Patent Grant
9945564
Field of the Invention
The present invention relates to a combustion furnace, in particular, to a combustion furnace in which the temperature inside the combustion furnace can be maintained to achieve better combustion efficiency.
The Prior Arts
Combustion furnaces burn combustible materials, such as woods, leaves, papers, charcoals or other biomass fuels, so combustion furnaces can be provided to cook or to generate heat. Conventionally, a combustion furnace includes an inner shell and an outer shell. The inner shell is provided as the space for the combustion. Combustion furnaces are provided as heat providers for families. In addition to large combustion furnaces used in households or industries, combustion furnaces are also suitable for outdoor activities, and the volume and weight of combustion furnaces has gradually been reduced to allow for personal combustion furnaces.
However, conventionally, due to insufficient air in the combustion furnace, the ignition time may be too long to allow the materials inside the combustion furnace to ignite. Additionally, when larger sized materials are placed in the combustion furnace during combustion, the flame in the combustion furnace prevents complete combustion, and generates a considerable volume of black smoke and carbon monoxide, while combustion performance is poor.
Additionally, the combustion efficiency of the combustion furnace depends on whether the gas inside the combustion furnace flows fluently to maintain the internal temperature. Conventionally, since the heat convection of the combustion furnace is insufficient and the combustion furnace is devoid of a cover, the flame in the combustion furnace will be ejected upward, so the temperature inside the combustion furnace is insufficient to result in complete combustion. As a result, the conventional combustion furnace combustion process takes longer, and the user needs to add fuel to the combustion furnace continuously, to maintain the internal temperature.
Consequently, improvement of the combustion furnace's control mechanism to ensure stable combustion, how to reduce the black smoke and dust generated by the combustion furnace, how to maintain the temperature inside the combustion furnace, and how to improve the performance of the combustion furnace, are issues to be addressed by the applicants and related personnel.
To address these issues, the present invention provides a combustion furnace, comprising an inner shell, an outer shell, a gas inlet piping and a flame inhibiting cover. The inner shell defines a receiving cavity therein. The inner shell defines a plurality of first gas holes around the periphery of a top portion thereof. The inner shell defines a gas inlet hole at a bottom portion thereof. The outer shell encloses the inner shell such that a gas flowing space is defined between the inner shell and the outer shell. The gas inlet piping has an opening formed at one end thereof, and the gas inlet piping communicates with the gas flowing space. The flame inhibiting cover is atop the outer shell and the inner shell, and a lower flange of the flame inhibiting cover is below the first gas holes.
In one implementation aspect, the combustion furnace further comprises a baffle sheet assembled to the communicating portion between the gas inlet piping and the gas flowing space.
In one implementation aspect, the opening of the gas inlet piping is wedge-shaped.
In one implementation aspect, the combustion furnace further comprises a flame stopping plate enclosing the lower flange of the flame inhibiting cover.
In one implementation aspect, the width of the flame stopping plate is defined in the range from 1.5 cm to 4 cm.
In one implementation aspect, the inner shell further comprises a plurality of via holes defined there around and between the top portion and the bottom portion thereof.
In one implementation aspect, the diameter of each of the via holes is defined in the range from 0.6 cm to 1 cm.
In one implementation aspect, the inner shell further comprises a plurality of second gas holes defined around the periphery of the bottom portion thereof.
In one implementation aspect, the diameter of each of the second gas holes is defined in the range from 0.6 cm to 1 cm.
In one implementation aspect, the inner wall further comprises a plurality of third gas holes defined at the bottom thereof and defined around the gas inlet hole.
In one implementation aspect, the diameter of each of the third gas holes is defined in the range from 0.9 cm to 1.2 cm.
In one implementation aspect, the inner shell further comprises a plurality of ash removing openings formed at the bottom thereof, wherein the dust removing openings and the third gas holes are alternately arranged around the gas inlet hole.
In one implementation aspect, the combustion furnace further comprises a combustion supporting device in the receiving cavity and above the gas inlet hole. The combustion supporting device comprises a tubular member, a cone-shaped member and a base portion. The cone-shaped member defines an inserting groove therein. A bottom of the tubular member is received in the inserting groove. The base portion is connected to a bottom of the cone-shaped member.
In one implementation aspect, the tubular member further comprises a plurality of vents defined around a top portion thereof.
In one implementation aspect, a distance is defined between the bottom of the cone-shaped member and the gas inlet hole.
In one implementation aspect, the diameter of the inner shell is defined in the range from 40 cm to 70 cm.
In one implementation aspect, the diameter of the outer shell is defined in the range from 42 cm to 75 cm.
In one implementation aspect, the diameter of each of the first gas holes is defined in the range from 0.8 cm to 1.5 cm.
In one implementation aspect, the depth of the inner shell is defined in the range from 60 cm to 130 cm.
In one implementation aspect, the diameter of the gas inlet hole is 5 cm.
In one implementation aspect, the diameter of the lower flange of the flame inhibiting cover is defined in the range from 27 cm to 60 cm.
Accordingly, the first air holes allow the swirl generation when the fresh air enters into the inner shell, so that the gas inside the combustion furnace can flow fluently, the flame in the combustion furnace can be retarded from moving upwardly, and the temperature inside the combustion furnace can be maintained to improve the combustion performance of the combustion furnace. Additionally, the inlet gas hole at the bottom portion of the inner shell facilitates fresh air entering into the inner shell to mix with the fuels, so that complete combustion is accomplished.
Additionally, the wedge-shaped opening and the baffle sheet allows the air to generate an air flow when the air enters into the gas inlet piping, so that the air flow facilitates more fresh air entering into the inner shell to achieve better combustion performance.
Detailed description of the characteristics and the advantages of the present invention is shown in the following embodiments, the technical content and the implementation of the present invention should be readily apparent to any person skilled in the art from the detailed description, and the purposes and the advantages of the present invention should be readily understood by any person skilled in the art with reference to content, claims and drawings in the present invention.
The present invention will become more fully understood from the detailed description given herein below for illustration only, and thus not limitative of the present invention, wherein:
Please refer to
Accordingly, the first air holes 11a are defined around the periphery of the top portion of the inner shell 11, so that the gas inside the combustion furnace 1 flows fluently to generate a swirl 2 to retard the flame in the combustion furnace 1 from moving upwardly or ejecting upwardly, and the temperature inside the combustion furnace 1 can be maintained to improve the combustion performance of the combustion furnace 1. The diameter of each of the first air holes 11a may be, but not limited to, in the range from 0.8 cm to 1.5 cm. Additionally, the inlet gas hole 16 is defined at the bottom portion of the inner shell 11, so that fresh air can enter into the inner shell 11 to mix with the fuels (combustible materials), inside the inner shell 11 to accomplish complete combustion. The diameter of the gas inlet hole 16 may be, but not limited to, 5 cm. Preferably, the lower flange of the flame inhibiting cover 14 is below the first air holes 11a.
In addition, in some embodiments, the combustion furnace 1 further comprises a flame stopping plate 141 enclosing the lower flange of the flame inhibiting cover 14. The flame stopping plate 141 is provided for protecting the flame inhibiting cover 14 from suffering the flame coming up from the combustion area. In some embodiments, the width of the flame stopping plate 141 may be, but not limited to, in the range from 1.5 cm to 4 cm.
Please refer to
Additionally, as shown in
Alternatively, the opening of the gas inlet piping 13 can be unprocessed, as shown in
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Please refer to
Powdered ceramic materials can be placed into the space defined by the outer surface of the lower portion of the tubular member 171 and an inner wall of the cone-shaped member 172 to maintain the temperature of the combustion furnace 1, and ensure stable combustion. The ceramic materials are heat resistant, and may be made of, but are not limited to, zirconium oxide, aluminum oxide. In a preferred embodiment, a distance is defined between the bottom of the cone-shaped member 172 and the gas inlet hole 16. The distance is defined in the range from 0.3 cm to 20 cm. Preferably, the distance is defined in the range from 1 cm to 5 cm.
Please refer to
Moreover, in some embodiments, the inner shell 11 further comprises a plurality of ash removing openings 19 formed at the bottom thereof, wherein the ash removing openings 19 and the third gas holes 18 are alternately arranged around the gas inlet hole 16. Accordingly, after use, the user can remove ashes left in the combustion furnace 1 from the ash removing openings 19 conveniently.
Based on the above, the combustion furnace 1 according to the present invention may comprise the combustion supporting device 17 or may not. Details of the structure of the combustion furnace 1 are described as above. Here, the combustion furnace 1 devoid of the combustion supporting device 17 is preferably to be carried out by the embodiment shown in
Accordingly, the first air holes allow the swirl generation when the fresh air enters into the inner shell, so that the gas inside the combustion furnace can flow fluently, the flame in the combustion furnace can be retarded from moving upward, and the temperature inside the combustion furnace can be maintained to improve the combustion performance of the combustion furnace. Additionally, the inlet gas hole at the bottom portion of the inner shell facilitates fresh air entering into the inner shell to mix with the fuels, so that complete combustion is accomplished.
Additionally, the wedge-shaped opening and the baffle sheet allows the air to generate an air flow when the air enters into the gas inlet piping, so that the air flow facilitates more fresh air entering into the inner shell to achieve better combustion performance.
While the present invention has been described by the way of example and in terms of the preferred embodiments, it is to be understood that the present invention need not be limited to the disclosed embodiments. On the contrary, it is intended to cover various modifications and similar arrangements included within the spirit and scope of the appended claims, the scope of which should be accorded the broadest interpretation so as to encompass all such modifications and similar structures.
| Number | Date | Country | Kind |
|---|---|---|---|
| 104101529 A | Jan 2015 | TW | national |
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| Number | Date | Country | |
|---|---|---|---|
| 20160209043 A1 | Jul 2016 | US |
