Combustion furnace

Abstract

A combustion furnace includes 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 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.

Claims

1. A combustion furnace, comprising: an inner shell, defining a receiving cavity therein, the inner shell defining a plurality of first gas holes around the periphery of a top portion thereof, the inner shell defining a gas inlet hole at a bottom portion thereof; an outer shell, enclosing the inner shell such that a gas flowing space is defined between the inner shell and the outer shell; a gas inlet piping having an opening formed at one end thereof and the gas inlet piping communicating with the gas flowing space; a flame inhibiting cover including a conical portion and a cylindrical portion extending downwardly from the conical portion, a lower edge of the cylindrical portion being disposed below the first gas holes; and a combustion supporting device disposed in the receiving cavity and above the gas inlet hole, the combustion supporting device comprising: a tubular member; a cone-shaped member, defining an inserting groove therein, a bottom of the tubular member received in the inserting groove; and a base portion, connected to a bottom of the cone-shaped member, wherein a powdered ceramic material is placed into a space defined by an outer surface of the lower portion of the tubular member and an inner wall of the cone-shaped member to maintain the temperature of the combustion furnace; wherein a flame stopping plate encloses and is in direct contact with an outer surface of the cylindrical portion for preventing a flame coming out from the receiving cavity.

2. The combustion furnace according to claim 1, further comprising a baffle sheet assembled to a communicating portion between the gas inlet piping and the gas flowing space.

3. The combustion furnace according to claim 1, wherein the opening of the gas inlet piping is wedge-shaped.

4. The combustion furnace according to claim 1, wherein the width of the flame stopping plate is defined in the range from 1.5 cm to 4 cm.

5. The combustion furnace according to claim 1, wherein the inner shell further comprises a plurality of via holes defined therearound and between the top portion and the bottom portion thereof, and wherein the diameter of each of the via holes is defined in the range from 0.6 cm to 1 cm.

6. The combustion furnace according to claim 1, wherein the inner shell further comprises a plurality of second gas holes defined around the periphery of the bottom portion thereof, and wherein the diameter of each of the second gas holes is defined in the range from 0.6 cm to 1 cm.

7. The combustion furnace according to claim 1, wherein the inner shell further comprises a plurality of third gas holes defined at the bottom thereof and defined around the gas inlet hole, and wherein the diameter of each of the third gas holes is defined in the range from 0.9 cm to 1.2 cm.

8. The combustion furnace according to claim 1, wherein the inner shell further comprises a plurality of ash removing openings formed at the bottom thereof, wherein the dust removing openings are arranged around the gas inlet hole.

9. The combustion furnace according to claim 1, wherein the diameter of the inner shell is defined in the range from 40 cm to 70 cm, wherein the depth of the inner shell is defined in the range from 60 cm to 130 cm, and wherein the diameter of the outer shell is defined in the range from 42 cm to 75 cm.

10. The combustion furnace according to claim 1, wherein the diameter of each of the first gas holes is defined in the range from 0.8 cm to 1.5 cm.

11. The combustion furnace according to claim 1, wherein the diameter of the gas inlet hole is 5 cm.

12. The combustion furnace according to claim 1, wherein the diameter of the lower flange of the flame inhibiting cover is defined in the range from 27 cm to 60 cm.

13. The combustion furnace according to claim 1, wherein the tubular member further comprises a plurality of vents defined around a top portion thereof.

14. The combustion furnace according to claim 1, wherein a distance is defined between the bottom of the cone-shaped member and the gas inlet hole.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) 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:

(2) FIG. 1 is an exploded view of a first embodiment of a combustion furnace according to the present invention;

(3) FIG. 2 is a sectional view of a second embodiment of a combustion furnace according to the present invention;

(4) FIG. 3 is a sectional view of a third embodiment of a combustion furnace according to the present invention;

(5) FIG. 4 is a sectional view of a fourth embodiment of a combustion furnace according to the present invention;

(6) FIG. 5 is a top view of the fourth embodiment of the combustion furnace according to the present invention;

(7) FIG. 6 is a sectional view of the first embodiment of the combustion furnace according to the present invention; and

(8) FIG. 7 is a bottom view of an inner shell of an exemplary embodiment of a combustion furnace according to the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(9) Please refer to FIG. 1, illustrating an exploded view of a first embodiment of a combustion furnace 1 according to the present invention. The combustion furnace 1 comprises an inner shell 11, an outer shell 12, a gas inlet piping 13 and a flame inhibiting cover 14. The inner shell 11 defines a receiving cavity 111 therein. The inner shell 11 defines a plurality of first gas holes 11a around the periphery of a top portion thereof. The inner shell 11 defines a gas inlet hole 16 at a bottom thereof. The outer shell 12 encloses the inner shell 11 such that a gas flowing space 15 is defined between the inner shell 11 and the outer shell 12. The diameter of the inner shell 11 may be, but not limited to, in the range from 40 cm to 70 cm. The depth of the inner shell 11 may be, but not limited to, in the range from 60 cm to 130 cm. The diameter of the outer shell 12 may be, but not limited to, in the range from 42 cm to 75 cm. The gas inlet piping 13 has an opening formed at one end thereof, and the gas inlet piping 13 communicates with the gas flowing space 15, so that the gas came from the gas inlet piping 13 can be guided to the receiving cavity 111. The flame inhibiting cover 14 is atop the outer shell 12 and the inner shell 11, wherein the diameter of a lower flange of the flame inhibiting cover 14 may be, but not limited to, in the range from 27 cm to 60 cm. The flame inhibiting cover 14 is closely mated with the inner shell 11 and the outer shell 12. That is, the flame inhibiting cover 14 encloses the top of the receiving cavity 111 and the top of the gas flowing space 15, as shown in FIG. 2. A lower flange of the flame inhibiting cover 14 is below the first gas holes 11a.

(10) 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.

(11) FIG. 2 is a sectional view of a second embodiment of a combustion furnace 1 according to the present invention. FIG. 3 is a sectional view of a third embodiment of a combustion furnace 1 according to the present invention. FIG. 4 is a sectional view of a fourth embodiment of a combustion furnace 1 according to the present invention. Please refer to FIG. 2 to FIG. 4, in which embodiments the inner shell 11 further defines a plurality of via holes 11c there around. The via holes 11c are between the top portion and the bottom portion of the inner shell 11. Similarly, the via holes 11c allow fresh air to enter into the inner shell 11 to mix with the combustible materials inside the inner shell 11, so that the materials inside the inner shell 11 which are locate at a combustion area (namely, the receiving cavity 111) can be burned completely. In some embodiment, the diameter of each of the via holes 11c may be, but not limited to, in the range from 0.6 cm to 1 cm.

(12) 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.

(13) Please refer to FIG. 2, in which embodiment the inner shell 11 further defines a plurality of second gas holes 11b around the periphery of the bottom portion thereof. Again, the second gas holes 11b are provided to induce the communication of fresh air so as to improve the combustion performance of the combustion furnace 1. In some embodiments, the diameter of each of the second gas holes 11b may be, but not limited to, in the range from 0.6 to 1 cm.

(14) Additionally, as shown in FIG. 2, in this embodiment, the opening of the gas inlet piping 13 is wedge-shaped. The wedge-shaped opening 13a of the gas inlet piping 13 allows the air to generate an air flow when the air enters into the gas inlet piping 13. Next, with the configurations of the gas inlet hole 16 and the gas flowing space 15, the air flow facilitates more fresh air entering into the inner shell 11 to achieve better combustion performance.

(15) Alternatively, the opening of the gas inlet piping 13 can be unprocessed, as shown in FIG. 3.

(16) Please refer to FIG. 4 and FIG. 5, in which embodiment the gas inlet piping 13 further comprises a baffle sheet 13b assembled to the communicating portion between the gas inlet piping 13 and the gas flowing space 15. As shown in FIG. 5, the baffle sheet 13b is inclinedly assembled to allow the air to generate an air flow when the air enters into the gas inlet piping 13. Next, with the configurations of the gas inlet hole 16 and the gas flowing space 15, the air flow facilitates more fresh air entering into the inner shell 11 to achieve better combustion performance.

(17) Please refer to FIG. 6, illustrating a sectional view of the fourth embodiment of the combustion furnace 1 according to the present invention. The combustion furnace 1 further comprises a combustion supporting device 17 in the receiving cavity 111 and above the gas inlet hole 16. The combustion supporting device 17 comprises a tubular member 171, a cone-shaped member 172 and a base portion 173. The cone-shaped member 172 defines an inserting groove 1721 therein, such that a bottom of the tubular member 171 is received in the inserting groove 1721, as shown in FIG. 5. The base portion 173 is connected to a bottom of the cone-shaped member 172. The tubular member 171 further defines a plurality of vents 1711 around a top portion thereof.

(18) 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.

(19) Please refer to FIG. 7, illustrating an inner shell 11 of an exemplary embodiment of a combustion furnace 1 according to the present invention. The inner shell 11 further comprises a plurality of third gas holes 18 defined at the bottom thereof and defined around the gas inlet hole 16. The diameter of each of the third gas holes 18 may be, but not limited to, in the range from 0.9 cm to 1.2 cm. The third gas holes 18 facilitate the air communication between the inside of the inner shell 11 and the outside of the inner shell 11 to promote the combustion in the inner shell 11.

(20) 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.

(21) 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 FIG. 2, and the combustion furnace 1 comprising the combustion supporting device 17 is preferably to be carried out by the embodiment shown in FIG. 6.

(22) 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.

(23) 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.

(24) 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.