Combustion chamber
11499717 · 2022-11-15
Assignee
Inventors
- Rongxin Zhao (Hangzhou, CN)
- Guoliang Chen (Hangzhou, CN)
- Yongqiang Wang (Huzhou, CN)
- Erpeng Qiu (Hangzhou, CN)
- Bingyuan Shen (Hangzhou, CN)
Cpc classification
F23D14/78
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/30
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F23D14/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2203/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23H2900/03021
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/82
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23H3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R2900/03044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23R3/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C99/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/78
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/82
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Embodiments provide a combustion structure that can achieve stable combustion by addressing the aforementioned drawbacks in the prior art such as low flame stability, backfire, deflagration, blockage and/or any other drawbacks. The combustion chamber structure in accordance with the disclosure can include: a grate structure including a first set of elongated components, a fire retention structure including a second set of elongated components. The first set of first elongated components can be arranged along an axial direction within the combustion chamber structure. The second set of elongated components can be arranged along the axial direction in a same direction as the first elongated components. The second set of elongated components can be configured to generate a negative pressure zone within the combustion chamber. The first set of elongated components can form apertures that can be aligned with apertures formed by the second set of elongated components.
Claims
1. A combustion chamber comprises: a gas inlet for providing a mixed gas to the combustion chamber, an ignition device, and a grate structure, wherein the grate structure comprises a first set of tubes and a second set of tubes proximal to the first set of tubes, wherein the first set of tubes are arranged to form first set of apertures between each of the first set of tubes, the second set of tubes are arranged to form second set of apertures between each of the second set of tubes, wherein the first set of apertures and the second set of apertures are arranged in intervals along flow direction of the mixed gas; the mixed gas from the gas inlet flows through the first set of apertures and the second set of apertures, and is ignited after flowing through the second set of apertures to form flames in the combustion chamber; each of the second set of tubes forms a blunt body configured to generate a negative pressure zone in the combustion chamber after the second set of apertures and to prevent backfire; each of the second set of tubes is aligned with one of the first set of apertures and is configured to split the mixed gas passing through one of the first set of apertures.
2. The combustion chamber of claim 1, wherein a side surface of each of the first set of tubes is flat.
3. The combustion chamber of claim 1, wherein each of the first set of tubes and the second set of tubes comprise a channel configured to allow a cooling medium to flow through the channel.
4. The combustion chamber of claim 1, wherein each of the second set of tubes has a circular cross section.
5. The combustion chamber of claim 1, wherein the combustion chamber comprises a distal end and a proximal end; and wherein the first set of tubes are distally positioned relatively to the second set of tubes within the combustion chamber.
6. The combustion chamber of claim 5, wherein the combustion chamber is configured such that a cooling medium flows into the first set of tubes from the distal end and flows out of the first set of tubes at the proximal end.
7. The combustion chamber of claim 5, wherein the combustion chamber is configured to receive a burning medium at the proximal end.
8. The combustion chamber of claim 1, wherein the first set of apertures each has a same size.
9. A burner comprising a combustion chamber, a first cooling pipe, and a second cooling pipe, wherein the combustion chamber comprises: a gas inlet for providing a mixed gas to the combustion chamber, an ignition device, and a grate structure, wherein the grate structure comprises a first set of tubes and a second set of tubes proximal to the first set of tubes, wherein the first set of tubes are arranged to form first set of apertures between each of the first set of tubes, the second set of tubes are arranged to form second set of apertures between each of the second set of tubes, wherein the first set of apertures and the second set of apertures are arranged in intervals along flow direction of the mixed gas; the mixed gas from the gas inlet flows through the first set of apertures and the second set of apertures, and is ignited after flowing through the second set of apertures to form flames in the combustion chamber; each of the second set of tubes forms a blunt body configured to generate a negative pressure zone in the combustion chamber after the second set of apertures and to prevent backfire; wherein: the first cooling pipe is in fluid communication with the first set of tubes and the second set of tubes at a distal end of the burner; the second cooling pipe is in fluid communication with the first set of tubes and the second set of tubes at a proximal end of the burner; and each of the second set of tubes is aligned with one of the first set of apertures and is configured to split the mixed gas passing through one of the first set of apertures.
10. The burner of claim 9, wherein the burner is configured such that a cooling medium in the first cooling pipe flows into the first set and second set of tubes at the distal end of the burner and flows out of the first set and second set of tubes at the proximal end of the burner into the second cooling pipe.
11. The burner of claim 9, further comprising one or more strengthening pipes supporting the burner, wherein the one or more strengthening pipes comprise channels to allow a cooling medium to flow through the strengthening pipes.
12. The burner of claim 9, further comprising a flame detector to detect a presence of a flame in the burner.
13. The burner of claim 9, wherein the ignition device is configured to ignite a flame within the burner.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF THE INVENTION
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(13) Attention is now directed to the grate structure 104 and the flame retention structure 106. The grate structure 104 can be configured to retain the burning medium 102 for combustion in the combustion zone. As shown, the grate structure 104 can comprise a set of elongated components 108. The elongated components 108 in the grate structure 104 can be arranged along the axis 112 to form apertures in between the elongated components.
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(15) The width of an aperture 202 is also not limited. One skill in the art will understand that the width of aperture can be a design choice depending on the application of chamber 100. However, for optimal flame retention, in some embodiments, the width of aperture 202 can be controlled no more than 2 millimeters. Referring back to
(16) The flame retention structure 106 can include a set of elongated components 110. As shown, the elongated components 110 can be arranged along the same axis, i.e. axis 112 in this example, as the elongated components 108. An insight provided by the inventor(s) is that the elongated components 110 can be installed in addition to the elongated components 108 to improve flame retention in the combustion chamber 100. The arrangement of the elongated components 110 as shown can function as a blunt body to help prevent flame backfire, and thus improve flame stability to maintain continuous and complete combustion. For achieving this, the elongated components can be configured to generate negative pressure zone in the primary combustion zone.
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(18) Referring back to
(19) In this example, the elongated components 110 are aligned with the elongated components 108 such that the apertures of the elongated components 108 and the apertures of the elongated components 110 correspond to each other. In this example, the width of the aperture 202 and the width of the aperture 302 is more or less the same and a given aperture 202 corresponds to a given a given aperture 302 in an interleaving fashion. This is shown in
(20) Referring back to
(21) With the combustion chamber 100 having been described and illustrated, attention is now directed to
(22) In the example shown in
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(25) Referring back to
(26) The specification and drawings are, accordingly, to be regarded in an illustrative rather than a restrictive sense. It will, however, be evident that additions, subtractions, deletions, and other modifications and changes may be made thereunto without departing from the broader spirit and scope. Illustrative methods and systems for providing features of the present disclosure are described above. Some or all of these systems and methods may, but need not, be implemented at least partially by architectures such as those shown in
(27) Although embodiments have been described in language specific to structural features and/or methodological acts, it is to be understood that the disclosure is not necessarily limited to the specific features or acts described. Rather, the specific features and acts are disclosed as illustrative forms of implementing the embodiments. Conditional language, such as, among others, “can,” “could,” “might,” or “may,” unless specifically stated otherwise, or otherwise understood within the context as used, is generally intended to convey that certain embodiments could include, while other embodiments do not include, certain features, elements, and/or steps. Thus, such conditional language is not generally intended to imply that features, elements, and/or steps are in any way required for one or more embodiments or that one or more embodiments necessarily include logic for deciding, with or without user input or prompting, whether these features, elements, and/or steps are included or are to be performed in any particular embodiment.