Combustion device with high combustion efficiency
The burner tube structure, designed with a horizontal mixing section and a rectangular coordinate system, solves the problem of reduced flow rate caused by the mixing port of traditional gas burners, achieving more efficient air-gas mixing and improving combustion efficiency.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- PRO IRODA INDS
- Filing Date
- 2022-05-05
- Publication Date
- 2026-04-21
AI Technical Summary
The mixing port design of traditional gas burners causes a rapid decrease in the gas flow rate in the outlet pipe, affecting the air intake effect and thus reducing combustion efficiency.
It adopts a horizontally extended mixing section design, combined with the furnace head tube structure of the X-axis and Y-axis rectangular coordinate system, including the mixing port, the bend section and the straight section. It uses the negative pressure generated by the gas flow rate to draw in air, and optimizes the mixing flow of air and gas through a specific bend section design.
It improves combustion efficiency, reduces the loss of gas and air flow velocity in the burner tube, increases air mixing, and enhances combustion performance.
Smart Images

Figure CN117053191B_ABST
Abstract
Description
Technical Field
[0001] This invention relates to a combustion device, particularly a combustion device with high combustion efficiency. Background Technology
[0002] Please refer to the Taiwan Patent No. I306498, "Improved Structure of Gas Burner Outlet Pipe", which is a gas burner outlet pipe. It is an outlet pipe with a first end and a second end. The first end has an air inlet to allow gas to enter. The outlet pipe has several small holes and several air inlets. The diameter of the air inlets is larger than that of the small holes. The small holes allow the flame to burst out when the gas is burning, and the air inlets allow fresh air to enter.
[0003] Reference Figure 5 The diagram shows a partially enlarged cross-sectional view of the outlet pipe of an existing gas burner. In addition to the air inlet in the middle and rear section, the outlet pipe 90 of the above-mentioned burner also needs to be equipped with a main mixing port 91 for air to enter. However, the main mixing port 91 of the conventional gas burner is located at the lower edge of the outlet pipe 90 in the vertical direction. This is mainly to prevent the juice produced during the grilling process from dripping into the outlet pipe 90 through the mixing port 91. However, this arrangement also causes the gas flow rate in the outlet pipe to drop rapidly due to the bending of the pipe, which in turn affects the air intake effect of the outlet pipe and leads to a decrease in combustion efficiency. Summary of the Invention
[0004] The purpose of this invention is to provide a combustion device with high combustion efficiency, thereby solving at least one of the aforementioned technical problems in the prior art.
[0005] To achieve the above objectives, the technical solution adopted by the present invention is as follows:
[0006] A combustion device with high combustion efficiency, characterized in that it comprises:
[0007] A base;
[0008] A burner tube is disposed within a base. The burner tube includes a mixing section and an outlet section. The mixing section extends axially along a horizontal and virtual baseline. One end of the mixing section has an air inlet and a first mixing port is disposed on its radial outer periphery. The burner tube is provided with a virtual X-axis and a Y-axis that are coplanar with the baseline. The X-axis is perpendicular to the baseline, and the Y-axis is perpendicular to the X-axis. The mixing section is provided with a first side and a second side opposite to the first side. The second side is adjacent to the Y-axis, and the first mixing port is disposed on the second side. The outlet section is connected to the end of the mixing section opposite to the air inlet. The outlet section is provided with a straight section and a first bend. The straight section extends axially along the baseline and is connected at one end to the mixing section. One end of the first bend is connected to the end of the straight section opposite to the mixing section, and the other end extends away from the mixing section and toward the Y-axis.
[0009] The burner tube is connected to a gas nozzle, which is inserted into the mixing section through the air inlet. A second mixing port is formed between the inner periphery of the mixing section and the outer periphery of the gas nozzle. The second mixing port is open at one end opposite to the gas outlet section.
[0010] The burner tube is equipped with a mixing cover. One side of the mixing cover is connected to the upper edge of the mixing section in the vertical direction, and the other side is connected to the lower edge of the mixing section in the vertical direction. The mixing cover covers but does not close the first mixing port.
[0011] The air inlet protrudes outside the base. One end of the air mixing cover along the axial direction of the baseline is located inside the base and the other end protrudes outside the base. The air mixing cover and the second side form an air passage. The two ends of the air passage along the axial direction of the baseline are open.
[0012] The X-axis and the Y-axis form a rectangular coordinate system, and the intersection of the X-axis and the Y-axis forms an origin. The first curved section is located in the second quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the first curved section is located on the side of the first curved section near the origin. The air outlet section is provided with a second curved section. One end of the second curved section is connected to the end of the first curved section opposite to the straight section. The second curved section is located in the first quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the second curved section is located on the side of the second curved section near the origin.
[0013] The air outlet section is provided with a third bend, one end of which is connected to the end of the second bend opposite to the first bend. The third bend is located in the third quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the bend arc of the third bend is located on the side of the third bend adjacent to the origin. The radius of the bend arc of the third bend is smaller than the radius of the bend arc of the first bend and the radius of the bend arc of the second bend.
[0014] The air outlet section is provided with a straight pipe section, one end of which is connected to the end of the third bend section opposite to the second bend section. The straight pipe section extends in a straight line in a direction parallel to the X-axis toward the straight section, and the end of the straight pipe section opposite to the third bend section is closed.
[0015] The high combustion efficiency combustion device provided by the present invention can improve combustion efficiency through the above-described structure. Attached Figure Description
[0016] Figure 1 This is a perspective view of the combustion device with high combustion efficiency according to the present invention.
[0017] Figure 2 This is an exploded perspective view of the high combustion efficiency combustion device of the present invention.
[0018] Figure 3 This is a cross-sectional view of the combustion device with high combustion efficiency of the present invention.
[0019] Figure 4 This is a partially enlarged cross-sectional view of the combustion device with high combustion efficiency of the present invention.
[0020] Figure 5 This is a partially enlarged cross-sectional view of the outlet pipe of an existing gas burner.
[0021] Explanation of reference numerals in the attached drawings: 10 Combustion device; 20 Base; 30 Furnace head tube; 31 Mixing section; 311 Air inlet; 312 First mixing port; 313 First side; 314 Second side; 315 Second mixing port; 32 Air outlet section; 321 Straight section; 322 First bend; 323 Second bend; 324 Third bend; 325 Straight pipe section; 33 Mixing cover; 331 Air passage; 40 Gas nozzle; 90 Air outlet pipe; 91 Mixing port; L Baseline; O Origin. Detailed Implementation
[0022] Reference Figures 1 to 5 The figures shown are a perspective view, an exploded perspective view, and a cross-sectional view of the high-efficiency combustion device of the present invention. The combustion device 10 of the present invention includes a base 20 and a burner tube 30; wherein:
[0023] The burner head tube 30 is disposed within the base 20. The burner head tube 30 includes a mixing section 31 and an outlet section 32. The mixing section 31 extends axially along a horizontal and virtual baseline L. One end of the mixing section 31 is provided with an inlet 311, and a first mixing port 312 is provided on its radially outer periphery. The burner head tube 30 is provided with a virtual X-axis and a Y-axis that are coplanar with the baseline L. The X-axis is perpendicular to the baseline L, and the Y-axis is perpendicular to the X-axis. The mixing section 31 is provided with a first side 313 and an outlet section opposite to the first side 313. A second side 314 is adjacent to the Y-axis. The first mixing port 312 is disposed on the second side 314. The exhaust section 32 is connected to one end of the mixing section 31 opposite to the intake port 311. The exhaust section 32 is provided with a straight section 321 and a first curved section 322. The straight section 321 extends along the baseline L-axis and one end is connected to the mixing section 31. One end of the first curved section 322 is connected to one end of the straight section 321 opposite to the mixing section 31, and the other end extends away from the mixing section 31 and toward the Y-axis.
[0024] The burner tube 30 is connected to a gas nozzle 40, which is inserted into the mixing section 31 through the air inlet 311. A second mixing port 315 is formed between the inner periphery of the mixing section 31 and the outer periphery of the gas nozzle 40. The second mixing port 315 is open at one end opposite to the gas outlet section 32.
[0025] The burner tube 30 is provided with a mixing cover 33. One side of the mixing cover 33 is connected to the upper edge of the mixing section 31 in the vertical direction and the other side is connected to the lower edge of the mixing section 31 in the vertical direction. The mixing cover 33 covers but does not close the first mixing port 312.
[0026] The air inlet 311 protrudes from the base 20. One end of the air mixing cover 33 along the axial direction of the baseline L is disposed inside the base 20 and the other end protrudes from the base 20. The air mixing cover 33 and the second side 314 form an air channel 331. The two ends of the air channel 331 along the axial direction of the baseline L are respectively open.
[0027] The X-axis and the Y-axis form a rectangular coordinate system, and the intersection of the X-axis and the Y-axis forms an origin O. The first curved portion 322 is located in the second quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the first curved portion 322 is located on the side of the first curved portion 322 adjacent to the origin O. The air outlet section 32 is provided with a second curved portion 323. One end of the second curved portion 323 is connected to the end of the first curved portion 322 opposite to the straight portion 321. The second curved portion 323 is located in the first quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the second curved portion 323 is located on the side of the second curved portion 323 adjacent to the origin O.
[0028] The air outlet section 32 is provided with a third curved section 324. One end of the third curved section 324 is connected to the end of the second curved section 323 opposite to the first curved section 322. The third curved section 324 is located in the third quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the third curved section 324 is located on the side of the third curved section 324 adjacent to the origin O. The radius of the curved arc of the third curved section 324 is smaller than the radius of the curved arc of the first curved section 322 and the radius of the curved arc of the second curved section 323.
[0029] The air outlet section 32 is provided with a straight pipe section 325. One end of the straight pipe section 325 is connected to the end of the third bend section 324 opposite to the second bend section 323. The straight pipe section 325 extends in a straight line along a direction parallel to the X-axis toward the straight passage section 321. The end of the straight pipe section 325 opposite to the third bend section 324 is closed.
[0030] The combustion device 10 improves combustion efficiency through the aforementioned structure. Gas can enter the burner tube 30 through the air inlet 311. The negative pressure generated by the gas flow rate draws air in through the first mixing port 312 and the second mixing port 315. After the gas mixes with the air, it flows to the straight section 321. Because the opening direction of the first mixing port 312 and the bending direction of the first curved section 322 are on the same side of the mixing section 31, the air and gas can flow smoothly along the shape of the first curved section 322 after mixing, reducing the velocity loss of gas and air flowing in the burner tube 30. This also avoids reducing the initial velocity of the gas in the mixing section 31, allowing the mixing section 31 to introduce more air and improve combustion efficiency.
[0031] Based on the above, the present invention has the following advantages:
[0032] 1. A high-efficiency combustion device of the present invention, wherein the combustion device includes a base and a burner tube, the burner tube being disposed within the base, the burner tube including a mixing section and a gas outlet section, the mixing section extending axially along a horizontal and virtual baseline, one end of the mixing section having an air inlet and a first mixing port being disposed on the radially outer periphery, the burner tube being provided with a virtual X-axis and a Y-axis coplanar with the baseline, the X-axis being perpendicular to the baseline, and the Y-axis being perpendicular to the X-axis, the mixing section being provided with The device has a first side and a second side opposite to the first side, the second side being adjacent to the Y-axis. The first mixing port is located on the second side. The exhaust section is connected to the end of the mixing section opposite to the intake port. The exhaust section has a straight section and a first curved section. The straight section extends axially along the baseline and one end is connected to the mixing section. One end of the first curved section is connected to the end of the straight section opposite to the mixing section, and the other end extends away from the mixing section and closer to the Y-axis. The combustion device can improve combustion efficiency through the above structure.
Claims
1. A high combustion efficiency combustion device characterized by, Including: A base; A burner tube is disposed within the base. The burner tube includes a mixing section and an outlet section. The mixing section extends axially along a horizontal, virtual baseline. One end of the mixing section has an inlet and a first mixing port on its radially outer periphery. The burner tube has a virtual X-axis and a Y-axis coplanar with the baseline. The X-axis is perpendicular to the baseline, and the Y-axis is perpendicular to the X-axis. The mixing section has a first side and a second side opposite to the first side, the second side being adjacent to the Y-axis. The first mixing port is located at the first... On both sides, the gas outlet section is connected to the end of the gas mixing section opposite to the gas inlet. The gas outlet section is provided with a straight section and a first curved section. The straight section extends axially along the baseline and one end is connected to the gas mixing section. One end of the first curved section is connected to the end of the straight section opposite to the gas mixing section and the other end extends away from the gas mixing section and closer to the Y-axis. The burner tube is provided with a gas mixing cover. One side of the gas mixing cover is connected to the upper edge of the gas mixing section in the vertical direction and the other side is connected to the lower edge of the gas mixing section in the vertical direction. The gas mixing cover covers but does not close the first gas mixing port.
2. The high combustion efficiency combustion apparatus according to claim 1, characterized by: The air inlet protrudes outside the base. One end of the air mixing cover along the axial direction of the baseline is disposed inside the base and the other end protrudes outside the base. The air mixing cover and the second side form an air passage. The two ends of the air passage along the axial direction of the baseline are respectively open.
3. The high combustion efficiency combustion apparatus of claim 2, wherein: The X-axis and the Y-axis form a rectangular coordinate system, and the intersection of the X-axis and the Y-axis forms an origin. The first curved section is located in the second quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the first curved section is located on the side of the first curved section near the origin. The air outlet section is provided with a second curved section. One end of the second curved section is connected to the end of the first curved section opposite to the straight section. The second curved section is located in the first quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the curved arc of the second curved section is located on the side of the second curved section near the origin.
4. The high combustion efficiency combustion apparatus of claim 3, wherein: The air outlet section is provided with a third bend, one end of which is connected to the end of the second bend opposite to the first bend. The third bend is located in the third quadrant of the rectangular coordinate system of the X-axis and the Y-axis. The center of the bend arc of the third bend is located on the side of the third bend adjacent to the origin. The radius of the bend arc of the third bend is smaller than the radius of the bend arc of the first bend and the radius of the bend arc of the second bend.
5. The high combustion efficiency combustion apparatus of claim 4, wherein: The air outlet section is provided with a straight pipe section, one end of which is connected to the end of the third bend section opposite to the second bend section. The straight pipe section extends in a straight line in a direction parallel to the X-axis toward the straight section, and the end of the straight pipe section opposite to the third bend section is closed.
Citation Information
Patent Citations
Structural improvement of gas discharge pipe for gas burner
TW200728661A
U-shaped burner for grill
US20090126716A1