17 coupled to an outer circumference of the inner member 14 and accommodating air upon receiving it from the air nozzle 16. Thus, the chamber 17 makes amounts of air jet through the plurality of air nozzles 16 uniform by uniformly maintaining pressure of supplied air.
Meanwhile, the electrode E forming the discharge region 111 together with the inner member 14 includes a fuel nozzle 26 jetting fuel. The fuel nozzle 26 is connected to the inflow side P11 of the fuel passage P1 and jets supplied fuel to the inner wall of the inner member 14 in the vicinity of the gap G.
The fuel jetted to the gap G of the discharge region 111 is mixed with air rotated upon being jetted through the air nozzle 16, and reacts under a partial oxidation condition, while generating a rotating arc by a voltage HV set between the electrode E and the inner member 14. Namely, fuel is modified into a high temperature gas including hydrogen.
The hydrogen and the modified gas modified in the discharge region 111 is recirculated in the expanded region 112 so as to be stabilized and discharged to the outlet 101. The discharged hydrogen and modified gas act as pushing force in the distance L within a pre-set range in front of the outlet 101 to thrust fuel and air supplied to the supply part 200 out of the range of the distance L.
Thus, the fuel and air supplied to the supply part 200 reaches outside of the range of the distance L through the outside of the region of the hydrogen and modified gas. At the same time, the modified gas is maintained to have a high temperature state and hydrogen has a fast combustion and spreading speed. Thus, the fuel and air supplied to the supply part 200 is implemented for lean combustion outside of the range of the distance L, stably maintaining the flame F.
While proceeding by the distance L, the fuel and air supplied to the supply part 20 are mixed to have a further uniform state for an additional mixture time, implementing lean combustion. Thus, when fuel is burnt, generation of NOx can be reduced.
FIG. 4 is a photograph showing a state of a flame when fuel is burnt by the combustion apparatus 1 of FIG. 1, and FIG. 5 is a photograph showing a state of a flame when fuel is burnt by the related art combustion apparatus.
Referring to FIGS. 4 and 5, the related art combustion apparatus 2 approaches the outlet to form a flame F2. In comparison, the combustion apparatus 1 according to an embodiment of the present invention stabilizes the flame F at a position distant from the outlet 101 by the distance L. It can be seen that the flame F is not formed in the central portion of the outlet 101.
Hereinafter, a second embodiment of the present invention will be described. A description of the same configuration as that of the first embodiment will be omitted and a different configuration from that of the first embodiment will be described.
FIG. 6 is a sectional view of a combustion apparatus according to a second embodiment of the present invention. Referring to FIG. 6, in a combustion apparatus 3 according to the second embodiment of the present invention, a supply part 300 is formed to jet fuel and air in a direction parallel to the discharge direction of the modified gas at an outer side of the modified gas including hydrogen discharged from the modifying part 100.
For example, an end portion E21 of the first housing 10 includes a flange 23 disposed at an inner side of an end portion E22 of the second hosing 20 and protruded inwardly in a diameter direction of the first housing 10.
The flange 23 is formed to narrow the outlet 102 in the discharge region 111 to thus lower or adjust a speed of the modified gas including hydrogen sprut through the outlet 102.
An end portion E23 of the third housing 30 is disposed to be parallel in the outlet 102 together with the end portion E22 of the second housing 20. A first swirler S1 may is provided between the end portions E21 and E22 of the first and second housings 10 and 20 forming the fuel passage P1 in order to swirl discharged fuel. A second swirler S2 is provided between the end portions E22 and E23 of the second and third housings 20 and 30 forming the air passage P2 in order to swirl discharged air.
Thus, fuel discharged between the end portions E21 and E22 of the first and second housings 10 and 20 and air discharged between the end portions E22 and E23 of the second and third housings 20 and 30 are swirled to be mixed by the first and second swirlers S1 and S2, so as to be discharged while being swirled in a direction parallel to the discharge direction of the modified gas.
The fuel and air mixed by the first and second swirlers S1 and S2 may form the flame F, without being blown out, at a position distant from the outlet 102 by the distance L according to the discharge speed of the modified gas.
While this invention has been described in connection with what is presently considered to be practical exemplary embodiments, it is to be understood that the invention is not limited to the disclosed embodiments, but, on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.


<Description of symbols>

10, 20, 30: first, second, and third housing	11: coupling portion
12: through hole	13, 23: flange
14: inner member	15: outer member
16: air nozzle	17: chamber
21: side wall	100: modifying part
101, 102: outlet	111: discharge region
112: expanded region	200: supply part
C: interval	E1, E2, E3, E21, E22,
	E23: end portion
F: flame	L: distance
P1: fuel passage	P11: inflow side
P12: supply side	P2: air passage
1, 2, 3: combustion apparatus

Claims

What is claimed is:

1. A combustion apparatus comprising:

a modifying part configured in the center to modify supplied hydrocarbon-based fuel and air and discharge high temperature modified gas including hydrogen to an outlet; and

a supply part configured at an outer side of the outlet to jet fuel and air to one side of the modified gas discharged from the modifying part to form a flame at a position spaced apart by a pre-set distance from the outlet.

2. The combustion apparatus of claim 1, wherein an equivalence ratio of hydrocarbon-based fuel in the mixture of fuel and air supplied to the modifying part ranges from a stoichiometric ratio of partial oxidation to a stoichiometric ratio of combustion.

3. The combustion apparatus of claim 1, wherein the modifying part comprises:

a first housing electrically earthed; and

an electrode separately installed in the center within the first housing and receiving a voltage applied thereto.

4. The combustion apparatus of claim 3, wherein the first housing comprises:

a discharge region forming a discharge gap with the electrode therebetween to allow fuel and air to react under a partial oxidation condition; and

an expanded region expanded from the discharge region to stabilize gas discharged after being reacted in the discharge region.

5. The combustion apparatus of claim 3, wherein the supply part is formed to jet fuel and air to an outer side of the modified gas discharged from the modifying part.

6. The combustion apparatus of claim 5, wherein the supply part comprises

a second housing separately disposed on an outer circumference of the first housing; and

a third housing separately disposed on an outer circumference of the second housing, and

further comprises:

a fuel passage formed between the first housing and the second housing; and

an air passage formed between the second housing and the third housing.

7. The combustion apparatus of claim 6, wherein the air passage is connected to the discharge region across the fuel passage by a passage connection member connecting the second housing and the first housing.

8. The combustion apparatus of claim 6, wherein the second housing has a side wall formed at one side of the fuel passage, and the first housing is connected to the side wall through a method such as screw-connection or welding.

9. The combustion apparatus of claim 8, wherein the first housing further comprises a coupling portion protruded toward the side wall of the second housing,

the fuel passage comprises

an inflow side formed at the center of one side of the first housing and

a supply side connected to the outer circumference of the first housing, and

the coupling portion comprises a through hole connecting the inflow side and the supply side.

10. The combustion apparatus of claim 9, wherein an end portion of the first housing includes a flange formed to be protruded to an outer side in a diameter direction of the second housing such that a space is formed with an end portion of the second housing in a length direction of the second housing in the opposite side of the side wall of the second housing, and

the space set between the flange and the end portion of the second housing allows the supply side of the fuel passage to open to the outside in the diameter direction of the second housing.

11. The combustion apparatus of claim 10, wherein the end portion of the second housing and an end portion of the third housing are disposed in the same line in the diameter direction.

12. The combustion apparatus of claim 3, wherein the first housing comprises:

an inner member forming an air nozzle jetting air toward the electrode; and

an outer member coupled to an outer circumference of the inner member and accommodating air to be jetted through the air nozzle upon receiving it.

13. The combustion apparatus of claim 12, wherein a plurality of air nozzles are disposed to be spaced apart from each other in a circumferential direction in the inner member, and have an angle sloped with respect to a diameter direction of the inner member.

14. The combustion apparatus of claim 3, wherein the supply part is formed to jet fuel and air in a direction parallel to the direction in which the modified gas is discharged from an outer side of the modified gas discharged from the modifying part.

15. The combustion apparatus of claim 12, wherein the supply part comprises:

a second housing separately disposed on an outer circumference of the first housing and

further comprises:

a fuel passage formed between the first housing and the second housing and

an air passage formed between the second housing and the third housing, and

an end portion of the first housing includes a flange disposed at an inner side of an end portion of the second housing and protruded inwardly in a diameter direction of the first housing.

16. The combustion apparatus of claim 15, wherein

the end portion of the first housing and the end portion of the second housing are formed to be parallel to each other, and

a first swirler is installed between the end portion of the first housing and the end portion of the second housing and

a second swirler is installed between the end portion of the second housing and the end portion of the third housing.