Quick-mounting type high-altitude torch igniter stable in operation

Abstract

The utility model discloses a stable-operation quick-mounting type high-altitude torch igniter, relates to the technical field of high-altitude torches, and aims to solve the problems that an existing high-altitude torch igniter is insufficient in quick assembly and disassembly, and the use flexibility and the overall working stability need to be improved. The end of the tube seat is fixedly connected with a flange plate, the symmetrical side surfaces of the tube seat are each fixedly connected with a self-locking seat, the two symmetrical sides of the tube seat are each provided with an ignition tube, the side surfaces of the ignition tubes are fixedly connected with a connecting rod, and one end of each connecting rod is fixedly provided with a steel ball self-locking end. The steel ball self-locking end is connected and buckled to the outer portion of the self-locking base in a sleeving mode, and two limiting plates are fixedly connected to the symmetrical side surfaces of the pipe base respectively. And the effects of quick assembly and disassembly, high use flexibility and high working stability are achieved.

Description

Technical Field

[0001] This utility model relates to the field of high-altitude flare technology, and in particular to a stable and quick-installation high-altitude flare igniter. Background Technology

[0002] This high-altitude flare igniter is meticulously designed to meet the precise ignition requirements of high-altitude flares. Utilizing advanced electronic pulse ignition technology, it generates a powerful electric spark in an extremely short time, ensuring reliable ignition of flare fuel even in complex high-altitude environments. Its high ignition energy and near 100% ignition success rate effectively eliminate the risk of ignition failure.

[0003] The existing high-altitude torch igniters have shortcomings in rapid assembly and disassembly, and their flexibility of use and overall operational stability need to be improved. Utility Model Content

[0004] The purpose of this invention is to provide a fast-installation high-altitude torch igniter that can be quickly assembled and disassembled, offering high flexibility and operational stability.

[0005] To achieve the above objectives, the present invention provides the following technical solution:

[0006] A stable and quick-installing high-altitude torch igniter includes a tube base, a flange fixedly connected to the end of the tube base, a self-locking seat fixedly connected to each of the symmetrical side surfaces of the tube base, an ignition tube respectively arranged at each of the symmetrical sides of the tube base, a connecting rod fixedly connected to the side surface of the ignition tube, and a steel ball self-locking end fixedly installed at one end of the connecting rod, the steel ball self-locking end being sleeved and snapped onto the outside of the self-locking seat.

[0007] By adopting the above technical solution, the various components can be installed and disassembled quickly and flexibly, which is highly practical and has strong operational stability.

[0008] Furthermore, two limiting plates are fixedly connected to the symmetrical side surfaces of the tube seat. One end of the limiting plate is provided with an arc-shaped notch, and the arc-shaped notch is adapted to the outer curvature of the ignition tube, and the ignition tube abuts against the arc-shaped notch of the limiting plate.

[0009] By adopting the above technical solution, the ignition tube can be installed flexibly and quickly.

[0010] Furthermore, a support bar is fixedly connected to the inner wall of the tube seat, and a threaded tube seat is provided at the middle position of the support bar, and a temperature sensor is installed in the internal thread of the threaded tube seat.

[0011] By adopting the above technical solution, the combustion status can be monitored and the temperature sensor can be installed flexibly.

[0012] Furthermore, a mounting base is fixedly connected to the side surface of the ignition tube, and an electronic igniter is snapped into the mounting groove of the mounting base.

[0013] By adopting the above technical solution, effective ignition operation can be performed.

[0014] Furthermore, a gas venting pipe is fixedly connected to the middle position of the end of the ignition tube, the outlet end of the gas venting pipe is placed inside the ignition tube, a gas guiding hose is installed at the inlet end of the gas venting pipe, and a solenoid valve is installed near the inlet end of the gas venting pipe.

[0015] By adopting the above technical solutions, the flexibility and convenience of the connection are improved.

[0016] Furthermore, the side surface of the self-locking seat is provided with an annular groove with a cross-section of arc. The self-locking end of the steel ball includes a base, a steel ball, a spring, and a movable sleeve. The steel ball is located at a circular hole on the side surface of the base. The movable sleeve is movably fitted onto the outside of the base, and the spring is installed inside the movable sleeve.

[0017] By adopting the above technical solution, effective self-locking operation can be performed.

[0018] In summary, the beneficial technical effects of this utility model are as follows:

[0019] This invention allows for quick installation. During installation, align the ignition tubes with the arc-shaped notches at the ends of the two limiting plates on the same side, then lock the steel ball self-locking end onto the end of the self-locking seat to quickly install the two ignition tubes on the symmetrical side surface of the pipe seat. Next, thread the temperature sensor onto the threaded pipe seat inside the pipe seat. Then, install the pipe seat on top of the riser pipe using a flange. Finally, connect the ignition pipe to the natural gas supply pipe via a gas guide hose. Combustion can then be performed. During operation, natural gas is introduced into the ignition pipe using the gas guide hose, and then the electronic igniter is used to ignite the outlet end of the ignition pipe. The flame then sprays out from the upper end of the ignition tube, igniting the gas discharged from the pipe seat. All components of the igniter can be quickly and easily disassembled and assembled, making it highly practical and flexible in assembly. Attached Figure Description

[0020] Figure 1 This is a first-view perspective view of the three-dimensional structure of this utility model;

[0021] Figure 2 This is a second-view perspective view of the three-dimensional structure of this utility model.

[0022] In the diagram: 1. Pipe seat; 2. Flange; 3. Self-locking seat; 4. Steel ball self-locking end; 5. Ignition tube; 6. Mounting base; 7. Electronic igniter; 8. Connecting rod; 9. Limiting plate; 10. Gas venting tube; 11. Solenoid valve; 12. Gas venting hose; 13. Temperature sensor. Detailed Implementation

[0023] The method of this utility model will be further described in detail below with reference to the accompanying drawings.

[0024] Reference Figure 1 , Figure 2 A stable and quick-installing high-altitude torch igniter includes a tube base 1, with a flange 2 fixedly connected to the end of the tube base 1. A self-locking seat 3 is fixedly connected to each of the symmetrical side surfaces of the tube base 1. An ignition tube 5 is located on each of the symmetrical sides of the tube base 1. A connecting rod 8 is fixedly connected to the side surface of the ignition tube 5. A steel ball self-locking end 4 is fixedly installed at one end of the connecting rod 8. The steel ball self-locking end 4 is sleeved and snapped onto the outside of the self-locking seat 3. An annular groove with a circular cross-section is provided on the side surface of the self-locking seat 3. The steel ball self-locking end 4 includes a base, a steel ball, a spring, and a movable sleeve. The steel ball is located at a circular hole on the side surface of the base. The movable sleeve is movably sleeved onto the outside of the base. The spring is installed inside the movable sleeve. Two limiting plates 9 are fixedly connected to the symmetrical side surfaces of the tube base 1. One end of each limiting plate 9 has an arc-shaped... The ignition tube 5 has an arc-shaped notch that matches the outer curvature of the ignition tube 5. The ignition tube 5 rests against the arc-shaped notch of the limiting plate 9. A support strip is fixedly connected to the inner wall of the tube seat 1, and a threaded tube seat is provided at the middle position of the support strip. A temperature sensor 13 is installed in the internal thread of the threaded tube seat. This allows for quick installation during use. During installation, align the ignition tube 5 with the arc-shaped notches at the ends of the two limiting plates 9 on the same side, and then lock the steel ball self-locking end 4 onto the end of the self-locking seat 3 to quickly install the two ignition tubes 5 on the symmetrical side surface of the tube seat 1. Then, thread the temperature sensor 13 onto the threaded tube seat inside the tube seat 1. Finally, install the tube seat 1 on the top of the riser pipe through the flange 2. The entire assembly operation is quick and convenient, and the connection is stable, ensuring the stability of each component during operation. The overall practicality is strong.

[0025] Reference Figure 1A mounting base 6 is fixedly connected to the side surface of the ignition tube 5. An electronic igniter 7 is snapped into the mounting groove of the mounting base 6. A gas priming tube 10 is fixedly connected to the middle position of the end of the ignition tube 5. The gas outlet end of the gas priming tube 10 is placed inside the ignition tube 5. A gas guide hose 12 is installed at the gas inlet end of the gas priming tube 10. A solenoid valve 11 is installed near the gas inlet end of the gas priming tube 10. The gas priming tube 10 is connected to the natural gas supply pipe through the gas guide hose 12, so that combustion can be performed. During operation, natural gas is introduced into the interior of the gas priming tube 10 through the gas guide hose 12, and then the electronic igniter 7 is used to ignite the gas outlet end of the gas priming tube 10. At this time, the flame of combustion is ejected from the upper end of the ignition tube 5, which can then ignite the gas discharged from the tube seat 1. The operation is stable.

[0026] Working principle: During use, quick installation is required. Align the ignition tube 5 with the arc-shaped notches at the ends of the two limiting plates 9 on the same side, then lock the steel ball self-locking end 4 onto the end of the self-locking seat 3 to quickly install the two ignition tubes 5 on the symmetrical side surface of the pipe seat 1. Then, thread the temperature sensor 13 onto the threaded pipe seat inside the pipe seat 1. Next, install the pipe seat 1 on the top of the riser pipe via the flange 2. Then, connect the gas inlet pipe 10 to the natural gas supply pipe via the gas inlet hose 12. Combustion operation is then possible. During operation, natural gas is introduced into the gas inlet pipe 10 via the gas inlet hose 12, and then the electronic igniter 7 is used to ignite the gas outlet of the gas inlet pipe 10. The flame then sprays out from the upper end of the ignition tube 5, thus igniting the gas discharged from the pipe seat 1.

[0027] The specific real-time examples described herein are preferred real-time examples of this utility model and are not intended to limit the scope of protection of this utility model. Therefore, all equivalent changes made to the structure, shape, and principle of this utility model should be included within the scope of protection of this utility model.

Claims

1. A stable and quick-installation high-altitude torch igniter, comprising a tube base (1), characterized in that: A flange (2) is fixedly connected to the end of the pipe seat (1). A self-locking seat (3) is fixedly connected to the symmetrical side surface of the pipe seat (1). An ignition pipe (5) is provided at the symmetrical two sides of the pipe seat (1). A connecting rod (8) is fixedly connected to the side surface of the ignition pipe (5). A steel ball self-locking end (4) is fixedly installed at one end of the connecting rod (8). The steel ball self-locking end (4) is sleeved and snapped onto the outside of the self-locking seat (3).

2. The stable-operating, quick-installation high-altitude torch igniter according to claim 1, characterized in that: Two limiting plates (9) are fixedly connected to the symmetrical side surface of the tube seat (1). One end of the limiting plate (9) is provided with an arc-shaped notch, and the arc-shaped notch is adapted to the outer curvature of the ignition tube (5). The ignition tube (5) abuts against the arc-shaped notch of the limiting plate (9).

3. The stable-operating, quick-installation high-altitude torch igniter according to claim 1, characterized in that: A support bar is fixedly connected to the inner wall of the tube seat (1), and a threaded tube seat is provided at the middle position of the support bar, and a temperature sensor (13) is installed in the internal thread of the threaded tube seat.

4. The stable-operating, quick-installation high-altitude torch igniter according to claim 1, characterized in that: An mounting base (6) is fixedly connected to the side surface of the ignition tube (5), and an electronic igniter (7) is snapped into the mounting groove of the mounting base (6).

5. A stable-operating, quick-installation high-altitude torch igniter according to claim 1, characterized in that: An air intake pipe (10) is fixedly connected to the middle position of the end of the ignition pipe (5). The outlet end of the air intake pipe (10) is placed inside the ignition pipe (5). An air guide hose (12) is installed at the air inlet end of the air intake pipe (10). A solenoid valve (11) is installed near the air inlet end of the air intake pipe (10).

6. A stable-operating, quick-installation high-altitude torch igniter according to claim 1, characterized in that: The self-locking seat (3) has an annular groove with a cross-section of arc on its side surface. The steel ball self-locking end (4) includes a base, a steel ball, a spring, and a movable sleeve. The steel ball is located at a circular hole on the side surface of the base. The movable sleeve is movably fitted onto the outside of the base, and the spring is installed inside the movable sleeve.

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